DNVGL-ST-0377 Standard for shipboard lifting appliances · 2016. 5. 19. · 9.6 Hydraulic systems...
Transcript of DNVGL-ST-0377 Standard for shipboard lifting appliances · 2016. 5. 19. · 9.6 Hydraulic systems...
The electronic pdf version of this document available free of chargefrom httpwwwdnvglcom is the officially binding version
DNV GL AS
STANDARD
DNVGL-ST-0377 Edition May 2016
Standard for shipboard lifting appliances
FOREWORD
DNV GL standards contain requirements principles and acceptance criteria for objects personnelorganisations andor operations
copy DNV GL AS May 2016
Any comments may be sent by e-mail to rulesdnvglcom
This service document has been prepared based on available knowledge technology andor information at the time of issuance of thisdocument The use of this document by others than DNV GL is at the users sole risk DNV GL does not accept any liability or responsibilityfor loss or damages resulting from any use of this document
Cha
nges
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Standard mdash DNVGL-ST-0377 Edition May 2016 Page 3Standard for shipboard lifting appliances
DNV GL AS
CHANGES - CURRENT
This is a new document
Con
tent
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DNV GL AS
CONTENTS
Changes - current3
Section 1 General information 811 Introduction812 Services 1613 Certification procedure 1814 Type of services20
Section 2 Documentation and certification 2221 Documentation to be submitted2222 Certification 23
Section 3 Materials2631 General 2632 Selection of materials2633 Manufacture and testing2834 Materials for welded components 3035 Materials for hydraulic cylinders3536 Forgings3737 Steel castings 3938 Bolts and nuts 41
Section 4 Design and calculation principles 4341 General 4342 Design principles 4343 Calculation principles5044 Proof of structural safety 5645 Proof of safety against overturning 5846 Proof of fatigue strength 5947 Proof of suitability for use7348 Joints 7449 Special structural elements 81
Section 5 Cranes and supporting structures 9951 General 9952 Crane groups 10053 Design loads 102
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DNV GL AS
54 Hoist load coefficients 10855 Load combinations and partial safety factors 11256 Proofs 11757 Requirements for design and equipment 120
Section 6 Special lifting appliances and means of transport 12961 General 12962 Rope and chain hoists 12963 Ramps and car decks13364 Lifting appliances for research work13765 Industrial cargo-handling vehicles13866 Means of conveying persons139
Section 7 Loose gear and interchangeable components14271 General 14272 Loose gear 14273 Interchangeable components15374 Marking of loose gear and interchangeable components16075 Wear damage repair 163
Section 8 Ropes and rope accessories 16581 General 16582 Wire ropes 16583 Fibre ropes17184 Rope-end attachments17385 Tests and examinations 17486 Documentation176
Section 9 Mechanical parts 17891 General 17892 Design criteria and operational requirements17993 Power drives18094 Slewing gears and slew rings 18095 Winches 18296 Hydraulic systems18597 Protective measures and safety devices 18798 Examination of drawings and supervision of construction 18799 Documentation189
Section 10 Electrical equipment192
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tent
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DNV GL AS
101 General 192102 Design criteria and operational requirements193103 Drives and brakes193104 Cables and lines195105 Switches196106 Protective measures and safety devices 197107 Examination of drawings and supervision of construction199108 Documentation200
Section 11 Construction of steel components 201111 General 201112 Requirements for manufacturers 201113 Design details 205114 Types of welds209115 Workmanship and testing of weld joints214116 Examination of drawings and supervision of construction217117 Documentation218
Section 12 Technical and operational safety requirements 220121 General 220122 Design requirements220123 Equipment225124 Safety devices226125 Passive protective measures228126 Stowage and lashing devices229127 Operational requirements 230
Section 13 Testing and examination of shipboard lifting appliances 232131 General 232132 Supervision of construction 233133 Initial test and examination 239134 Periodic tests and examinations 242135 Extraordinary tests and examinations 246136 Wear damage repair 247137 Lifting appliance documentation252
Appendix A Calculation of dynamic forces due to motions of the ship257A1 General 257A2 Dynamic forces generated by ships and similar floating bodies 257A3 Dynamic forces due to pontoons or barges260
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DNV GL AS
Appendix B Detail classification for fatigue strength analysis (FAT classes) 261B1 261
Appendix C Wind loads form and sheltering coefficients275C1 General 275C2 Form coefficients c 275C3 Sheltering coefficients η 275
Appendix D Rigging plan279
Changes ndash historic 280
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 8Standard for shipboard lifting appliances
DNV GL AS
SECTION 1 GENERAL INFORMATION
11 Introduction
111 Objective
1111 This standard provides requirements for certification and verification of lifting appliances intendedfor load handling within and outside vessel while in the harbour or in sheltered waters and within the vesselwhile at sea
Guidance noteFor lifting appliances intended for load handling outside vessel while at open sea and load handling onboard offshore unitsinstallations see DNVGL ST 0378 Standard for Offshore and Platform Lifting Appliances
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112 Scope
1121 This standard covers the design materials fabrication installation testing and commissioning ofshipboard lifting appliances and industrial lifting appliancesThe categorization of lifting appliances is based on installation and intended function for the lifting appliance
a) Shipboard lifting appliances
mdash lifting appliances on board ships intended for load handling within and outside ships while in theharbour and within ships while at sea
b) Industrial lifting appliances
mdash lifting appliances onshore and offshore not covered by a) and DNVGL ST 0378Guidance noteThe main purpose of the lifting appliance will define the category of the lifting appliance and relevant applicable standard
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
1122 Each lifting appliance has its separate intended functions Examples of intended functions are butnot limited to
mdash loading and discharging of shipsmdash handling of provision store and spare parts cargo hoses gangways and ammunitionmdash handling of Suez Canal boats and search lightsmdash conveyance of personspersonnelmdash handling of ramps and moveable cargo decks etc
1123 Requirements presented herein are minimum requirements to be satisfied although subject toacceptance by the Society other minimum requirements may be agreed eg based on new technologyavailable at the time of application for certification
1124 The requirements of this standard may be supplemented with additional requirements whereinstallation of specific design or assessment shows that standards that provides equivalent or higher level ofintegrity and safety are more appropriate
1125 The standard consists of a three level hierarchy of documents
mdash Sec1 and Sec2 provides principles and procedures of the Societys classification certification verificationand consultancy services
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 9Standard for shipboard lifting appliances
DNV GL AS
mdash Sec3 through Sec13 provides technical provisions and acceptance criteria as well as the technical basisfor the services stated in the first two sections
mdash Appendices provides proven technology and sound engineering practice as well as guidance for the higherlevel documents mentioned in this document
1126 This standard distinguishes between
mdash information and description of servicesmdash requirements
Consequently these two subjects are separated and the standard is divided into three parts
mdash Sec1 - Sec2 General information application definitions and references Description of applicableservices and relations to rules and regulation from institutions other than the Society
mdash Sec3 - Sec13 Requirements and technical provisionsmdash Appendices
113 Application
1131 This standard shall be applied for certification of shipboard lifting appliances for vessels with classnotation Crane This standard may also be applied as voluntary basis for verification and certification oflifting appliances that are not classed with the Society
Guidance noteThe standard may also be applied to industrial cranes
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1132 The requirements presented herein should be applied consequently from concept design through thefinal construction including major modifications
1133 Specifications of the services provided by this standard are given in [12] and [14]
1134 The standard does not apply to launching appliances for LSA launching gear for diving equipmentand ROVs structural parts of ramps and car decks dredging appliances which are no loading gear personnellifts (elevators) jacks overhead drilling equipment fork lifts portable hoisting gear etc
1135 Personnel lifting with cranes otherwise designed for lifting of loadscargo may be covered uponagreement
1136 Without prejudice to [1124] deviations from the requirements given in this standard may onlybe substituted where shown to provide an equivalent or higher level of integrity or safer than under thisstandard
1137 At the Societyrsquos discretion equivalent solutions and exemptions from the requirements given in thisstandard may be accepted
1138 In case of conflict between requirements given in this standard and a reference document therequirements given in this standard shall prevail
1139 Where reference is made to codes other than the Societys documents the valid revision shall betaken as the revision which was current at the date of issue of this standard unless otherwise noted
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 10Standard for shipboard lifting appliances
DNV GL AS
114 Relation to the Societys other documents
1141 For lifting appliances covered by the class notation Crane see RU SHIP Pt6 Ch5 Sec3Permanently installed cranes ndash Crane
115 Definitions abbreviations symbols and references1151 AccessoriesLoad-bearing not rigidly attached interchangeable parts which may be integral components of liftingappliances and loose gear as well as employed individually such as Hooks blocks shackles swivels ringschains claws clamps pliers load fastening ropes (slingsstrops) lifting straps etc
1152 Active cable tensioning system (ACT)System keeping the tension of the hoisting wire to a given set point value
Guidance noteA supply of external energy is required
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
1153 Active heave compensation system (AHC)System that maintains the position of the load to a given set point value
Guidance noteA supply of external energy is required
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
1154 Actual hook loadThe static weight of the load attached to the hook includes the useful load lifted plus any loose gear usedsuch as slings lifting beams etc
1155 Additional class notationsCode used by the classification societies to confirm that a vessel possesses certain systems equipment orfeatures covered by the classification (Examples are HELDK Crane E0 and F-AMC)
Guidance noteE0 means that the vessel complies with requirements for having unattended machinery space and F-AMC means that the vesselcomplies with requirements for additional fire protection in this case both for accommodation machinery space and cargo space
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
1156 Ship type notationCode used by the classification societies to define a type of vessel related to its most typical service (Tankerfor oil Passenger ship and Crane vessel are typical examples)
1157 Automatic overload protection system (AOPS)A system that automatically safeguards and protects the crane against overload and ldquoover-momentrdquo duringoperation by allowing the hook to be pulled away from the crane in order to avoid significant damage
1158 Certificate of conformityA document attesting that a product or service is in conformity with specific standards or technicalspecifications (ISO ldquoCertification - Principles and practicerdquo 1980) Issued by manufacturer or vendor
1159 Competent personbodyPerson or body possessing knowledge and experience required for performing thorough examination and testof lifting appliances and loose gear and who is acceptable to the competent authority
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DNV GL AS
11510 Crane stiffnessCoefficient defined as the weight attached to the hook necessary to obtain a unit deflection at the hook level
11511 CustomerAgreement (contract) holder with the Society Signifies the party who has requested the Societyrsquos service
11512 Dead loadsDead loads are the weights of all the fixed and mobile components of lifting appliances and loose gearpermanently present during operationFor the purpose of marking the dead loads of loose gear are designated as weight by the ILO The unit isspecified in tons (t) or kilograms (kg)
11513 DesignerSignifies a party who creates documentation submitted to the Society for approval or information
11514 Design approvalVerifying that a design represented by a drawing or set of drawings is found to comply with all requirementgiven in a specified Society standard or Society regulation
Guidance noteIn the Societys business procedures design approvals are valid for one order only One order however may include a specifiednumber of units for specified locationsvessels
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11515 Design approval letterWritten confirmation of a design approval
11516 Design assessment for type approvalExamination and acceptance of a design for type approval The type approval will be assigned first after aprototype test also has been successfully carried out
11517 Design dynamic factorThe dynamic factor applied to the working load for a specific SWL
Guidance noteFor an offshore crane the design dynamic factor is normally referred to the still water condition for determining the SWL at still waterThe design dynamic factor may however be defined also to refer to a specified significant wave height
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
11518 Design verification report (DVR)Formalized report confirming the result of a completed design verification assignment
11519 Dynamic factorA variable factor representing the dynamic effects that the working load is exposed to Also named dynamiccoefficient
11520 Dynamic loadThe working load when subjected to (multiplied with) a dynamic factor
11521 Dynamic load chartDiagram or table showing rated capacity depending on sea state and on radius or boom angle
11522 Engineered liftSafe lift planned by qualified engineers with basis in thorough information with respect to crane capacitycrane functions and performance rigging crane support as well as weather and sea conditions
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DNV GL AS
11523 Heavy lift craneCrane with SWL above 2500 kN
11524 ILOInternational Labour Organization
11525 Inertia forcesThe forces induced by change of velocity
11526 Inspection certificate 31A document issued by the manufacturer which contains the results of all the required tests It shall certifythat the tests have been carried out by the manufacturer on samples taken from the delivered productsdirect Ref EN 10204 and ISO 10474
11527 Inspection certificate 32A document prepared by both the manufacturers authorized inspection representative independent of themanufacturing department and either the purchasers authorized representative or the inspector designatedby the official regulations and in which they declare that the products supplied are in compliance with therequirements of the order and in which test results are supplied Ref EN 10204 and ISO 10474
11528 Lifting applianceMachine or appliance used for the purpose of lifting goods and materials or in special modes personnel
11529 Lifting equipmentGeneral expression including lifting appliances lifting gear loose gear and other lifting attachments usedseparately or in combination
11530 Lifting gearRef also Accessories ([1151]) and Loose gear ([11533])Load carrying accessories used in combination with a lifting appliance however that are not necessarily apart of the permanent arrangement of the lifting appliance such as
mdash attachment rings shackles swivels balls pinsmdash sheaves hook-blocks hooks load cellsmdash loose gear
Guidance noteLifting gear considered as separate components shall be designed and tested in accordance with the provisions for loose gear
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
11531 Load chartDiagram or table showing rated capacity depending on radius or boom angle
11532 Loose gearMeans by which loads can be attached to lifting appliances but which do not form part either of thelifting appliance or of the load They include devices and steel structures such as but not limited tograbs spreaders lifting magnets traverses etc as well as Accessories (ref[1151]) which are integralcomponents of the loose gear
11533 Machinery componentsRotating components transferring torque for drivingbraking purpose Examples are gearboxes wheels andshafts
11534 Man riding winchDevice specially designed for hoistinglowering of a person
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 13Standard for shipboard lifting appliances
DNV GL AS
11535 Manual overload protection system (MOPS)System activated by the crane operator protecting the crane against overload and ldquoover-momentrdquo byreducing the load-carrying capacity and allowing the hook to be pulled away from the crane
11536 Mean time to failure (MTTF)The mean value of service time until failure occurs
11537 MechanismDevices needed to cause or to stop a relative motion between two rigid parts of a crane between the craneand its foundation or between the crane and the lifted load Thus motors brakes transmission systems andsimilar components are defined as mechanisms
11538 Mobile deck craneA mobile deck crane is a cable-controlled crane mounted on crawlers or rubber-tired carriers or a hydraulic-powered crane with a boom mounted on truck-type carriers or as self-propelled types
11539 Nominal loadNominal load is the designation for the maximum permissible useful load of lifting appliances and loose gearLifting appliances and loose gear can have different nominal loads depending on varying equipment conditionor operational conditions cable tackle systems or load radii
11540 OverloadLoad which exceeds the safe working load (SWL)
11541 Over-momentLoad moment which exceeds the maximum load moment (safe working load (SWL) multiplied by radius)
11542 Passive cable tensioning system (PCT)System keeping the tension of the hoisting wire between predefined limits using stored energy
11543 Passive heave compensation system (PHC)System that maintains the position of the load between predefined limits using stored energy
11544 Probability of failure on demand (PFD)Probability of failure on demand
11545 Product certificate (general)A compliance document validated and signed by the issuing organization
mdash identifying the product that the certificate applies tomdash conforming compliance with the referred requirements
It is required that
mdash the tests and inspection s have been performed on the certified product itself or on samples taken fromthe certified product itself
mdash the tests were witnessed by a qualified representative of the organization issuing the certificate or hisauthorized representative
11546 Product certificate (the Societyrsquos)The Societys product certificate is a compliance document validated and signed by the issuing organizationand the Societys representative
mdash identifying the product that the certificate applies tomdash confirming compliance with referred requirements
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 14Standard for shipboard lifting appliances
DNV GL AS
It is required that
mdash the tests and inspection s have been performed on the certified product itself or on samples taken fromthe certified product itself
mdash that the tests were witnessed by a qualified representative of the organization issuing the certificate andthe Societys representative or in accordance with special agreements
11547 PurchaserCompany or person who orders the lifting equipment from a manufacturer This standard does not necessarilyrequire that the purchaser will need to have any direct relationship to or communication with the Society
11548 Rated capacityActual hook load that the crane is designed to lift for a given operating condition (eg boom configurationreeving arrangement off leadside lead heeltrim radius wave height etc)
11549 REPRope exit point Location on the lifting appliance where the rope is suspended - typically found at the outersheave in the crane boom tip
11550 RiskCombination of the probability of occurrence (frequency) of harm and the severity (consequence) of theharm
11551 Risk control measure (RCM)A means of controlling a single element of risk typically risk control is achieved by reducing either theconsequence or the frequencies
11552 ROVRemote operated vehicle
11553 Running riggingWire ropes passing over rope sheaves of guide rollers or wound on winches irrespective of whether or notthe ropes are moved under load
11554 Safe working load (SWL)Safe working load is the international designation for the nominal load by ILO The abbreviation SWL is usedfor marking the lifting appliance loose gear and accessoriesThe unit of SWL is specified in tons (t) or kilograms (kg)
11555 Significant wave height HsignAverage height of the highest one third of the individual wave heights in a short-term constant seastatetypically 3 hours
11556 The SocietyThe Society signifies DNVGL
11557 Standing riggingRopes that are not turned round or wound on to winches (eg guided wires pendants stays)
11558 Subsea cranesCranes intended for handling of unmanned submersibles for lowering to and retrieval from below sea level
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 15Standard for shipboard lifting appliances
DNV GL AS
11559 Test reportA document signed by the manufacturer stating
mdash conformity with requirements given by a relevant standardmdash that tests are carried out on samples from the current production
11560 Type approvalApproval of conformity with specified requirements on the basis of systematic examination of one or morespecimens of a product representative of the production
11561 Type approval certificate (DNV GL)A document issued by the Society confirming compliance with specified requirements is named DNV GL TypeApproval Certificate (TA)
11562 Useful loadUseful load is the load which may be directly lifted by the supporting component (eg cargo hook or grab) ofthe lifting appliance by the lift car of a lift by the platform of a lifting platform or by loose gearThe useful load consists of the load to be transported and where applicable also of the dead load of theloose gear
11563 VerificationA service that signifies a confirmation through the provision of objective evidence (analysis observationmeasurement test records or other evidence) that specified requirements have been met
11564 VesselA common term for ships craft offshore units and offshore installations
11565 Working load (suspended load)Also designated ldquoHoist loadrdquoThe static weight of the useful load lifted plus the weight of the lifting gear The working load is subjected toinertia forces
11566 Works product certificateReference is made to RU SHIP Pt1 Ch3 Sec5 [25] A document signed by the manufacturer stating
mdash conformity with rule requirementsmdash that tests are carried out on the certified product itselfmdash that tests are made on samples taken from the certified product itselfmdash that tests are witnessed and signed by a qualified department of the manufacturers
116 Crane design types
1161 Winch luffing crane a crane where the boom is controlled by wire ropes through a winch
1162 Cylinder luffing crane a crane where the boom is controlled by hydraulic cylinder(s)
1163 Knuckle boom crane a crane where the boom is hinged and the boom and knuckle angles arecontrolled by a set of hydraulic cylinders
1164 Derrick crane a simple crane consisting of a vertical mast and a hinged jib The derrick crane isprovided with devices for raising and lowering a load luffing the jib and slewing the jib about the mast
1165 Overhead travelling crane a crane which lifts the object by a trolley which normally moveshorizontally along the crane beam The crane beam ends have wheels running on rails at high level
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DNV GL AS
1166 Gantry crane a crane which lifts the object by a trolley which normally moves horizontally along thecrane beam The crane beam is supported by vertical legs having wheels running on rails at ground level
1167 A-frame crane a hinged frame intended for lifting Hydraulic cylinders control the movement of theA-frame while a winch is fitted for hoisting and lowering the load
117 Design temperature
1171 Design temperature is a reference temperature used as a criterion for the selection of steel grades
1172 The design temperature TD for lifting appliances is defined as the lowest acceptable servicetemperature for the crane
1173 For shipboard lifting appliances installed on vessels with Crane notations the design temperaturesof the appliances shall be compatible with the design temperature specified for the vesselunit
1174 If not otherwise specified design temperature according to Table 1-1 shall be applied
Table 1-1 Design temperature for lifting appliances
Type of Lifting Appliance Design temperature Corresponding Extreme Low Temperature
Shipboard Lifting Appliances -10degC (-30degC)
Engine rooms and other similar spaces withcontrolled temp +10degC (0degC)
118 Extreme low temperatureThe lowest temperature estimated to appear in an area with a corresponding specified design temperature
12 Services
121 Introduction
1211 This sub-section describes possible combinations of the different services offered Furthermorevarious alternatives are described for confirmation of the various services by the Society
1212 Figure 1-1 describes the services offered and the associated documents issued by the Society toproof compliance
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 17Standard for shipboard lifting appliances
DNV GL AS
Figure 1-1 Alternatives for documentation that may be issued to Customers depending on typeand combination of services requested
122 Regulatory basis
1221 This standard is based on the Societyrsquos understanding and interpretation of the ILO ConventionNo152 of 1979
123 Acceptance by national authorities
1231 Regulatory bodies such as port authorities flag administrations shelf authorities and municipal orgovernmental health and safety authorities require that lifting appliances and loose gear shall be certifiedNormally the Societys certification in accordance with this standard will satisfy the authoritiesrsquo requirements
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 18Standard for shipboard lifting appliances
DNV GL AS
1232 In cases where requirements laid down by the pertinent body exceeds the Societys requirementsdescribed in Sec3 through Sec13 The Society may as a voluntary service include the additionalrequirements in the examination and confirm whether or not they are found to be fulfilled
13 Certification procedure
131 General
1311 The following parts components and systems are covered by this standard
mdash all load-carrying structural members and components of the lifting appliancemdash cargo hooks chains rings blocks sheaves shackles lifting beams swivels and ropesmdash structural integrity of grabs hydraulic dampers or other load transferring componentsmdash rope drumsmdash slewing bearing including fastenersmdash power systems (for hoisting derricking slewing and travelling)mdash brakes and braking systemsmdash safety equipmentmdash protection against firemdash seating and fasteners for prime movers winches and for bearings of power transmitting componentsmdash control and monitoring systemsmdash electrical installation
1312 The following activities are covered by this standard
mdash design examinationmdash survey during fabrication and installationmdash witness testing and marking
132 Design examination
1321 Load-carrying and other important components of a lifting appliance are subject to designexamination with respect to strength and suitability for its purpose A design approval is granted when thedesign examination has been concluded without detection of non-compliancesThe design examination may be substituted partly or completely by enhanced manufacturing survey andortesting In cases where the substitutions are applied for by the customer agreements shall be made betweenthe customer and the Society regarding possible reductions of documentation to be submitted for approvalinformationUpon special agreement the design examination may be substituted by a strength evaluation based upontesting until failureStrength examination of components related to power supply and safety equipment is normally not carriedout by the Society
Guidance noteThe Societyrsquos splitting of the certification process in the sequences design approval manufacturing survey (including installationsurvey) and testing shall be considered as a part of the Societyrsquos internal scheme to organize its workThe Societyrsquos reports covering the separate phases is considered internal documents and information enabling the progress of thecertification project
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 19Standard for shipboard lifting appliances
DNV GL AS
The Societyrsquos formal documentation of the certification to the customer will be the product certificate Form 7103a issued aftercompleteion of manufacturing process and full testing at the manufacturer and CG2 issued after installation and full testing onboardin accordance with ILO152 requirements For lifting appliances not subject to ILO 152 test report in accordance with Form OLA101may be issued after installation and full testing onboard
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
1322 Each lifting appliance is normally given a separate design approval
1323 The design approval may be obtained either on a case-by-case basis or as a type approvalThe type approval means that the design as approved can be applied for identical units to be fabricated ierequested documents need not be submitted for each unitThe type approval will be based on certain conditions and its period of validity will be limitedReference is made to the Societys document DNVGL CP 0338 Type approval scheme
133 Survey during fabrication and installation
1331 Normally a survey during manufacture of each separate lifting appliance shall be carried out by theSocietys surveyor in order to ascertain compliance with the approved drawings other requirements given inthis standard as well as general good workmanship
1332 As an alternative to survey during manufacture of each separate lifting appliance modified surveyprocedures and survey arrangements may be accepted provided the manufacturer operates a quality-assurance system approved and certified by the Society Acceptance shall be clearly formalized
1333 After a lifting appliance has been installed on its permanent foundation and before testing can takeplace it shall be subjected to a survey by a surveyor of the Society
134 Testing and marking
1341 Components and each completed lifting appliance shall be subjected to functional testing and load-testing as specified in Sec13
135 Extension of scope of work
1351 Upon request from the customer the scope of work may be extended beyond the subjects andaspects covered in this standard
1352 Extensions shall be agreed in writing The Society may if found necessary require that the customerpresents reference documents for the extended scope of work such as authority regulations norms andstandards
1353 In case of disputes regarding interpretations of requirements on which extended work is based thecustomer shall contact the publisherowner of the requirements and obtain their written interpretationIf the publisherowner is not willing to interpret the disputed requirement or an interpretation for otherreasons cannot be acquired the respective extension of the scope of work shall be omitted
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DNV GL AS
136 Reduced scope of work
1361 For lifting appliances not to be installed on vessels classed by the Society upon request from andagreement with the customer parts of the scope of work components systems or specific aspects orrequirements may be excluded from the scope of work specified in the standard This will be annotated in thedocumentary evidence of the completed assignment (certificate)
1362 The Society will not agree to limit the scope of work or parts of the suggested services if they are ofthe opinion that this may lead to hazards or unacceptable lowering of the safety standard
14 Type of services
141 Basic certification
1411 The basic requirements presented in Sec3 through Sec13 are considered to cover the requirementsgiven in the ILO Convention No152 of 1979 specified in [1221] Lifting appliance and loose gear foundto comply with these basic requirements are qualified for the Societys product certification whereupon theproduct certificate Form 7103a may be issued based on FAT (Factory Acceptance Test) and survey Followingsuccessful testing and survey after installation onboard a DNVGL CG2 certificate will be issued for cranescovered by the ILO regime (cargo cranes) For cranes not covered by the ILO regime a test report FormOLA101 will be issued by the Society following successful onboard testing The cargo gear register (CG1 ifpublished by the Society) may be endorsed accordingly either as ILO crane or as other lifting appliances
1412 The basic requirement covers the two categories of lifting appliances a) and b) defined in [121] aswell as loose gear components allocated the same lifting appliances as well as personnel lifting as denoted in[122]
1413 Some details of the basic requirements given in Sec3 through Sec13 are different for the differentcategory of lifting appliance a) and b) Furthermore some specific requirements are stated for cranes alsoused for personnel lifting
142 Cranes included in class scope
1421 On a voluntary basis cranes installed on board vessels and offshore units classed with the Societymay be included in the scope of work covered by classification In such cases the vesseloffshore unit will beassigned the additional class notation Crane or Crane(N)In order to obtain this notation at least the main crane onboard shall have been certified in accordance withthe basic requirements given in Sec3 through Sec13 as well as having been assigned the product certificateCG2 or test report Form OLA101
1422 Some of the requirements given in this standard have been extended with additional detailedrequirements for cranes to be covered by classification
143 Assignments completed before installation
1431 Assignments completed at the manufacturersrsquo premises can be agreed Such services are normally tobe completed with monitoring of tests at the manufacturer (FAT-tests) Applicable reports or certificates maybe issued See also [1432]
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 21Standard for shipboard lifting appliances
DNV GL AS
1432 The reason for or purpose of such assignments may eg be
mdash completed certification of loose gear or components The Society will normally issue the product certificateCG3 after completion of the tests
mdash provisional certification after FAT-test For instance if final destination is not decided or if themanufacturer is producing for stock Or the customer has requested FAT-tests and a documentaryconfirmation of the Societyrsquos service rendered until a certain point A Manufacturing Survey ReportCertificate of Conformity may be assigned
See also Figure 1-1
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 22Standard for shipboard lifting appliances
DNV GL AS
SECTION 2 DOCUMENTATION AND CERTIFICATION
21 Documentation to be submitted
211 General
2111 The documentation necessary for verification assignments will depend on the scope of work agreedThe documentation and information requirements stated below are necessary for design approval andensuing certification
212 Documentation requirements
2121 Documentation shall be submitted as required by Table 2-1 as applicable for the lifting appliance
Table 2-1 Documentation requirements
Object Document type Additional description Shipboardcranes
Shipboardcranes(class
notation)
C010 - Design criteria
Load charts andor load tablesdynamic factors
Environment conditions
Category of crane see definitions [112]
Particulars of brake spring performance
FI FI
C020 - Assembly or arrangementdrawing FI FI
C030 - Detailed drawing
Crane structure and components forslewing luffing and hoisting Gears andbrakes for shipboard cranes are normallynot subject to approval Drawings of gearstransmitting braking forces should containrelevant parameters including torquecapacity
AP AP
C040 - Design analysis FI FI
C050 - Non-destructive testing (NDT)plan FI FI
Z060 - Functional description FI FI
General
Z161 - Operation manual FI FI
Power supply Z030 - System arrangement plan
Type and maker of prime mover orspecification of other main andemergency power supply
Including mechanical components
FI FI
E170 - Electrical schematic drawing Including cable list FI APElectric powersystem Z090 - Equipment list FI FI
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 23Standard for shipboard lifting appliances
DNV GL AS
Object Document type Additional description Shipboardcranes
Shipboardcranes(class
notation)
S011 - System diagram (PampID) FI AP
S042 - Hydraulic control diagram FI AP
Z060 - Functional description FI FI
Hydraulicpower system
Z090 - Equipment list FI FI
Control andmonitoring
I200 - Control and monitoring systemdocumentation
Functional description of safety systemand the safety equipment to be included FI AP
2122 For general requirements for documentation including definition of the Info codes see RU SHIP Pt1Ch3 Sec2
2123 For a full definition of the documentation types see RU SHIP Pt1 Ch3 Sec3
213 Design analysis
2131 For structural parts and components specified in [212] the drawings shall be supplemented withcalculations demonstrating that the structural strength complies with the requirements
2132 A complete listing of structural components and parts subjected to strength calculations shall besubmitted The list shall include information of
mdash types of failures considered (excessive yielding buckling fatigue fracture)mdash method of analysis performedmdash permissible stress or limit state method used
See also [43]
2133 The design calculations for hydraulic cylinders shall be based on the maximum obtainable pressure(safety valve setting) Alternatively if the maximum dynamic force applied on the crane is known this maybe used as basis for the design calculations In both cases different outreach positions shall be evaluated
22 Certification
221 Certificate requirements
2211 Certificates shall be issued as required by Table 2-2 for Shipboard cranesFor certificate definitions see [115] ldquoDefinitions Abbreviations Symbols and Referencesrdquo
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 24Standard for shipboard lifting appliances
DNV GL AS
Table 2-2 Certificate requirements for shipboard cranes
Object Certificatetype
Issued by Certification standard Additional description
Slewing bearings PC The Society 31 if maker is DNV GL approved
Hydraulic cylinders PC The Society Applicable also for accumulators
Sheaves PC Manufacturer Plastic sheaves to be deliveredwith the Societys TA and PC
Hoisting blocks PC The SocietyCG3 alternatively ILO form No3 issued by IACS class or FlagState administration
Hooks PC The SocietyCG3 alternatively ILO form No3 issued by IACS class or FlagState administration
Chains PC The SocietyCG3 alternatively ILO form No3 issued by IACS class or FlagState administration
Swivels PC The SocietyCG3 alternatively ILO form No3 issued by IACS class or FlagState administration
Shackles PC The SocietyCG3 alternatively ILO form No3 issued by IACS class or FlagState administration
Wire ropes PC The SocietyCG4 alternatively ILO form No4 issued by IACS class or FlagState administration
Winches PC The Society
Slewing gear PC Manufacturer Works product certificate
Transmission gearsand brakes PC Manufacturer
Works product certificateApplicable when transmittingbraking forces for hoisting andluffing For personnel handlingthe Societys PC required
Hydraulic components TR Manufacturer Except mountings
Unless otherwise specified the certification standard is this standard
PC = Product Certificate MC = Material Certificate TR = Test Report
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 25Standard for shipboard lifting appliances
DNV GL AS
Table 2-3 Additional certificate requirements for Crane notations
Object Certificatetype
Issued by Certification standard Additional description
Control amp monitoringsystem PC The Society
ELmotors with rating100 kW and above PC The Society
Motor starters andfrequency conver-terswith rating 100 kWand above
PC TA The SocietyThe Societys product certificatesor the Societys type approvalcertificate
Slip rings 100 kW andabove PC The Society
Unless otherwise specified the certification standard is this standard
PC = Product certificate TA = Type approval certificate MC = Material certificate TR = Test report
For general certification requirements see RU SHIP Pt1 Ch3 Sec4For a definition of the certification types see RU SHIP Pt1 Ch1 Sec4 and RU SHIP Pt1 Ch3 Sec5
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 26Standard for shipboard lifting appliances
DNV GL AS
SECTION 3 MATERIALS
31 General
311 This section contains provisions for the selection manufacture and testing as well as the specification of steelmaterials for various loading gear (including their foundations) and loose gear components They are basedon RU SHIP Pt2 Ch1 Sec1 [34]
312 Materials not covered by this section see list in [3215] are as far as possible to be dealt with inaccordance with the RU SHIP Pt2 according to recognized standards or by agreement
313 Suitable standardized steels which are not covered in Table 3-2 to Table 3-4 may also be used uponagreement with the Society
314 In the following the Societys rules stated in [311] are referred to as DNV GL rules for materials andwelding
32 Selection of materials
321 Selection criteria
3211 The selection of materials shall be carried out taking all material properties into consideration andthe Societys approval is normally effected by means of approved drawings
3212 When selecting materials of normal strength high strength and extra high strength steel for thevarious lifting appliances and loose gear components the following criteria shall be applied
mdash effect of the components on the mechanical strength of the assemblymdash type and magnitude of the load (static or dynamic loading internal stresses in the component stress
concentrations direction of the stress relative to the structure of the material)mdash design temperature (see [423])mdash chemical composition and weldabilitymdash mechanical properties of the material (dimensioning of components)mdash toughness of the material (resistance to brittle fracture at design temperature as verified by the notched-
bar impact test)mdash properties of the material perpendicular to the surface of the product (resistance to lamellar fracture)
It may be appropriate to apply further criteria to the selection of materials
3213 For shipboard lifting appliance application at temperatures below -10degC and in consideration of[423] steels shall be used which have sufficient toughness at these temperatures as verified by thenotched-bar impact test at the prescribed temperatureFor crane pedestals and crane pedestal sub-structures refer to rules RU SHIP Pt3 Ch1 Sec2 [354]
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 27Standard for shipboard lifting appliances
DNV GL AS
3214 If a component is subject to multi-axial stresses eg on greater material thicknessrsquo and largevolume welding connections steels with improved properties in the direction of thickness shall be selected
3215 Other materials such as stainless steels cast steel aluminium alloys timber or plastics shall bechosen and used in accordance with the criteria stated in [3212] and in consideration of their properties asand when applicable
322 Categorization of components
3221 Depending on their relevance to the overall safety of the structure components shall be allocated tothe following 3 categories see Table 3-1
3222 The categorization of components according to the criteria of Table 3-1 shall take place at the designstage and be submitted with the documents for approval
3223 Components not specifically mentioned in Table 3-1 shall be categorized in accordance with theloading conditions
323 Strength categories
3231 Materials for welded components shall be subdivided into the following strength categories on thebasis of their minimum yield strength
mdash normal strength materials with minimum yield strengths up to 265 Nmm2
mdash high strength materials with minimum yield strengths over 265 Nmm2 up to 420 Nmm2
mdash extra high strength materials with minimum yield strengths above 420 Nmm2
Table 3-1 Categorization of components into categories of order
Category of order Component description Component 1) (examples)
1st order
Components essential for the totalsafety of the structure as well asits safe operation and which whereapplicable are exposed to local oralso multi-axial stresses in addition toglobal stresses
mdash crane jibsmdash crane housesmdash crane columnsmdash foundationsmdash hydraulic cylinders for lifting gear and luffing gear as
well as for telescopic crane boomsmdash derrick heel bearing and rotary bearingmdash screws for slew ringsmdash load-bearing components of loose gearmdash axlesmdash winch drumsmdash winch frames
2nd order Components essential for safeoperation and functional capability
mdash hydraulic cylinders for slewing mechanismsmdash fittingsmdash lateral wind bracingsmdash rope-sheavesmdash hoisting eyes
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 28Standard for shipboard lifting appliances
DNV GL AS
Category of order Component description Component 1) (examples)
3rd order
Components subjected to low loads orof minor importance respectively andwhich cannot be allocated to the 1st or2nd category of order
mdash cabinsmdash stairsmdash platformsmdash reinforcementsmdash consoles
1) For fasteners such as bolts and screws the category of order of the joined components is applicable In case ofdiffering categories of the joined components the higher category shall be chosen
3232 The strength category selected for the component concerned or the material allocated to thiscategory shall be indicated in the documents for approval The same applies where the material is requiredto meet special conditionsWhen selecting materials it shall be borne in mind that a decline in the mechanical characteristics shall beexpected as the product thickness increases
33 Manufacture and testing
331 Requirements for materials and products3311 ManufacturingAll materials and products shall be manufactured in accordance with sufficiently tested procedures whichguarantee that the required properties are achieved
3312 Chemical composition and required propertiesAll materials and items manufactured from them which shall be categorized as 1st or 2nd order componentsaccording to Table 3-1 shall comply with the requirements given in this section or other applicable provisionswith respect to chemical composition and mechanical properties
3313 Supply condition and heat treatmentAll products shall be supplied in the required heat-treated condition Where the final heat treatment isonly carried out at the final manufacturer the supply condition of the pre-material shall be appropriatelydocumented in the test certificates
3314 Absence of defectsMaterials and products shall not show defects which may adversely affect the use or further processing of thematerial more than insignificantly
3315 WeldabilityMaterials intended for the manufacture of welded constructions shall be weldable in terms of applyingcustomary workshop procedures If welding is only possible under special conditions the conditions shall bedetermined in consultation with the Society and verified by a weldability test
332 Testing3321 Chemical compositionThe chemical composition of the materials shall be verified by the manufacturer by means of heat analysisand shall include all elements for which limit values are set in this section or in other applicable provisions orwhich are added on as alloys in order to achieve the required mechanical propertiesIn general the manufacturers analysis report is accepted as proof of the chemical composition
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 29Standard for shipboard lifting appliances
DNV GL AS
3322 Mechanical and technological properties
33221 When the mechanical and technological properties are tested the general procedures and testsamples shall be in accordance with RU SHIP Pt2 Ch1 Sec3 Test requirements and results shall bepresented in international (SI) units
3323 Dimensions and absence of defects
33231 All products shall be checked by the manufacturer for compliance with the prescribed dimensionssurveyed in respect of possible defects and if required presented to the Societys surveyorUnless specially agreed in the following sections the Societys surveyor will carry out a random examinationof the dimensions and the surface conditions as deemed necessary
33232 Where non-destructive tests are required for the various types of products they shall be performedby the manufacturer in accordance with DNVGL CG 0051The results as well as the particulars of the test procedure shall be evaluated in accordance with recognizedacceptance criteria and attested by a certificateProducts not complying with the requirements shall be set aside by the manufacturer
3324 Proof of mechanical properties
33241 The results of the required tests on materials and products of 1st and 2nd order components shallbe attested by a certificate according to RU SHIP Pt2 Ch1 Sec2 [423] eg inspection certificate 31 asper ISO10474 if not specified otherwise in this standard
33242 The material certificates of products for components of 1st and 2nd order shall include specificdetails on manufacturing method composition heat treatment mechanical properties and marking
33243 Materials and products for 3rd order components may be certified non-specifically by themanufacturer in accordance with RU SHIP Pt2 Ch1 Sec2 [424] eg test report 22 as per ISO 10474Corresponding equivalent certificates may be accepted
3325 RetestingWhere the certificates for materials or products are insufficient or their identification or correlation with thetest certificates is not properly possible the Society may ask for retests on the delivery under the SocietyrsquossupervisionType and scope of the tests will be determined case by case based on the rules for Materials
3326 Marking
33261 Materials and products shall be marked by the manufacturer in such a way that a properidentification on the basis of the material certificates can be madeMaterials and products which have been tested under the Societys supervision also receive test stampsaccording to RU SHIP Pt2 Ch1 Sec2 [41]
33262 Cast steel and forgings shall be marked with the manufacturers stamp an abbreviation for thecast type and a mark or code number for the melting charge (eg the last three digits of the melting chargenumber) Any additional markings are a matter of agreement between customer and manufacturer of thematerial
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 30Standard for shipboard lifting appliances
DNV GL AS
34 Materials for welded components
341 General noteThe following requirements apply to plates profiles bars and hollow sections which are intended for themanufacture of welded 1st and 2nd order loading gear and loose gear components
342 Selection of materials
3421 The criteria and provisions set out in [32] are applicable Steel materials shall comply with therequirements given in [343]
3422 Products made of aluminium or aluminium alloys shall comply with RU SHIP Pt2 Ch2 Sec10 or therequirements given in the relevant standards or approved material specifications respectively
3423 For design temperatures TE down to and including -10degC the normal strength high strength andextra high strength materials set out in the Table 3-2 Table 3-3 and Table 3-4 can be used taking intoconsideration the thickness-related requirements for the material toughness
Table 3-2 Suitable materials for welded components in strength category normal strength
Applicable product thickness fordesign temperatures down to 10degC
Components belonging to one of theorder categories set out in Table 3-1
Material group DNV GL rulesmaterial standard
Strength class or steelgrade respectively
1st order 2nd order 3rd order
VL-A le 125 mm le 25 mm
VL-B le 25 mm le 50 mm
VL-D le 50 mm over 50 mm
Normal strengthhull structural steels
RU SHIP Pt2 Ch2Sec2 [3]
VL-E over 50 mm
no particularprovisions
Table 3-3 Suitable materials of strength category high strength for welded components
Applicable product thickness fordesign temperatures down to -10degC
Components belonging to one of theorder categories set out in Table 3-1
Material group DNV GL rulesmaterial standard
Strength class or steelgrade respectively
1st order 2nd order 3rd order
VL-A27SVL-A32VL-A36VL-A40 le 25 mm le 50 mm
VL-D27SVL-D32VL-D36VL-D40 le 50 mm over 50 mmHigh strength hull
structural steelsRU SHIP Pt2 Ch2Sec2 [4]
VL-E27SVL-E32VL-E36VL-E40 over 50 mm
no particularprovisions
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 31Standard for shipboard lifting appliances
DNV GL AS
Applicable product thickness fordesign temperatures down to -10degC
Components belonging to one of theorder categories set out in Table 3-1
Material group DNV GL rulesmaterial standard
Strength class or steelgrade respectively
1st order 2nd order 3rd order
VL-F27SVL-F32VL-F36VL-F40 over 50 mm
Table 3-4 Suitable materials of strength category extra high strength for welded components
Applicable product thickness fordesign temperatures down to -10degC
Components belonging to one of theorder categories set out in Table 3-1
Material group DNV GL rulesmaterial standard
Strength class or steelgrade respectively
1st order 2nd order 3rd order
VL-A420 A460VL-A500 A550VL-
A620 A690le 25 mm le 50 mm
VL-D420 D460VL-D500 D550VL-
D620 D690le 50 mm le 70 mm
VL-E420 E460VL-E500 E550VL-
E620 E690le 70 mm
Extra high strengthsteels for weldedconstructionshullstructural steels
RU SHIP Pt2 Ch2Sec2 [5]
VL-F420 F460VL-F500 F550VL-
F620 F690le 70 mm
by specialagreement
Table 3-5 Percentage limits for the chemical composition of other normal strength and higherstrength carbon and carbon manganese steels
C Si Mn P S Cr Mo Cu Ni Al Other
022 055 160 004 004 030 008 030 040 008 1
1) Nb max 005 V max 010 Ti max 002
Nb + V + Ti max 012
343 Requirements for steel materials for welded components3431 Production methodThe steels shall be produced in accordance with a method approved by the Society The steels shall be fullykilled
3432 Chemical composition
34321 For normal strength and higher strength carbon and carbon-manganese steels the chemicalcomposition shall not exceed the maximum content given in Table 3-5 in the heat analysis
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 32Standard for shipboard lifting appliances
DNV GL AS
34322 For evaluation of the weldability or susceptibility to cold cracking respectively the carbonequivalent Caumlq or the Pcm-value shall be determined by the following equations
1
The values determined by the above equations shall not exceed the values given in Table 3-6
34323 For extra high strength or alloyed steels above strength class 460 the provisions of the Societysapproved material specifications apply
3433 Delivery condition and heat treatment
34331 For normal strength and high strength steels the provisions of RU SHIP Pt2 Ch2 Sec2 [33] or RUSHIP Pt2 Ch2 Sec2 [43] apply respectively
34332 Extra high strength steels shall be delivered in principle in a heat-treated condition or treated bya method approved by the Society eg thermo-mechanically formed according to RU SHIP Pt2 Ch2 Sec2[53]
34333 For austenitic stainless steels the provisions of RU SHIP Pt2 Ch2 Sec3 [4] apply
Table 3-6 Weldability requirements
Carbon equivalent []Strength category Strength class
general TM-rolledPcm []
Normal strength 235 045 by special agreement
275
315036
355 038High strength
390
045
040
420 048 045
460 053 046Extra high strength
over 460 by special agreement
by special agreement
3434 Mechanical properties
34341 The requirements given in RU SHIP Pt2 Ch2 Sec2 [34] RU SHIP Pt2 Ch2 Sec2 [44] and RUSHIP Pt2 Ch2 Sec2 [54] apply as well as the requirements given in the relevant standards or approvedmaterial specifications
34342 The requirements relating to tensile strength yield strength or 02 proof stress respectivelyelongation and reduction in area at fracture shall be verified by tests
1 Value for determining the preheating temperature and cold crack sensitivity
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 33Standard for shipboard lifting appliances
DNV GL AS
3435 Impact energy
34351 The requirements relating to impact energy depend on the category of order of the componentunder consideration see [322] the product thickness the yield strength and the design temperature Therequirements shall be determined in accordance with Table 3-7 and Table 3-8
34352 Material selection shall be made based on the material specification such that the requirementscan be met by it For design temperatures down to ndash10degC the applicable product thicknesses for normalstrength high strength and extra high strength materials are given in the Table 3-2 Table 3-3 and Table 3-4
34353 The requirements relating to impact energy of steels apply similarly to components which areunwelded tension-stressed notched or otherwise subjected to a 3-axial stress state and shall be verified asprescribed by tests with an ISO-V-specimen
3436 Characteristics in direction of thicknessWhere steel plates and wide flats are required to have enhanced properties in the direction of thickness RUSHIP Pt2 Ch2 Sec2 [6] shall be observed
3437 Test of surface finish and dimensions
34371 The requirements given in RU SHIP Pt2 Ch2 Sec2 [211] or the requirements given in therelevant standards or approved material specifications respectively applyCompliance with the requirements shall be confirmed by the manufacturer of the material
34372 The manufacturer shall check the products with respect to their external finish and dimensionsSurface defects may be removed mechanically weld repairs are not permitted
3438 Non-destructive tests (de-lamination proof)
34381 Plates and wide flats with enhanced properties in the direction of thickness shall be subjectedto an ultra-sonic test They shall meet the requirements for Test Class 2 laid down in the Stahl-Eisen-Lieferbedingungen 072 or of Test Class S2E3 according to EN 10160The test width of the rim zone depends on the product thickness but should have a minimum width of 50mm
34382 Flats products with a product thickness of t ge 15 mm which are used for the manufacture ofconnection flanges and rings for 1st order components shall undergo an ultrasonic surface test They shallmeet the requirements for Test Class 2 laid down in the Stahl-Eisen-Lieferbedingungen 072 or of Test ClassS2 in accordance with EN 10160 The test grid used shall not exceed 100 mm
34383 Connection flanges and rings made of flat products with a product thickness t ge 40 mm shallundergo a non-destructive test according to [3636]
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 34Standard for shipboard lifting appliances
DNV GL AS
344 Proof of mechanical properties of pipesThe mechanical properties of pipes shall be certified in accordance with [3334]
Table 3-7 Requirements for impact energy
Impact energy KV 1) [J] minStrength category Strength class
Longitudinal Transverse
Normal strength 235 27 20
275 29 21
315 31 22
355 34 24High strength
390 41 27
420 42 28
460 46 31
500 50 33
550 55 37
620 62 41
Extra high strength 2)
over 690 69 46
1) Mean value for 3 specimens There may be one lower value but not less than 70 of the mean value2) Up to 70 mm thickness larger thicknesses upon special agreement
Table 3-8 Test temperatures for the notched bar impact test (welded components)
Test temperature Tp [degC]
Components belonging to one of the order categories set out in Table 3-1Product thickness t [mm]
1st order 2nd order 3rd order
t le 125 Tp = TE + 30 2) minus 1)
125 lt t le 25 Tp = TE + 10 Tp = TE + 30
25 lt t le 50 Tp = TE ndash 10 Tp = TE + 10
50 lt t le 70 Tp = TE ndash 20 Tp = TE + 10
over 70 Tp = TE ndash 30 3) Tp = TE ndash 10
No special provisions 1)
1) The requirements given in RU SHIP Pt2 Ch2 or in the relevant standards or approved material specifications apply2) TE = design temperature3) Generally test temperatures below -60degC are not required (-50degC for δy le 355 Nmm2)
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 35Standard for shipboard lifting appliances
DNV GL AS
Table 3-9 Test temperatures for the notched bar impact test (non-welded components 1- or 2-axial stress state)
Test temperature Tp [degC]
Components belonging to one of the order categories set out in Table 3-1Product thickness t [mm]
1st order 2nd order 3rd order
t le 125 minus 1)
125 lt t le 25 Tp = TE + 20 2)
25 lt t le 50 Tp = TE + 10
50 lt t le 70 Tp = TE + 10
over 70 Tp = TE ndash 10
No special provisions 1) No special provisions 1)
1) The requirements given in RU SHIP Pt2 Ch2 or in the relevant standards or approved material specifications apply2) TE = design temperature
35 Materials for hydraulic cylinders
351 General notes
3511 The following provisions apply to pipes intended for the manufacture of cylinder jackets of 1st and2nd order hydraulic cylinders
3512 Where cylinder jackets are manufactured from flat products by rolling and fusion welding therequirements given in this section apply as and where relevant to the basic material In addition the DNV GLrules for welding shall be observed
352 Selection of materials
3521 For the selection of material the selection cri-teria and provisions laid down in [32] apply Theselected materials shall comply with the requirements given in [353]
3522 Special steels or pipes manufactured by cold rolling shall comply with a material specificationapproved by the Society
353 Requirements3531 Chemical composition
35311 For the manufacture of welded hydraulic cylinders carbon and carbon-manganese steels shallpreferably be used the chemical composition of which complies with the limit values set out in [3432] Thecarbon equivalent Ceq shall not exceed 045
35312 The requirements given in RU SHIP Pt2 Ch2 Sec5 [17] or RU SHIP Pt2 Ch2 Sec5 [4] applyrespectively
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 36Standard for shipboard lifting appliances
DNV GL AS
35313 Compliance with the requirements shall be verified by the material manufacturer Where the basematerial is not molten at the pipe manufacturer the manufacturers heat analysis of the base material can beaccepted For special steels the properties stated in the approved specifications apply
3532 Delivery condition and heat treatment
35321 For welded hydraulic cylinders the provisions of RU SHIP Pt2 Ch2 Sec5 [18] or RU SHIP Pt2Ch2 Sec5 [4] apply
35322 For hydraulic cylinders which are not produced by welding cold-rolled pipes can be used up to awall thickness of 15 mm and design temperatures down to and including ndash10 C if the requirements relatingto impact energy set out in [3535] are achieved and elongation A is 15 as a minimum
3533 Mechanical properties
35331 The requirements given in RU SHIP Pt2 Ch2 Sec5 [19] or RU SHIP Pt2 Ch2 Sec5 [4] of therequirements given in the relevant standards or approved material specifications apply respectively
35332 The requirements relating to tensile strength yield strength or 02 proof stress respectivelyelongation and reduction in area at fracture shall be verified by tests
3534 Technological test
35341 Pipes with longitudinal weld seams and seamless pipes of UTS = 490 Nmm2 shall undergo one ofthe ring test examinations specified in RU SHIP Pt2 Ch1 Sec3 [35]
35342 In the case of fusion-welded pipes with an outer diameter over 200 mm a weld seam bend test inaccordance with RU SHIP Pt2 Ch1 Sec3 [33] shall be carried out applying a bending mandrel diameter of3 times wall thickness t
3535 Impact energy
35351 The requirements relating to impact energy depend on the order category of the component underconsideration see [322] the product thickness and the design temperature and shall be verified by ISO-Vspecimen tests
35352 For product thicknesses up to and including 25 mm RU SHIP Pt2 Ch2 apply or the requirementsgiven in the other applicable standards or approved material specifications
35353 Unless otherwise specified the materials used shall have an impact energy of 41 J (longitudinalspecimen) or 27 J (transverse specimen) at a test temperature as per Table 3-10
35354 For pipes manufactured by hot rolling up to a product thickness of 10 mm the impact energy testmay be dispensed with Below 6 mm an impact energy test is not generally required
3536 Test of surface finish and dimensions
35361 The requirements given in RU SHIP Pt2 Ch2 Sec5 [111] and the requirements given in therelevant standards or approved material specifications respectively applyCompliance with the requirements shall be confirmed by the manufacturer of the material
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 37Standard for shipboard lifting appliances
DNV GL AS
Table 3-10 Test temperatures for the notched bar impact test (hydraulic cylinders)
Test temperature Tp [degC]
Order categories of componentsProduct thickness t [mm]
1st order 2nd order
t le 25 Tp = TE +30 2) minus 1)
25 lt t le 50 Tp = TE ndash 10 Tp = TE +30
50 lt t le 70 Tp = TE ndash 20 Tp = TE ndash 10
over 70 Tp = TE ndash 30 3) Tp = TE ndash 10
1) The requirements given in RU SHIP Pt2 Ch2 Sec5 or the requirements given in the other applicable standards orapproved material specifications apply
2) TE = design temperature3) Generally test temperatures below -60degC are not required (-50degC for δy le 355 Nmm2)
35362 The manufacturer shall check the products with respect to their external finish and dimensionalproperties Weld repairs are not allowed
3537 Non-destructive testAll pipes shall be subjected to non-destructive tests along their total length The success of the test shall beconfirmed by the manufacturer
3538 Tightness testAll pipes shall be tested for leaks by the manufacturer The success of the test shall be confirmed by themanufacturer
354 Proof of mechanical properties
3541 Mechanical properties of pipes shall be certified in accordance with [3334]
3542 Based on a special approval diverging from [33341] proof of mechanical properties of 1st orderhydraulic cylinders may also be furnished by certifying in accordance with RU SHIP Pt2 Ch1 Sec2 [423] W(works) Certificate eg inspection certificate 31 as per ISO 10474
36 Forgings
361 General notes
3611 The provisions of this section apply to steel forgings and rolled or forged slewing rings as well as forrolled or forged bars for piston rods of hydraulic cylinders The slewing rings shall conform to a specificationapproved by the Society
3612 For rolled or forged bars for the manufacture of bolts and nuts with proof of mechanical propertiesthe requirements given in [38] apply
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 38Standard for shipboard lifting appliances
DNV GL AS
362 Selection of materialsFor the selection of materials the selection criteria and provisions stated in [32] apply Accordingly slewingrings are considered to be 1st order componentsThe selected materials shall comply with the following requirements
363 Requirements3631 Chemical composition
36311 The requirements given in RU SHIP Pt2 Ch2 Sec6 applyFor special steels and slewing rings the properties in the approved specifications apply
36312 Where forgings shall be used in welded structures preference shall be given to carbon and carbon-manganese steels whose chemical composition meets the limit values stated in [3432] The carbonequivalent Ceq thereof shall not exceed 045
36313 Compliance with the requirements shall be verified by the manufacturer of the material Where thebase material is not molten at the forge shop the manufacturers heat analysis of the base material can beaccepted
3632 Delivery condition and heat treatmentThe provisions of RU SHIP Pt2 Ch2 Sec6 apply
3633 Mechanical properties
36331 The requirements given in RU SHIP Pt2 Ch2 and the requirements given in the other relevantstandards or approved material specifications apply respectively
36332 The requirements relating to tensile strength yield strength or 02 proof stress respectivelyelongation and reduction in area at fracture shall be verified by tests
3634 Impact energy
36341 For design temperatures down to and including -10degC the requirements given in RU SHIP Pt2 Ch2Sec6 and the requirements given in the other relevant standards or approved material specifications applyrespectively
36342 Unless otherwise specified for design temperatures below -10degC the requirements given in Table3-11 apply
36343 The requirements related to impact energy shall be verified by tests with ISO-V specimens
Table 3-11 Impact energy requirements for forgings with design temperatures below -10degC
Minimum impact energyKV 1) [J]Components belonging to one of theorder categories set out in Table 3-1 longitudinal transverse
Test temperatureTP [degC]
1st order 41 (29) 27 (19) TE ndash 10 2)
2nd order 41 (29) 27 (19) TE + 10
3rd order No special requirements 3)
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 39Standard for shipboard lifting appliances
DNV GL AS
Minimum impact energyKV 1) [J]Components belonging to one of theorder categories set out in Table 3-1 longitudinal transverse
Test temperatureTP [degC]
1) Mean value for 3 specimens One individual value may be below the mean value but not less than the individualvalues given in brackets
2) TE = design temperature3) The requirements given in RU SHIP Pt2 Ch2 Sec6 or the requirements given in the other applicable standards or
approved material specifications apply
3635 Test of surface finish and dimensions
36351 The manufacturer shall check the forgings at every stage of the process with respect to theirexternal finish and dimensional properties Forging defects shall be eliminated if they are not removed by thesubsequent mechanical treatment Weld repairs are not permitted
3636 Non-destructive test
36361 Forged or rolled rings shall be subjected to an ultrasonic test by the manufacturer and whereapplicable also to a surface crack test The tests shall be carried out in accordance with RU SHIP Pt2 Ch2Sec6
36362 The results of the non-destructive tests shall be documented by the manufacturer The test reportsshall be presented to a the Societys surveyor
364 Proof of mechanical propertiesThe mechanical properties of forgings shall be certified in accordance with [3334] Diverging from thisproof of the mechanical properties of slewing rings of ships cranes of groups A or B and of bars for pistonrods may be attested by a certificate in accordance with RU SHIP Pt2 Ch1 Sec2 [423] W (works)Certificate eg inspection certificate 31 as per ISO 10474
37 Steel castings
371 General notesThe provisions in this section apply to steel castings for use in welded constructions
372 Selection of materialsFor the selection of materials the selection criteria and provisions stated in [32] apply The selectedmaterials shall comply with the following requirements
373 Requirements3731 Chemical composition
37311 The requirements given in RU SHIP Pt2 Ch2 Sec8 applyCompliance with the requirements shall be verified by the manufacturer of the material by means of heatanalyses
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 40Standard for shipboard lifting appliances
DNV GL AS
37312 Where steel castings shall be used in welded structures preference shall be given to carbon andcarbon-manganese steels whose chemical composition meets the limit values stated in [3432] The carbonequivalent Ceq thereof shall not exceed 045
37313 For alloyed steel castings the properties stated in the approved specifications apply
3732 Delivery condition and heat treatmentThe requirements given in RU SHIP Pt2 Ch2 Sec8 apply
3733 Mechanical properties
37331 The requirements given in RU SHIP Pt2 Ch2 Sec8 and the requirements given in the otherrelevant standards or approved material specifications apply respectively
37332 The requirements relating to tensile strength yield strength or 02 proof stress respectivelyelongation and reduction in area at fracture shall be verified by tests
3734 Impact energy
37341 For design temperatures down to and in-cluding -10degC the requirements given in RU SHIP Pt2Ch2 Sec8 and the requirements given in the other relevant standards or approved material specificationsapply respectively
37342 For design temperatures below ndash10degC the requirements given in Table 3-12 apply unless otherwisespecified
37343 The requirements related to impact energy shall be verified by tests with ISO-V specimens
3735 Test of surface finish and dimensions
37351 The manufacturer shall check the steel castings with respect to their external finish anddimensional properties Casting defects shall be eliminated if they are not removed by the subsequentmechanical treatment RU SHIP Pt2 Ch2 Sec8 shall be observedRepair of defects by means of welding requires approval by the Society
3736 Non-destructive testSteel castings for 1st order components shall be subjected to an ultrasonic test by the manufacturer andwhere applicable also to a surface crack testThe tests shall be carried out in accordance with RU SHIP Pt2 Ch2 Sec8 The test reports shall bepresented to a the Societys surveyor during the inspection of the steel castings
374 Proof of mechanical propertiesThe mechanical properties of the steel castings shall be certified in accordance with [3334]
Table 3-12 Impact energy requirements for steel castings for design temperatures below -10degC
Components belonging to one of theorder categories set out in Table 3-1 Minimum impact energyKV 1)[J] Test temperatureTP [degC]
1st order 27 (19) TE ndash 10 2)
2nd order 27 (19) TE + 10
3rd order no special requirements 3)
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 41Standard for shipboard lifting appliances
DNV GL AS
Components belonging to one of theorder categories set out in Table 3-1 Minimum impact energyKV 1)[J] Test temperatureTP [degC]
1) Mean value for 3 specimens One individual value may be below the mean value but not less than the individualvalues given in brackets
2) TE = design temperature3) The requirements given in RU SHIP Pt2 Ch2 Sec8 or the requirements given in the other applicable standards or
approved material specifications apply
38 Bolts and nuts
381 General noteThe provisions of this section apply to bolts and nuts and to non-alloyed and alloyed steel bars used in theirmanufacture The scope includes all bolts and nuts with nominal tensile strengths of gt 600 Nmm2 for whicha quality certificate is required
382 Manufacture
3821 Bolts and nuts can be produced by hot or cold forming or by machining Hot-formed and cold-formed bolts and nuts shall undergo heat treatment
3822 Heat treatment can be dispensed with in the case of hot-formed bolts and nuts made of non-alloyedsteels if they shall be used at normal ambient temperatures in accordance with Table 3-13 and a uniformstructure is brought about by the hot-forming process
383 Requirements
3831 Bolts and nuts shall comply with the requirements given in RU SHIP Pt2 Ch2 Sec6 [92] or with therequirements given in recognized standards
3832 Notwithstanding [3831] machining steels with enhanced S- P- or Pb contents may be usedfor bolts and nuts provided that no requirements relating to heat resistance or impact strength at lowtemperatures exist
3833 Chemical compositionFor the chemical composition the requirements given in RU SHIP Pt2 Ch2 Sec6 [94] apply In additionthe carbon content of the steels shall not exceed 055 as established by product analysis
3834 Elongation at fractureThe elongation at fracture A shall conform to the characteristic values for the strength class or steel grade Itshall in any case not be less than 8 for ferritic steels or 30 for austenitic steels
3835 Impact energyThe impact energy shall conform to the characteristic values of the steel grade but shall at a minimummeet the requirements given in Table 3-13
3836 Expansion (of nuts)The expansion of ferritic steel nuts shall be at least 4 with non-machining forming processes and atleast 5 with machining methods The expansion requirements for austenitic steel nuts shall be speciallyspecified Proof of expansion is subject to random tests
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 42Standard for shipboard lifting appliances
DNV GL AS
3837 Non-destructive testBolts used for the assembly of 1st order components shall be subjected to a crack test by the manufacturerThe results of the non-destructive tests shall be documented by the manufacturer
384 Proof of mechanical propertiesThe mechanical properties of bolts and nuts shall be certified in accordance with [3334]
Table 3-13 Impact energy requirements for bolts and nuts
Minimum impact energyService or designtemperature 1)
Steel grade or nominaltensile strength KV [J] KU [J]
Test temperatureTp [degC]
lt 800 Nmm2 32 30
ge 800 Nmm2 32 30
ge 1000 Nmm2 25 25Ferritic
ge 1200 Nmm2 18 20
-10degC
Austenitic 41 minus
Alloyed and tempered 41 minus
Non-alloyed 41 minus
+20degC
Below -10degC to -55degC All 41 minus 10degC below lowestdesign temperature
1) At increased temp gt +50degC
Alloyed and tempered KV 52 J ndash Tp +20degC
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 43Standard for shipboard lifting appliances
DNV GL AS
SECTION 4 DESIGN AND CALCULATION PRINCIPLES
41 General
411 This section contains provisions of general validity governing the design and calculation of lifting applianceson seagoing shipsThe special provisions contained in the following sections of this standard shall be observed additionally orwith priority respectively
412 Calculations according to established calculation principles or standards eg according to EN 13001 or EN13852 may be accepted if the particular properties of seagoing ships as stated in these rules have beentaken into consideration
42 Design principles
421 General notes4211 Prerequisites for the design
42111 Determination and specification of the operating and seagoing conditions on which the designis based are in principle the responsibility of the customer and the manufacturer The shipyard shall beconsulted as well The specifications decided upon are of considerable importance for the reliable operationand expected service life
42112 The intended use of ships and lifting appliances the shipping routes and the operational area highship speeds and the shape of the ships hull shall be considered as required
4212 Design criteria for operating lifting appliancesEssential design criteria in addition to the statements in [422] to [425] are in particular
mdash the total service life ie the number of loading cycles within the expected service lifemdash the loading condition ie the relative or percentage frequency at which the various hoist loads are
reached or exceeded in the total service lifemdash the type of service eg handling containers general or palletized cargo grabs or provision under harbour
or sea conditions
4213 Design criteria for the status out of operation
42131 Essential criteria for the design are in relation to [4212] increased inclinations of the supportingstructure and increased wind loads as well as ship accelerations
42132 In particular cases loads caused by vibrations shall be considered which may be generated eg byship machinery or seagoing influences
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DNV GL AS
422 Environmental conditions
4221 Special attention shall be given to the operation site weather conditions humidity dust aggressivemedia oil and salt-bearing air exhaust gases and exhaust gas heat vibrations etc if known or specified bycontract
4222 Machinery and electrical installations shall be dimensioned with respect to temperature and humidityat least for the following limit values if no stricter limit values are specified
a) in enclosed spaces
mdash air temperature 0degC to +45degCmdash relative air humidity 80
b) on the open deck
mdash air temperature
mdash lifting appliances in operation -10degC to +45degCmdash lifting appliances out of operation -25degC to +45degC
mdash relative air humidity 80 and influence of salt spray
4223 Vibrations are in general not part of dimensioning of the shipboard lifting appliances Whereshipboard lifting appliances are prone to vibrations vibration analyses shall be performed
4224 Where necessary manufacturer ship yard or operator shall specify the environmental conditions inparticular
423 Design temperature4231 Definitions
42311 The design temperature is the mean value of the lowest daily average temperature in theoperational area of a lifting appliance The definitions of [42312] to [42314] apply
42312 The daily average temperature is the mean value of day and night temperature
42313 The lowest daily average temperature is the lowest value of daily average temperature measuredduring one yearWhere the duration of operation is limited with respect to seasons of the year the lowest value of dailyaverage temperature measured during the period of operation shall be used
42314 The mean value of the lowest daily average temperature is the statistical mean value measuredduring an observation period of at least 20 years
4232 Application
42321 The design temperature of shipboard lifting appliances not operated in closed heatedcompartments shall be at least ndash10degC
42322 Where the design temperature is specified below ndash10degC this shall be explicitly stated by theshipyard or the manufacturer of the lifting appliance in the drawings or in other documents submitted to theSociety for approval It also shall be considered with respect to material selection and processing (welding)as well as with respect to dimensioning of systems sensitive to low temperatures
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 45Standard for shipboard lifting appliances
DNV GL AS
42323 The lowest applicable design temperature shall not be below ndash30degC
42324 In extreme cases shipboard lifting appliances may be operated at an environmental temperaturewhich is lower than design temperature In this case the following conditions shall be complied with
a) The environmental temperature shall not be less than 20degC below design temperatureb) The number nlow of the lifting operations at low temperatures is yearly to be limited as follows
nlow le N 1000
N = total number of all lifting operations in the expected life time for the lifting appliance (to betaken from load assumptions of the fatigue analysis)
If the fatigue analysis for a lifting appliance could be dispensed with then the number of liftingoperations at low temperatures shall be limited to nlow le 20 per year
c) The manufacturer of the lifting appliance shall agree on the low temperature Where necessary thesusceptibility of certain components to low temperatures |shall be considered
424 Load assumptions4241 General notes
42411 Shipboard lifting appliances are subject to other and partly greater loads than lifting appliancesonshore This includes amongst others ship inclinations seagoing accelerations as well as increased windloads
42412 For the design in principle all loads shall be considered which act upon the lifting appliance ldquoinoperationrdquo and in the out of operation state
42413 The design as well as the calculation and dimensioning of all shipboard lifting appliances shall bebased on the following load assumptions if applicable
42414 The following sections of this standard may contain further load assumptions which are then to beobserved additionally or given preference where applicable for the lifting appliance under consideration
42415 Where shipboard lifting appliances are exposed to special loads which are not stated in thisstandard then these shall be taken as a basis for design and dimensioningSpecial loads shall be indicated expressly by the shipyard or manufacturer of the lifting appliance in thedrawings or in other documents submitted to the Society for approval Regarding the proof according to[438] the partial safety factor to be considered shall be agreed with the Society
4242 Dead loads
42421 Dead loads according to [41512] shall be calculated using recognized standards such as eg EN1991-1-1 or shall be determined by weighing
42422 Dead loads are calculated by multiplying the mass by the acceleration of gravity g = 981 mssup2
4243 Dynamic forces
42431 Dynamic forces due to drives424311 The acceleration of lifting appliance components andor useful loads due to drives generatespositive or negative dynamic forces depending on definition which shall be calculated as follows
force [N] = mass [kg] acceleration [ms2]
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 46Standard for shipboard lifting appliances
DNV GL AS
424312 Braking forces due to drives shall be assumed as negative dynamic forces424313 Dynamic forces due to drives may normally be assumed as quasi-static loads They are specifiedin [5324] as dimensioning loads
42432 Seagoing dynamic forces424321 Horizontal dynamic forces due to motions of a floating body shall be considered for shipboardlifting appliances used in occasional sea operations in accordance with the method described in [5325]424322 Vertical dynamic forces due to motions of a floating body shall be considered if the calculation ismade in according with [53251] If AppA is applied they are included in the method used therein if Table5-2 is applied they may be ignored424323 Seagoing dynamic forces may be assumed as quasi-static loads
4244 Inclinations of the supporting structure
42441 Lifting appliances in operation424411 Lifting appliances shall be dimensioned for operation at the static minimum inclinationsaccording to Table 4-1Exceptions from this provision are defined in [24416]424412 Dynamic loads due to motions of the supporting structure shall be considered in according with[5325]
424413 Static inclinations α (= heel) and β (= trim) shall be assumed to be acting simultaneously424414 Simplifying it may be assumed that heel and trim are superimposed as follows
ε
The resulting angle ε shall be assumed to have the most unfavourable direction
Table 4-1 Static minimum inclinations
Static minimum inclinationType of floating body
Heel angle α Trim angle β
Ships and vessels having ship-shape properties plusmn 5deg plusmn 2deg
Barges of length less than 4 times breadth andcatamarans plusmn 3deg plusmn 2deg
Floating docks plusmn 2deg plusmn 2deg
Semi-submersibles plusmn 3deg plusmn 3deg
424415 The values of Table 4-1 assume sufficient stability of the floating body Where larger inclinationsshall be expected during operation of the lifting appliance then these shall be taken as the basis424416 In special cases to be proven by measurements or calculations the values may be lower thanthose in Table 4-1For dimensioning the inclinations which are determined shall be increased by 1deg heel and 05deg trim
42442 Lifting appliances out of operation424421 For the calculation of dynamic forces in the out of operation state the dynamic inclinations aswell as the respective accelerations of the floating body shall be observedFor this purpose the dynamic inclinations of the floating body according to Table 4-1 shall be assumed424422 Simplifying the calculation of dynamic forces may be performed according to AppA
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 47Standard for shipboard lifting appliances
DNV GL AS
4245 Wind loads
42451 General notes424511 Shipboard lifting appliances shall in general only be operated up to a mean wind speed ofapproximately 80 of the dimensioning wind speedAt higher wind speeds the loading gear shall be taken out of operation and to be stowed in the stowingposition424512 Simplifying the statements in [42452] and [42453] are based on a constant mean windspeed acting in any assumed direction and height424513 Static or dynamic calculations of wind loads in accordance with recognized rules or standards orcalculations with suitable wind load parameters may be accepted by the Society
42452 Calculation of wind loadThe wind load LW acting on a structure shall be assumed to have the most unfavourable direction and shallbe calculated using the following formula
[N]
q = v216 [Nm2] (dynamic pressure)v = wind speed according to [42453] [ms]cf = form coefficient according to [42454] [-]Aw = wind area [m2]
42453 Wind speeds424531 The determination of wind load shall be based on the wind speeds according to Table 4-2
Table 4-2 Wind speeds
Wind speedMode of operation of the lifting appliance
in operation out of operation
Shipboard lifting appliances harbour operation 20 ms 50 ms 1
Shipboard lifting appliances sea operation 25 ms 50 ms 1
1) Not to apply for topped cranes
424532 For topped shipboard lifting appliances out of operation the wind speed shall be calculated as afunction of height according to the following formula
hL = height of the centre of area of the boom above waterline [m]
424533 The wind speed v is assumed to be constant along the height
424534 Floating cranes shall be treated like shipboard lifting appliances
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 48Standard for shipboard lifting appliances
DNV GL AS
42454 Form coefficientsThe form coefficients may be determined according to AppC or simplified as follows
cf = 16 for rolled profiles and box girderscf = 13 for rectangular areas of closed super structures like eg engine housescf = 12 for cylindrical structural elements
42455 Wind areas located behind one anotherThe wind loads of areas located behind one another may be determined according to AppC or simplified asfollowsFor wind loads of areas located behind one another the wind load of the respective area lying behind may beassumed to be 75 of the area lying in front From the 9th area onwards the wind load remains constant at10
42456 Wind load on the useful load424561 The wind load acting on the useful load shall be calculated according to [42452] based onthe largest wind area of the useful load and acting in the most unfavourable direction
424562 Where a more precise information on the useful load is not available the wind load may becalculated using the following values for cf ∙ Aw
LN = useful load [t]
4246 Snow and ice loads
42461 The manufacturer has to specify by agreement with the client if and to what extent snow and iceloads shall be considered for individual operating conditions Generally lifting appliances with ice accretionshall not be operated
42462 Where ice accretion shall be considered and no empiric or specified values are available simplifieda general ice accretion of 3 cm thickness may be assumed for all parts of the construction which are exposedto the weather conditions
42463 The specific weight of the ice is assumed to be 700 kgm3 The specific weight of snow is assumedto be 200 kgm3
42464 In the case of ice load the wind load shall be related to the area increased by ice accretion
4247 Loads due to temperatureParts of the structure or other structural elements which cannot expand or contract freely shall be avoided ifpossible Otherwise the lower and upper temperature shall be agreed with the Society and the temperatureloads shall be considered in the calculated strength analyses
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 49Standard for shipboard lifting appliances
DNV GL AS
425 Special provisions4251 Conveyance of persons in the harbourThe following provisions imply safety devices which are required in principle in [99] and Sec13 such as eg
mdash emergency shut-down switches or buttonsmdash control elements return automatically to the neutral positionmdash load and load moment reducing motions when safety devices apply
42511 The nominal load (LNe) of shipboard lifting appliances for the conveyance of persons shall be atleast twice the sum of the dead load and nominal load for the means of conveyance of persons used
42512 The maximum lowering and hoisting speed for the conveyance of persons shall not exceed 05 msThe control system shall be capable of observing this speed limitation
42513 At a lowering speed of more than 03 ms the control system shall be capable of setting-downgently the means of conveying persons
42514 The minimum lowering and hoisting speed for the conveyance of persons shall not be less than005 ms
42515 Means of conveying persons shall be attached to the loading gear by secured shackles or otherapproved fixed connections Cargo hooks with seawater-resistant safety latch are permitted if compatiblewith the master link of the meansAutomatically release hooks for life-saving appliances are also not permissible
42516 Hoisting and luffing winches of shipboard lifting appliances for conveying persons shall be equippedwith a mechanical second brake The second brake shall be independent of the primary brake
42517 If hydraulic cylinders are used for luffing knuckling or telescoping of a boom they shall beequipped with hydraulic restriction systems Alternatively two independent hydraulic cylinders can be usedof which each single one shall be capable to hold the nominal load resulting from the conveyance of persons(SWL (M)) if the other hydraulic cylinder failsSafety against failure shall then be verified for loading condition III5 as per [552]
42518 Special devices shall be provided to rescue passengers from a means of conveying persons in caseof the failure of the drive
4252 Conveyance of personnel at seaFor the conveyance of personnel at sea the provisions of [4251] apply with the exception of [42512]and [42513] In addition the following provisions shall be observed
42521 Aside from an emergency the following environmental conditions shall be adhered to unlessdeviating conditions are agreed upon
mdash average wind speed le 10 msmdash significant wave height le 2 mmdash visibility conditions daylight or sufficient illumination
42522 Shipboard lifting appliances for occasional operations at sea shall be equipped with a manualswitch which allows switching between normal operation and conveyance of personnel if provided for theconveyance of personnel
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 50Standard for shipboard lifting appliances
DNV GL AS
42523 Shipboard lifting appliances according to [42522] shall comply with the following conditions inthe conveyance of personnel mode if applicable
mdash automatic de-activation of safety systems for release of the cargo runner (emergency system for hookingon of cargo hooks)
mdash automatic de-activation of active or passive heave compensatorrsquos These are however permissible for thehandling of work boats if they are adjusted to these boats
mdash in addition to the main power supply an emergency power supply shall be available to ensure mainfunctions of the lifting appliance (lifting luffing slewing telescoping and knuckling) at a minimum speedof 10 of the nominal operational speed in the mode conveyance of personnel Exceptions (eg verylarge cranes) are individually to be agreed with the Society
4253 Sea lashing
42531 All mobile parts of shipboard lifting appliances such as derricks crane booms trolleys gantriesetc shall have a special park and stowage position where they can be lashed to be seaworthyExceptions like eg free hanging or topped booms require approval by the Society case by case
42532 Special stowage positions shall be provided for mobile lifting appliances They shall be selectedsuch that the prospective loads like eg ship accelerations wind and wash are minimized
42533 The lifting appliances as well as their support and lashing devices shall be sufficiently dimensionedfor the loads in the out of operation state
43 Calculation principles
431 Basic requirements
4311 All strength analyses shall correspond to generally recognized rules of statics dynamics and strengthof materials
4312 Details on system measurements sections materials used etc in the drawings shall agree with thecorresponding calculations
4313 Mobile loads shall be assumed in the most unfavourable positions for the structural elementconsidered
4314 Where non-linear relations inherent to the system exist between loads and stresses the stressdetermination shall be performed according to the 2nd order theory for γpfold loads with consideration ofdeformations
4315 Calculations according to 2nd order theory shall be based on a reduced value for dimensioning theYoungs modulus
Ed = Ek γm
Ed = dimensioning value of Youngs modulusEk = significant value of the Youngs modulusγm = partial safety factor for resistance values according to [43743]
Explanations on this can be found in [4371] and [4372]
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 51Standard for shipboard lifting appliances
DNV GL AS
432 Proofs required
4321 Normally the following proofs shall be submitted for all lifting appliances
mdash proof of structural safety according to [44]mdash proof of stability according to [45]mdash proof of fatigue strength according to [46]mdash proof of suitability for use according to [47]
4322 The following sections of this standard may contain more detailed andor additional information onproofs required for the lifting appliance considered there
433 Materials4331 General notes
43311 The materials intended for use shall be indicated in the calculation
43312 Table 3-2 to Table3-4 show a selection of steels generally approved by the Society for plates andprofilesOther steels may be approved
43313 Regarding the materials for machinery elements axes shafts bolts etc as well as for non-ferrousmetals the DNV GL rules for materials apply
43314 Regarding bolts and nuts the provisions in Sec3 [38] apply
4332 Calculated yield strength
43321 General notes433211 The strength analyses according to this standard refer as a failure criterium to the yield strengthof the material433212 For metallic materials without significant yield strength ReH the yield strength Rp02 is usedinstead433213 To avoid brittle fracture the materials used shall be sufficiently ductileThis means that the failure of a structural element due to overload may possibly be indicated sooner by largeplastic deformations433214 For less ductile materials with a small ratio of tensile strength Rm over yield strength ReHadditional safety against reaching or exceeding the tensile strength is stipulatedThis is achieved in strength analyses by taking into consideration a reduced value for the yield strength ndash thecalculated yield strength fyr
43322 Steels433221 The calculated yield strength fyr is determined as follows
fyr = 083 ∙ Rm le ReH (or le Rp 02)
Rm = tensile strength [Nmm2]ReH = yield strength [Nmm2]Rp02 = 02-yield strength [Nmm2]
433222 Where austenitic steels are used with a ratio Rp02Rm le 05 subject to special approval by theSociety for dimensioning the 1-yield strength Rp10 may by applied instead of Rp02
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 52Standard for shipboard lifting appliances
DNV GL AS
43323 Aluminium alloys433231 If aluminium alloys suitable for seawater stated in the DNV GL rules for materials are used theyield strength is calculated as follows
fyr = 037 ∙ (Rp 02 + Rm) le Rp 02
Rm = tensile strength [Nmmsup2]Rp02 = 02-yield strength [Nmmsup2]
433232 In the case of welded connections the respective mechanical properties in the welded conditionshall be assumed If these values are not available the corresponding values in the soft condition shall beassumed
434 4341 Hole weakening by bolts
43411 The sections to be considered are the net sections (including hole deduction) for all structuralelements stressed by tension
43412 A calculated deduction due to holes may be dispensed with for all sections stressed by pressure andshear if
mdash the maximum hole clearance is 1 mm andmdash the deformations of the structure shall not be limited
43413 Where the conditions according to [43412] are complied with the section values of sectionswhich are subject to bending may be determined simplified as followsFor the tension side the net section and for the compression side the gross section shall be taken For thecentre of gravity the centre of gravity of the gross section shall be assumed
43414 Elastic deformations are normally to be determined using the gross sections
4342 Effective breadth of platingWhen determining section values the effective breadth of plating shall be taken into consideration ifnecessary The calculation of the effective breadth of plating may eg be conducted in according withEurocode 3 (EN 1993-1-5)
435 Particularities4351 Local stressesThe local stresses in the area of force transmissions and discontinuities such as eg diversions of forcesteps of a section cut-outs etc see Figure 4-1 shall be proven separately and superimposed on the globalstressesNotes regarding local stresses due to wheel loads may be taken from [495]
4352 Tie rodsTie rods which may be subject to compressive stresses due to small deviations from the regular loadassumptions shall be proven in the same way as compression members
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 53Standard for shipboard lifting appliances
DNV GL AS
436 Verification procedures4361 General noteIn this standard the methods of partial safety factors and permissible stresses are allowed to be used forverification
4362 Partial safety factor methodThe partial safety factors method is generally applicable It enables weighting of different loads and is thestandard proof of this standard
4363 Method of permissible stressesThe method of permissible stresses is not generally applicable and therefore shall not be used if one or moreof the following structural characteristics exist
a) non-linearity between loads and stresses (compression-stressed structural elements with major defor-mations requiring proof according to 2nd order theory)
b) dead loads with a favourable effect (counter- weightsoverhanging engine houses)c) pre-stresses due to
mdash weights (besides b) in particular mobile weights)mdash ropestension elementsmdash bolts (in general only relevant in special cases)
d) lifting appliance is not fixed and stability against turn-over has not been proven by tests
437 Proof by the method of partial safety factors4371 General notesThe method of partial safety factors distinguishes between safety factors γm relating to resistance values andsafety factors γP relating to loads
4372 Definitions
43721 Loads437211 Loads is the term for all external influences which impact on a structure437212 Loads can eg be dead loads hoisting loads dynamic loads temperature changes or enforceddeformations437213 The loads to be considered in each individual case are regulated in the following sections for therespective lifting appliance
43722 Stresses437221 Stresses is the term for the effects of loads on a structure437222 Stresses can eg be stresses and deformations437223 Stresses are marked by the index Sldquo
43723 Load bearing capacities437231 Load bearing capacities is the term for the permissible limit values of a stress437232 Load bearing capacities are marked by the index Rldquo
43724 Resistance valuesResistance values are material properties like eg yield strength tensile strength and Youngs modulus bywhich eg load bearing capacities and stiffness of cross-sections are calculated
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 54Standard for shipboard lifting appliances
DNV GL AS
43725 Characteristic values437251 Characteristic values of loads or resistance values do not include safety factors437252 Characteristic values are marked by the index k
43726 Dimensioning values437261 Dimensioning values of loads L are the characteristic values increased by the partial safetyfactor γP
Ld = γP ∙ Lk
437262 Dimensioning values of resistance values WG are the characteristic values reduced by thepartial safety factor γm
WGd = WGk γm
437263 Dimensioning values are marked by the index dldquo
4373 General proof formatIn general the degree of utilization (stressutilization ratio) shall be calculated The proof is demonstrated ifthe degree of utilization is not larger than 100
As an alternative stress and utilization can be compared directly The proof is demonstrated if the stress isnot larger than the utilization
Sd Rd le 1 or Sd le Rd
Sd = dimensioning value of load determined from the impacts multiplied by varying partial safety factorsγP
Rd = dimensioning value of load bearing capacity determined from the resistance values divided by thepartial safety factor γm
4374 Partial safety factors
43741 For the calculation the loads which lifting appliance is exposed to are increased by partial safetyfactors of varying magnitude
43742 The partial safety factors for loads are given in Sec5 together with the load combinations to beverified
43743 The partial safety factor for resistance values γm is always
γm = 110unless stated otherwise in individual cases
4375 Load combinations
43751 Loads acting simultaneously according to [424] shall be increased by the partial safety factorsaccording to [4374] and to be superimposed in load combinations
43752 Notes and explanations regarding load combinations are given in the following sections inconnection with the required proofs
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 55Standard for shipboard lifting appliances
DNV GL AS
438 Proof by the method of permissible stresses4381 General notes
43811 The method of permissible stresses is only applicable under certain prerequisites It is regarded tobe a special case within the method of partial safety factors see [4362] and [4363]
43812 Depending on the type of design differing results are possible with the two methods of proofTherefore the Society reserves the right in individual cases to apply a proof using the method of partialsafety factors
4382 Proof formatsWithout partial safety factors the following proof formats exist
Figure 4-1 Examples for local force transmissions and discontinuities
fyr = calculated yield strength according to [4332]γS = global safety factor depending on the load combinations according to Table 5-4 and Table 5-5
load combination I γS = 148
load combination II γS = 134
load combination III γS = 122
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 56Standard for shipboard lifting appliances
DNV GL AS
44 Proof of structural safety
441 General notes
4411 The following statements shall be observed for proofs load bearing structural elements made of steeland aluminium as well as for proofs of special machinery elements according to the method of partial safetyfactors
4412 Calculation and dimensioning of machinery elements which are not dealt with may be performedusing recognized standards or generally recognized technology rules
442 Scope of proofs4421 General notes
44211 The ultimate strength analysis consists of two partial proofs
mdash the general stress analysis according to [4422] andmdash the proof of stability according to [4423]
44212 The internal forces and moments on which the proof of the structural element being consideredcross-section or a weldbolt are based shall include all impacting static and dynamic load components
44213 The proofs of structural safety shall be shown in each case for the most unfavourable loadcombination according to [4375]
44214 If load combinations are not taken into consideration or proofs not carried out this shall besubstantiated in writing unless the reasons for doing so are obvious
4422 General stress analysisThe general stress analysis is the proof of safety against reaching the calculated yield strength according to[4332]
44221 General notes442211 The designations of axes of structural elements used in this standard as well as forces andmoments which may have an impact on a structural element are illustrated in Figure 4-2
Figure 4-2 Axes of structural elements and possible loads
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 57Standard for shipboard lifting appliances
DNV GL AS
Fxyz = Force in direction of the respective axis [N]Mxyz = Moment around the respective axis [Nmm]σxy = Normal stress in direction of the respective axis [Nmm2]τ = Shear stress [Nmm2]
44222 Equivalent stresses442221 Where normal and shear stresses act simultaneously in a cross-section the equivalent stress σvshall be calculated from the respective allocated stresses Spatially oriented stresses shall be broken down tothe co-ordinate system according to Figure 4-2442222 Generally the equivalent stress σv shall be calculated according to the distortion energy theory(von Mises) as follows
442223 In the case of biaxial stresses the calculation of σv is simplified as follows
442224 In the case of uniaxial stresses the calculation of σv is simplified as follows
44223 Format of the strength analysis442231 The strength analysis shall be performed for both the individual stress components as well asthe equivalent stresses analogous to [4373] as follows
σSd σRd le 1 σSd le σRd
τSd τRd le 1 τSd le τRd
σvSd σRd le 1
or
σvSd le σRd
σSd
τSd
σvSd
=dimensioning values of the stresses basedon the loads multiplied by partial safetyfactors γP
= dimensioning values of the permissiblestresses (load bearing capacity)
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fyr = calculated yield strength [4332]
γm = partial safety factor according to[43743]
442232 Where more accurate strength analyses according to recognized calculation methods egaccording to the method of finite elements are conducted or where test results exist the Society maydepending on the facts agree to an increase of the locally permissible stresses
4423 Proof of stability
44231 Proof of calculated safety against lateral buckling lateral torsional buckling or buckling shall beconducted according to a recognized calculation principle or standard for all essential combinations of loads
44232 Proofs of stability for steel constructions may be conducted according to Eurocode 3 (EN 1993-1-1EN 1993-1-3 EN 1993-1-5 EN 1993-1-7)
44233 Proofs of stability for aluminium alloy constructions may be conducted according to Eurocode 9 (EN1999-1-1 EN 1999-1-4 EN 1999-1-5)
44234 Proofs of stability for constructions made of austenitic steel may be conducted according toEurocode 3 (EN 1993-1-4)
44235 When applying Eurocodes for stability proofs the following shall be taken into consideration
mdash Instead of safety factor γM1 according to the Eurocode the value γm according to [43743] shall beused
mdash Instead of the yield strength the calculated yield strength fyr according to [4332] shall be used
45 Proof of safety against overturning
451 General notes
4511 Lifting appliances and parts of lifting appliances not connected integrally to the residual structureshall be sufficiently safe against overturning at all timesFor mobile lifting appliances also whereat operating on a circular track safety against overturning shall beproven in all cases
4512 Safety against overturning of lifting appliances is a measure of its resistance to overturning anddrifting eg by wind andor inclinations of the supporting structureThe many factors which influence safety against overturning in the longitudinal and transverse directionsinclude dead load and dead load distribution track gauge wheel base Safe Working Load and load radiusmotor and braking power and the deformations which occur under load
4513 Lifting appliances which travel on rails shall be equipped with devices to prevent overturning andshall generally be stable even without such devices
4514 Proof of safety against overturning ensures safe working if the equipment is normally and carefullyoperatedIt should be noted that the danger of overturning arising from inexpert or incorrect operation cannot beprecluded no matter how stringent the conditions for proof of safety against overturning
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452 Proof of safety against overturningWith regard to safety against overturning a distinction is made between lifting appliance on rails and fork lifttrucksWhere the danger of overturning exists for parts of non-mobile lifting appliances the proof shall bedemonstrated analogously to [4521]
4521 Lifting appliances on rails
45211 Mathematical proof is regarded as sufficient for the safety against overturning of lifting applianceson railsThis proof shall be conducted using the method of partial safety factors according to [437]Thereby the partial safety factors for loads according to [437] are generally to be considered
45212 Lifting appliances are deemed to be sufficiently safe against overturning if - relative to therespective most unfavourable tilting edge - in the most unfavourable proof and in consideration of the partialsafety factors the sum of restoring moments is larger than the sum of overturning moments
The following condition shall be observed
= sum of restoring moments
= sum of overturning moments
45213 Where desirable or necessary eg in the case of existing lifting appliances proof of safety againstoverturning may also be provided by a special loading testThis test shall in each case be agreed with the Society who will also determine the magnitude of the testload and the nature of the test (static andor dynamic)
45214 Devices to prevent overturning shall be dimensioned for the overturning moment which wouldresult from twice the static hoist load or where lifting appliances without prevention devices are not safeagainst overturning in accordance with the forces occurring in operation
4522 Fork lift trucksThe safety against overturning of fork lift trucks shall be determined on an inclinable platform for each newtypeOn the basis of the results obtained from these measurements the manufacturer shall on demand reviseand certify the conditions ensuring stable operation on inclined planes (due to inclinations of the ship or thecamber and sheer of decks)
46 Proof of fatigue strength
461 General notes
4611 The proof of sufficient fatigue strength i e the strength against crack initiation under dynamic loadsduring operation is useful for judging and reducing the probability of crack initiation of structural membersduring the design stage
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Due to the randomness of the load process the spreading of material properties and fabrication factors andto the effects of ageing crack initiation cannot be completely excluded during later operation Thereforeamong other things periodical surveys are necessary
4612 The fatigue strength analysis shall be conducted according to requirements as given in this sectionor subject to agreement with the Society according to another recognized basic calculation principle
462 Application
4621 The fatigue strength analysis is in principle required for all structural elements connections andsupporting structures of lifting appliances which are exposed to dynamic loads for the states in operationand out of operation and may be demanded by the Society for any type of lifting appliance and operationalcondition
4622 The provisions stated here are applicable to constructions made of normal and high-strength hullstructural steels austenitic steels as well as aluminium alloys Other materials such as extra high-strengthstructural steel and cast steel can be treated upon agreement with the Society in an analogous manner byusing appropriate design S-N curves
4623 Low cycle fatigue problems are not subject to the following rules and shall be specially consideredwhere applicable
463 Definitions
Figure 4-3 Dynamic load cycle
Δσ = applied stress range [Nmm2] (see also Figure 4-3) defined asΔσ = σmax ndash σmin
σmax = maximum upper stress [Nmm2] of a stress cycleσmin = maximum lower stress [Nmm2] of a stress cycleΔσmax = applied peak stress [Nmm2] range within a stress range spectrumσm = mean stress [Nmm2] defined asσm = (σmax + σmin) 2Δσp = permissible stress range [Nmm2]Δτ = Corresponding range [Nmm2] for shear stress
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n = number of applied stress cyclesN = number of endured stress cycles according to S-N curve (= endured stress cycles under constant
amplitude loading)ΔσR = fatigue strength reference value of S-N curve at 2 middot 106 cycles of stress range [Nmm2]
(= FAT class according to Table B-1)fn = factor considering stress spectrum and number of cycles for calculation of permissible stress
rangeΔσRc = corrected fatigue strength reference value of S-N curve at 2 middot 106 stress cycles [Nmm2]D = cumulative damage ratio
464 Quality requirements (fabrication tolerances)
4641 The detail classification of the different welded joints as given in Table B-1 is based on theassumption that the fabrication of the structural detail or welded joint respectively corresponds in regard toexternal defects at least to quality group B according to DIN EN ISO 5817 and in regard to internal defects atleast to quality group C
4642 Relevant information shall be included in the manufacturing document for fabrication If it is notpossible to comply with the tolerances given in the standards this shall be accounted for when designingthe structural details or welded joints respectively In special cases an improved manufacture as stated in[4641] may be required eg stricter tolerances or improved weld shapes see also [46924]
4643 The following stress increase factors km for considering significant influence of axial and angularmisalignment are already included in the fatigue strength reference values ΔσR Table B-1
km = 115 butt welds (corresponding type A1 A2 A11)km = 130 butt welds (corresponding type A3 ndash A10)km = 145 cruciform joints (corresponding type D1 ndash D5)km = 125 T-joints (corresponding type D1 ndash D3)km = 125 fillet welds on one plate surface (corresponding type C7 C8)
Other additional stresses need to be considered separately
465 Stress range spectrum4651 Definitions
46511 The stress range spectrum of a design detail describes the frequency of the different stress rangesto be expected at that location during the lifetime of the lifting appliance
46512 The standard stress range spectrum of lifting appliances describes the frequency of the differentuseful loads to be handled during the lifetime of the lifting appliance
46513 Regarding the fatigue strength analysis it shall be taken into consideration that the standard stressrange spectrum of lifting appliances and the stress range spectrum of a design detail may be different interms of form of spectrum and particularly in terms of number of load cycles or stress cycles respectively
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4652 Stress range spectrum for the condition in operation
46521 Regarding the fatigue strength analysis for the condition in operation lifting appliances arenormally to be categorized in groups corresponding to the standard stress range spectra S0 to S7 accordingto Figure 4-4
46522 Where the operating conditions are precisely known individual clearly separated from each otherstructural groups or elements may or must be categorized differently
46523 The number nmax of stress cycles during operation shall be provided by the manufacturer
46524 The stress spectra S0 to S6 are defined by the following equation (see Figure 4-4)
Δσ = stress rangeΔσmax = maximum stress range of the spectrum according to [464]n = number of stress cyclesnmax = total number of stress cycles
κ =
p = coefficient according to Table 4-3
For p = 0 κ = 15 shall be assumed
Table 4-3 Coefficients for the calculation of the κ-value
Spectrum S0 S1 S2 S3 S4 S5 S6
p 07 17 27 37 47 57 67
46525 Applicable for the stress range spectrum S7
= 1 = constant
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Figure 4-4 Standard stress range spectra
46526 Where the operating conditions of shipboard lifting appliances are exactly known individuallydetermined stress range spectra may be used for the fatigue strength analysis based on calculatedcumulative damage ratios The individual stress range spectra shall be proven by the manufacturer
4653 Stress range spectra for the condition out of operationThe fatigue strength analysis for the condition out of operation shall be conducted for the straight-linespectrum A according to Figure 4-4 and a total number of stress cycles nmax = 5 middot 107
466 Calculation of the maximum stress range
4661 The fatigue strength analysis is depending on the detail considered based on one of the followingtypes of stress
mdash for notches of free plate edges the notch stress σk determined for linear-elastic material behaviour isrelevant The fatigue strength is determined by the FAT class (ΔσR) according to Table B-1 type E2 and E3
mdash for welded joints the fatigue strength analysis is normally based on the nominal stress σn at the structuraldetail considered and on an appropriate detail classification as given in Table B-1 which defines the FATclass (ΔσR)
mdash for those welded joints for which the detail classification is not possible or additional stresses occur whichare not or not adequately considered by the detail classification the fatigue strength analysis may beperformed on the basis of the structural stress σS in accordance with [468]
4662 The maximum stress range for a construction detail shall be calculated from the highest maximumstress σmax and the lowest minimum stress σmin in this detail
Δσmax = σmax- σmin
4663 The maximum upper stress σmax and the minimum lower stress σmin shall be determined each fromloads of the most unfavourable magnitude location and direction acting on the lifting appliance in the mostunfavourable position
Thereby all partial safety factors shall be set γp = 1
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467 Fatigue strength analysis for free plate edges and for welded jointsusing detail classification4671 Definition of nominal stress and detail classification for welded joints
46711 Corresponding to their notch effect welded joints are normally classified into detail categoriesconsidering particulars in geometry and fabrication including subsequent quality control and definition ofnominal stress Table B-1 shows the detail classification based on recommendations of the InternationalInstitute of Welding (IIW) giving the FAT class (ΔσR) for structures made of steel or aluminium alloys (Al)It shall be noted that some influence parameters cannot be considered by the detail classification and that alarge scatter of fatigue strength has therefore to be expected
46712 Details which are not contained in Table B-1 may be classified either on the basis of local stressesin accordance with [468] or else by reference to published experimental work or by carrying out specialfatigue tests assuming a sufficiently high confidence level (see [4691]) and taking into account thecorrection factors as given in [46926]Details contained in Table B-1 produced by improved manufacturing technology may be classified bycarrying out special fatigue tests as described above Such classification of details shall be agreed upon withthe Society case by case
46713 Regarding the definition of nominal stress the arrows in Table B-1 indicate the location anddirection of the stress for which the stress range shall be calculated The potential crack location is alsoshown in Table B-1 Depending on this crack location the nominal stress range shall be determined by usingeither the cross sectional area of the parent metal or the weld throat thickness respectivelyBending stresses in plate and shell structures shall be incorporated into the nominal stress taking thenominal bending stress acting at the location of crack initiation
Guidance noteThe factor Ks for the stress increase at transverse butt welds between plates of different thickness (see type A5 in Table B-1) canbe estimated in a first approximation as follows
t1 = smaller plate thickness
t2 = larger plate thickness
Additional stress concentrations which are not characteristic of the FAT class itself eg due to cut-outs in the neighbourhood of thedetail shall also be incorporated into the nominal stress
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
46714 In the case of combined normal and shear stress the relevant stress range shall be taken as therange of the principal stress at the potential crack location which acts approximately perpendicular (withinplusmn45deg) to the crack front as shown in Table B-1 as long as it is larger than the individual stress components
46715 Where solely shear stresses are acting the largest principal stress σ1 = τ may be used incombination with the relevant FAT class
468 Fatigue strength analysis for welded joints based on local stresses
4681 Alternatively to the procedure described in the preceding paragraphs the fatigue strength analysisfor welded joints may be performed on the basis of local stresses For common plate and shell structures inships the assessment based on the so-called structural (or hot-spot) stress σs is normally sufficient
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The structural stress is defined as the stress being extrapolated to the weld toe excluding the local stressconcentration in the local vicinity of the weld see Figure 4-5
Figure 4-5 Structural stress
4682 The structural stress can be determined by measurements or numerically eg by the finite elementmethod using shell or volumetric models under the assumption of linear stress distribution over the platethickness Normally the stress is extrapolated linearly to the weld toe over two reference points which arelocated 05 and 15 times plate thickness away from the weld toe In some cases the structural stress can becalculated from the nominal stress σn and a structural stress concentration factor Ks which has been derivedfrom parametric investigations using the methods mentioned Parametric equations should be used with dueconsideration of their inherent limitations and accuracy
4683 For the fatigue strength analysis based on structural stress the S-N curves shown in Figure 4-6apply with the following reference values
ΔσR = 100 (resp 40 for Al) for the butt welds types A1 ndash A6 and for K-butt welds with fillet welded endseg type D1 in Table B-1 and for fillet welds which carry no load or only part of the load of theattached plate type C1 ndash C9 in Table B-1
ΔσR = 90 (resp 36 for Al) for fillet welds which carry the total load of the attached plate eg type D2 inTable B-1
In special cases where eg the structural stresses are obtained by non-linear extrapolation to the weld toeand where they contain a high bending portion increased reference values of up to 15 can be allowed
4684 In addition to the assessment of the structural stress at the weld toe the fatigue strength withregard to root failure shall be considered by analogous application of the respective FAT class eg type D3 ofTable B-1In this case the relevant stress is the stress in the weld cross section caused by the axial stress in the plateperpendicular to the weld It shall be converted at a ratio of t (2 middot a)
469 Design S-N curves4691 Description of the design S-N curves
46911 The design S-N curves for the calculation of the cumulative damage ratio according to [46101]are shown in Figure 4-6 for welded joints at steel and in Figure 4-7 for notches at plate edges of steel platesFor aluminium alloys (Al) corresponding S-N curves apply with reduced reference values of the S-N curves(FAT classes) according to Table B-1 The S-N curves represent the lower limit of the scatter band of 95 ofall test results available (corresponding to 975 survival probability) considering further detrimental effectsin large structures
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To account for different influence factors the design S-N curves shall be corrected according to [4692]
Figure 4-6 S-N curves for welded joints at steel
Figure 4-7 S-N curves for notches at plate edges of steel plates
46912 The S-N curves represent section-wise linear relationships between log (Δσ) and log (N)
log(N) = 70 + m middot Q
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Q = coefficient defined as
Q = log(ΔσR Δσ) - 069897 m0
m = slope exponent of S-N curve see [46913] and [46914]m0 = inverse slope in the range N le 1 middot 107 defined asm0 = 3 for welded jointsm0 = 35 divide 5 for free plate edges (see Figure 4-7)
The S-N curve for FAT class 160 forms the upper limit for the S-N curves of free edges of steel plates withdetail categories 100 ndash 150 in the range of low stress cycles see Figure 4-7 The same applies accordingly toFAT classes 32 ndash 40 of aluminium alloys with an upper limit of FAT 71 see type E1 in Table B-1
46913 For structures subjected to variable stress ranges the S-N curves shown by the solid lines in Figure4-6 and Figure 4-7 shall be applied (S-N curves of type M) ie
m = m0 for N le 107 (Q le 0)m = 2 middot m0 ndash 1 for N gt 107 (Q gt 0)
46914 For stress ranges of constant magnitude (stress range spectrum S7) in non-corrosive environmentfrom N = 1 middot 107 the S-N curves of type O in Figure 4-6 and Figure 4-7 can be used thus
m = m0 for N le 107 (Q le 0)m = 22 for N gt 107 (Q gt 0)
4692 Correction of the reference value of the design S-N curve
46921 A correction of the reference value of the S-N curve (FAT class) is required to account for additionalinfluence factors on fatigue strength as follows
ΔσRc = fm fR fw fi ft fs ΔσR
ΔσR = FAT class according to Table B-1 or EN 1993-1-9fm = correction factor for material effect according to [46922]fR = correction factor for mean stress effect according to [46923]fw = correction factor for weld shape effect according to [46924]fi = correction factor for importance of structural element according to Table 4-4ft = correction factor for thickness effect according to [46925]fs = additional correction factor for structural stress analysis according to [46926]
For the description of the corrected design S-N curve the formulae given in m may be used by replacing ΔσRby ΔσRc
46922 Material effect (f)For welded joints it is generally assumed that the fatigue strength is independent of steel strength ie
fm = 10For free edges at steel plates the effect of the materials yield strength is accounted for as follows
For aluminium alloys fm = 1 generally applies
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46923 Effect of mean stress (f)The correction factor fR shall be determined by the following formulae
fR = 10 for σm ge (∆σmax2) (range of tensile pulsating stresses)
fR = for ndash (∆σmax2) le σm le (∆σmax2) (range of alternating stresses)
fR = 1 + 2 c for σm le ndash (∆σmax2) (range of compressive pulsating stresses)
c = coefficient defined as
c = 0 for welded joints subjected to constant stress cycles (stress range spectrum S7)c = 015 for welded joints subjected to variable stress cycles (corresponding to stress range
spectrum A or S0divideS6)c = 030 for unwelded base material
46924 Effect of weld shape (f)In normal cases
fw = 10A factor fw gt 10 applies for welds treated eg by grinding Grinding removes surface defects such as slaginclusions porosity and crack-like undercuts to achieve a smooth transition from the weld to the basematerial Final grinding shall be performed transversely to the weld direction The depth should be about 05mm larger than the depth of visible undercutsFor ground weld toes of fillet and K-butt welds machined by
fw = 115 for disc grinderfw = 130 for burr grinder
Premise for this is that root and internal failures can be excluded Application of toe grinding to improvefatigue strength is limited to following details of Table B-1
mdash butt welds of type A2 A3 and A5 if they are ground from both sidesmdash non-load-carrying attachments of type C1 C2 C5 and C6 if they are completed with a full penetration
weldmdash transverse stiffeners of type C7mdash doubling plates of type C9 if the weld throat thickness according to Sec11 [326] was increased by 30mdash cruciform and T-joints of type D1 with full penetration welds
The corrected FAT class that can be reached by toe grinding is limited for all types of welded connections ofsteel to fw ΔσR = 100 Nmm2 and of aluminium to fw ΔσR = 40 Nmm2For butt welds ground flush the corresponding reference value of the S-N curve (FAT class) shall be choseneg type A1 A10 or A12 in Table B-1For endings of stiffeners or brackets eg type C2 in Table B-1 which have a full penetration weld and arecompletely ground flush to achieve a notch-free transition the following factor applies
fw = 14The assessment of a local post-weld treatment of the weld surface and the weld toe by other methods egultrasonic impact treatment shall be agreed on in each case
46925 Plate thickness effect (f)In order to account for the plate thickness effect application of the reduction factor ft is required for buttwelds oriented transversely to the direction of applied stress for plate thicknesses t gt 25 mm
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n = exponent for additional notch effect at weld toe defined as
n = 020 as weldedn = 010 toe-ground
k = exponent for misalignment (see [4643]) defined as
k = 010 for butt welds with km = 130k = 005 for butt welds with km = 115
km = factor according to [4643]
For all other weld connections consideration of the thickness effect may be required subject to agreementwith the Society
46926 Correction factor for structural stress analysis (f)If the fatigue strength analysis for welded joints is based on local stresses according to [468] then thereference value ΔσRc of the corrected S-N curve shall be determined according to [4643] taking intoaccount the following additional correction factor which describes influencing parameters not included in thecalculation model such as eg misalignment
Δσsmax = applied peak stress range within a stress range spectrumΔσsb = bending portion of Δσsmax
krsquom = effective stress increase factor due to misalignments under axial loading defined askrsquom = km ndash 005
km = stress increase factor due to misalignments under axial loading at least km according[4643]
If the fatigue strength analysis for free plate edges and for welded joints is based on detail classificationaccording to [467] then fs = 10
Table 4-4 Influence of the importance fn of a structural element on the fatigue strength analysis
Not safe to operate structural elementAccessibility Safe to operate
structural element No hazard to persons Hazard to persons
Accessible structuralelements 10 09 083
Badly accessible structuralelements 095 087 08
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Not safe to operate structural elementAccessibility Safe to operate
structural element No hazard to persons Hazard to persons
Safe to operate structural elements are parts with restricted consequences of a failure ie where the local breakage ofa structural element does not result in the failure of the structure or fall-down of the load
Not safe to operate structural elements are parts where the local breakage of a structural element results in immediatefailure of the structure of fall-down of the load
4610 Proof46101 Calculation of the cumulative damage ratio
461011 Where the fatigue strength analysis is based on the calculated cumulative damage ratio thepartial damages Di caused by the operating conditions in operation and out of operation shall bedetermined as follows
K = total number of blocks of the stress range spectrum for summation (in general K ge 20)nk = number of stress cycles in block kNk = number of endured stress cycles determined from the corrected S-N curve (see [469]) taking Δσ
= Δσk
Δσk = stress range of block k
For this purpose in the condition in operation standard stress range spectra according to [46524] or[46525] or individually determined stress range spectra according to [46526] may be applied For thecondition out of operation the straight-line stress range spectrum according to [4653] shall be applied
461012 The proof of fatigue strength is demonstrated if for the total cumulative damage ratio D thefollowing condition is met
46102 Permissible stress range
461021 The fatigue strength analysis may be performed based on the permissible maximum stressranges For this purpose in the condition in operation standard stress range spectra according to[46524] or [46525] shall be applied for the condition out of operation the straight-line stress rangespectrum according to [4653]The requirements given in the following are applicable for fatigue strength analyses conducted separately forthe conditions in operation and out of operationA superposition of the damages caused by the conditions in operation and out of operation is notrequired provided that the maximum stress range caused by the condition out of operation does notexceed 10 of the maximum stress range caused by the condition in operation Otherwise the fatiguestrength analysis shall be conducted on the basis of the calculated cumulative damage ratios according to[46101] or upon agreement with the Society
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Table 4-5 Factor fn for the determination of the permissible stress range for welded joints (m0 =3)
Number of stress cycles nmaxStressspectrum 2∙104 5∙104 105 3∙105 6∙105 106 3∙106 6∙106 107 5∙107 108
S0 1654 1294 1068 784 644 558 409 336 291 195 167
S1 1263 970 787 568 461 397 284 232 201 137 119
S2 1025 775 623 443 357 304 215 174 151 105 092
S3 836 623 500 352 282 240 168 134 116 082 072
S4 693 516 412 288 230 195 136 108 093 066 058
S5 592 438 348 244 194 164 114 091 077 056 048
S6 513 378 302 209 166 140 098 078 066 047 041
S7 470 345 275 191 151 127 089 070 059 043 037
Table 4-6 Factor fn for the determination of the permissible stress range for free edges of plateswith (m0 = 35)
Number of stress cycles nmaxStressspectrum 2∙104 5∙104 105 3∙105 6∙105 106 3∙106 6∙106 107 5∙107 108
S0 9341251 1
8181019 1
739873 1
620677 1
548574 1 496 391 333 296 209 184
S1775
983 1668
787 1595
665 1485 420 372 282 238 211 151 134
S2665
809 1568
638 1497
534 1394 333 290 217 182 161 117 105
S3562
665 1475
520 1414 320 266 230 171 141 125 093 083
S4475
555 1400
430 1350 262 217 188 138 114 100 076 068
S5407
473 1340
366 1300 222 183 159 116 095 084 063 056
S6354
412 1296
317 1260 191 157 136 100 082 071 054 048
S7325
377 1270
290 1235 174 143 123 090 074 064 049 043
1) For ΔσR lt 125 [Nmm2]
(ΔσR FAT class according to legacy GL Rules for Hull Structures (I-1-1) Section 20 Table 203)
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Table 4-7 Factor fn for the determination of the permissible stress range for free edges of plateswith (m0 = 4)
Number of stress cycles nmaxStressspectrum 2∙104 5∙104 105 3∙105 6∙105 106 3∙106 6∙106 107 5∙107 108
S0778
883 1
1007 2
685732 1
848 2
620662 1
745 2
528560 1
598 2473
500 1436
458 1 365 322 293 219 195
S1647
693 1
809 2
562600 1
668 2
502536 1
580 2418
443 1372
388 1 339 275 240 217 161 145
S2554
594 1
674 2
475507 1
552 2
421449 1
473 2356
363 1 304 275 217 186 168 127 115
S3467
500 1
560 2
397424 1
453 2349
372 1 285 248 224 172 146 132 101 092
S4395
424 1
470 2
333356 1
377 2291
311 1 237 205 183 140 118 106 083 075
S5339
363 1
401 2
284304 1
320 2248
266 1 201 174 154 117 099 088 069 063
S6296
317 1
349 2
247265 1
278 2215
230 1 173 150 133 101 085 075 06 054
S7270
290 1
319 2
225241 1
254 2196
211 1 158 137 120 092 077 068 054 049
1) For ΔσR lt 150 [Nmm2]2) For ΔσR lt 140 [Nmm2]
(ΔσR FAT class according to legacy GL Rules for Hull Structures (I-1-1) Section 20 Table 203)
Table 4-8 Factor fn for the determination of the permissible stress range for free edges of plateswith (m0 = 5)
Number of stress cycles nmaxStressspectrum 2∙104 5∙104 105 3∙105 6∙105 106 3∙106 6∙106 107 5∙107 108
S0 729 642 583 496 447 414 349 314 291 230 209
S1 607 526 471 394 352 323 269 240 221 175 160
S2 519 446 395 327 288 263 217 192 177 142 130
S3 438 371 327 267 235 214 174 153 141 114 106
S4 371 311 273 221 194 176 142 124 114 094 087
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Number of stress cycles nmaxStressspectrum 2∙104 5∙104 105 3∙105 6∙105 106 3∙106 6∙106 107 5∙107 108
S5 317 266 233 188 164 149 120 105 095 079 073
S6 277 231 201 163 142 128 103 090 081 068 063
S7 253 211 184 148 129 116 093 081 073 061 057
Table 4-9 Factor fn for the straight-line stress spectrum with nmax = 5 middot 107
Welded joints Free edges of plates
m0 = 3 m0 = 5 m0 = 4 m0 = 35
353 363 366 365
461022 The maximum stress range of the spectrum shall not exceed the permissible value Δσp
Δσmax le Δσp
Δσmax = maximum stress range according to [466]Δσp = permissible stress range according to [461023]
461023 The permissible stress ranges shall be calculated by the following formula
Δσp = fn middot ΔσRc
ΔσRc = corrected FAT class according to [46921]fn = factor for the shape and extent of the spectrum according to Table 4-5 to Table 4-9
47 Proof of suitability for use
471 General notes
4711 Shipboard lifting appliances as well as its structural elements and equipment shall be such designedand dimensioned that its safety and proper functioning is not adversely affected or endangered by one ormore of the influences stated hereafter
mdash deformations(eg formation of large amplitudes of vibration bending loads on hydraulic cylinders of telescopic beams)
mdash vibrations(eg generated by simultaneous operation of several lifting appliance drives by ship machinery orinfluences of sea state)
mdash heat(eg expansion overheating of drives or brakes)
mdash highest position of boom(see [12211])
4712 Suitability for use shall be demonstrated in the course of the initial testing on board
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DNV GL AS
472 Permissible deformations4721 Compression members
47211 The uniform deflection of compression members under permissible load shall not be larger than therod length divided by 250
47212 The uniform deflection of unloaded compression members or compression members loaded by thedead load which are 1st order structural elements shall not be larger than the rod length divided by 500
47213 The uniform deflection of unloaded compression members or compression members loaded by thedead load which are 2nd order structural elements such as eg wind installations or framework stiffenersshall not be larger than the rod length divided by 350
4722 Tension membersThe uniform deflection of unloaded tension members shall not be larger than the rod length divided by 50
48 Joints
481 Proof of weld joints4811 PrerequisitesThe strength of welding consumables shall be equal to or higher than that of the structural elements to beconnectedFor further general prerequisites see Sec11
4812 General strength analysis
48121 General notesWeld thicknessrsquos which are the basis of the strength analysis are given in [114] for various shapes ofwelds
48122 Welds located in the plate planeThe permissible stress of welds located in the plate plane is the dimensioning value of the permissible stressof the adjoining plate according to [442231]
48123 Fillet weldsFor fillet welds the strength analysis may be conducted according to RU SHIP Pt6 Ch13 or according to arecognized basic principle of calculation or standard
48124 Plates loaded by tension transversely to the direction of rolling481241 Where enhanced properties in thickness direction are required for plates and wide flat bar steelthe following minimum requirements apply for the reduction of area after fracture Z which is the meanvalue of 3 tensile test samples to be taken with their longitudinal axis perpendicular to the surface of theproduct
Zmin = 25Of these one single value may be less than 25 but not less than 20481242 Where structural elements are exposed to increased loads a minimum value of 35 (lowestsingle value 25) may be required see Eurocode 3 (EN 1993-1-10)
4813 Proof of fatigue strengthRegarding the proof of fatigue strength the statements in [46] apply
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DNV GL AS
482 Proofs for bolted connections4821 General notes
48211 Bolted connections shall be dimensioned according to recognized guidelines basic principles ofcalculation or standards which possibly also allow for a fatigue strength analysis for the bolts
48212 The approaches according to [4822] and [4823] in principle imply that
mdash connected areas are secured against distortion eg by use of at least 2 boltsmdash contacting areas are smooth and free from greasemdash the use of bolts of strength class 129 is agreed with the Society
4822 Gusset connections with fitting-bolts (fitting-bolt shear connections)
48221 DefinitionIn the case of fitting-bolt shear connections the loads to be carried are transferred by form-fitting Theseforces generate shear stresses in the bolts and bearing stresses at the gussets
48222 Construction notes482221 Figure 4-9 shows a typical gusset connection If it is intended to be constructed as a fitting-boltshear connection the following notes shall be observed
mdash The clearance between bolt and drilling hole shall correspond to the tolerance classes h13 and H11 (orless) according to ISO 286-2
mdash Bolt shafts shall be as long as the thickness of the parts to be connected Where due to the cylindric shaftlength it is not possible to tighten the bolts washers shall be used
mdash Controlled pre-stressing of bolts is not required however a suitable securing device against looseningmdash A special surface treatment of the contact areas is not requiredmdash Forces to be transferred may at the maximum be distributed over 5 (strength classes 46 and 56) or
3 (strength classes 88 109 and possibly 129) bolts per row to be arranged one after another in thedirection of force
482222 Regarding the edge and hole distances according to Figure 4-9 the limit values according toTable 4-10 apply
Table 4-10 Limit values for edge and hole distances
Min Max 1
Edge distances e1 and e2 15 middot dℓ 4 middot t + 40 mm
Hole distances p1 and p2 30 middot dℓ The lesser value of 14 middot t or 200 mm
1) t ndash thickness of the thinnest external plate
48223 Permissible stresses for bearing stress and shearing-off482231 For the bearing stress of structural elements made of steel as well as for the shearing-off ofbolts the following permissible stresses apply
σzul = (bearing stress)
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DNV GL AS
τzul = (shearing-off)
ReH = yield strength of structural elements andor gussets according to material standard (nominalvalue)
ReHs = yield strength of bolts according to Table 4-11
482232 Correction coefficients ασ ατ
a) Multishear bolt connections
ασm = minimum of
mdash c1 (3 middot d ℓ) or
mdash p1 (3 middot d ℓ) minus 025 or
mdash Rms Rm or
mdash 10
ατm = 10Rms = tensile strength of bolts according to Table 4-11 [Nmm2]Rm = tensile strength of structural elements according to material standard (nominal value) [N
mm2]
b) Single-shear bolt connections
ασe = 078 middot α σm
ατe = 077
Table 4-11 Strength values of bolts
Strength class 46 56 88 109 129
ReHs [Nmm2] 240 300 640 900 1080
Rms [Nmm2] 400 500 800 1000 1200
48224 Proofs for transmissible bolt forces482241 To determine the largest bolt forces for the example in Figure 4-9 the following forces shall beadded geometrically
ΔFxd =
ΔFzd =
ΔFMd =
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DNV GL AS
482242 For the most unfavourably stressed fitting-bolts on a connection or joint the following proofs forshearing-off of bolts and bearing stresses of the connected parts shall be provided
mdash bearing stresses Frd le ds middot tmin middot σzulmdash shearing-off Frd le As middot nf middot τzul
Frd = largest resulting bolt force (rectangular to the bolt axis) according to [482241]ds = shaft diameter of the fitting-bolt (nominal diameter + 10 mm)tmin = smallest effective plate thicknessAs = cross-section area of shaft of fitting-boltnf = number of effective shear areas (single-shear or multishear)
σzul τzul = permissible stresses according to [48223] [Nmm2]
482243 In the case of a dynamic shear load the fatigue strength analysis shall be conducted for themost unfavourably loaded fitting-bolt as follows
Stress spectra shall be determined according to [46]
The maximum stress range of the shear stress Δτmax shall be determined according to [46] for the shaftcross-section of the fitting-bolt
The design S-N curve for shear stress of fitting-bolts is shown in Figure 4-8
The fatigue strength analysis may be conducted on the basis of calculated damage ratios according to [46]
As an alternative the fatigue strength analysis may be conducted on the basis of permissible stress rangesfor the standard spectra S0 to S7 according to [46] as follows
Δτmax le fnmiddot fi middot ΔτR
Δτmax = maximum stress range of the shear stress for the shaft cross-section of the fitting-boltΔτR = reference value for the stress range of the shear stress at 2middot106 stress cycles
ΔτR = 100 Nmm2
fn = factor for the shape and extent of the spectrum according to Table 4-12fi = influence of the importance of the structural element according to Table 4-4
Figure 4-8 Design S-N curve for shear load of fitting-bolts
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DNV GL AS
48225 Proofs for structural elements and gussetsThe strength analyses for the structural elements and gussets connected with each other shall be based onthe cross-sections designed for tension compression shear and bending according to [434]For the permissible stresses see [4422]
4823 Gasset connections with prestressed bolts (friction-grip connections)
48231 DefinitionWith friction-grip connections the forces to be sustained are submitted by friction between the contact areas(frictional locking)Fitting-bolts with the normal clearance do not effect any increase in the transmissible forces
Table 4-12 Factor fn for standard stress range spectra S0 to S7 according to [465] and design S-N curve according to Figure 4-8
Number of stress cycles nmaxStressspectrum 2middot104 5middot104 105 3middot105 6middot105 106 3middot106 6middot106 107 5middot107 108
S0 729 642 583 496 447 414 349 313 288 224 201
S1 607 526 471 394 351 323 269 238 218 167 151
S2 519 446 395 327 288 263 216 191 173 132 119
S3 438 371 327 267 235 214 174 153 138 103 094
S4 371 311 273 221 194 176 142 124 113 082 076
S5 317 266 233 188 164 149 120 105 095 069 062
S6 277 231 201 163 142 128 103 090 081 059 053
S7 253 211 183 147 128 116 093 081 073 053 046
48232 Construction notesFigure 4-9 shows a typical gusset connection For construction purposes the following notes shall beobserved
mdash Bolt holes shall not exceed the shaft diameter by more than 10 mmmdash The bolts shall be pre-stressed by controlled procedures and under consideration of the dispersion of the
installation force to the maximum installation force FMmax = αs middot ReHs middot Aσ where Aσ is the stress cross-section of the bolt Preferably the pre-stress coefficient is αs = 07 Well-founded deviations in the rangeof 06 le αs le 08 may be permitted
mdash Up to a thread diameter of 30 mm the pre-stress may be effected by the application of a torque Withlarger diameters hydraulic lengthening shall be applied
mdash For the contact areas a special surface treatment is required according to [48233]mdash Casting compound for compensation of unevennesses in the contact areas is not permissiblemdash Only bolts of strength class 88 109 and possibly 129 may be usedmdash The forces to be submitted may be distributed over 3 rows of bolts at a maximummdash The hole distances shall comply with the requirements according to [482222]mdash Only one plate of a gusset connection may have a plate thickness which is equal to or higher than the
bolt diametermdash Bolts of strength class 129 require a highly accurate layout in the supporting areas under the head and
nut
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DNV GL AS
48233 Friction coefficient microThe friction coefficient depends on the surface treatment and shall be selected as followsmicro = 050 for surfaces
mdash of shining metal layers steel shot or sand blasted without unevennessrsquomdash steel shot or sandblasted and covered with aluminiummdash steel shot or sandblasted and metal covered by a metal cover made of a zinc material which effects a
friction coefficient of at least 05
micro = 040 for surfaces
mdash steel shot or sand blasted and coated with a 50 microm to 80 microm thick alkali-zinc-silicate layer
micro = 030 for surfaces
mdash shiny metallic cleaned with a steel brush or by flame deseaming
micro = 020 for surfaces
mdash free of rust oil and dirt
48234 Proof of transmissible forcesA sufficient slide resistance shall be proven for the most unfavourable bolt in a connection or joint seeexample in [482241] using the following condition
Frd le Fμd middot nr
Fμd =
Fμd = force transmissible by friction in 1 friction areanr = number of effective friction areaAσ = stress section-area of the bolt according to Table 4-13Fa = external tension force in the direction of the bolt axismicro = friction coefficient according to [48233]ΔFSetz = loss of pre-stress force by setting according to [49142]αA = tightening factor of the tightening procedure used αA = FMmaxFMmin
FMmax = maximum installation force in consideration of the dispersion of installation force for thetightening procedure used
FMmin = minimum installation force in consideration of the dispersion of installation force for thetightening procedure used
Additionally sufficient resistance against shearing-off and bearing pressure according to [4822] shall beproven including the calculation of the shear capability of the stress cross-section Aσ
48235 Proof of surface pressure under head and nut of the boltFor material S 235 and where applicable also for S 355 proof of the permissible surface pressure under thehead or nut of the bolt respectively shall be to carried out in the following way
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DNV GL AS
If proof cannot be provided tempered washers shall be used
σp zul = permissible surface pressure in according with Table 4-14 [Nmm2]Aa = smallest contact surface of the bolt head or nut considering bore diameter and chamfers [mm2]Fad = Dimensioning value of the external tensile force in the direction of the bolt axisΦ = tensioning factor according to [49132]
Figure 4-9 Example of a gusset connection
48236 Proofs for structural elements and gussetsFor the strength analyses the statements according to [48225] apply It may be assumed that 13 of theforce Fμd transmissible by friction has already been transmitted before the bolt hole see [48234]
Table 4-13 Stress and core sections of bolts
Diameter [mm] Stress section Aσ [mm2] Core section AK [mm2]
Metric ISO thread according to DIN 13
12 843 7625
14 115 1047
16 157 1441
18 193 1751
20 245 2252
22 303 2815
24 353 3243
27 459 4271
30 561 5190
Metric thread with large clearance according to DIN 2510 Sheet 2
33 668 617
36 786 723
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Diameter [mm] Stress section Aσ [mm2] Core section AK [mm2]
39 943 873
42 1083 999
45 1265 1174
48 1426 1320
52 1707 1590
56 1971 1833
64 2599 2426
72 3372 3174
80 4245 4023
90 5479 5226
100 6858 6575
Table 4-14 Permissible surface pressure under heads and nuts of bolts
Material σp zul [Nmm2]
S235 260
S355 C45N 46G2N 46Cr4N 420
C45V 46Cr4V 42CrMo4V 700
GG25 800
483 Proofs for rivet connectionsFor proof of rivetshear connections the statements in [4822] apply analogously Instead of shaftdiameter the hole diameter shall be usedOnly hydraulic riveting is permissible The clamping length of the rivet shall be restricted to the value 65 middotdrivet where drivet is the nominal diameter of the rivet
49 Special structural elements
491 Flange connections with pre-stressed bolts4911 General
49111 In the case of flange connections with pre-stressed bolts the forces to be sustained are transmittedby tensional load of the bolts and possibly by friction fitting
49112 The provisions under [4913] and [4913] do not apply to flanges for the connection of largeslewing bearings In this respect [5741] shall be observed
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DNV GL AS
4912 Construction noteFigure 4-10 shows a typical flange connection For construction purposes the following notes shall beobserved
mdash Bolt holes may be larger than the shaft diameter ds by the value ΔdΔd le 01 middot ds le 30 mm
mdash In general the bolt distance s (see Figure 5-4) shall not be larger than 6 middot dsmdash In general the span length of bolts shall be at least 3 middot dsmdash At least 3 threads shall remain freemdash The bolts shall be pretensioned by controlled procedures The degree of utilization ν of the yield strength
ReHs of the bolt in the mounted condition is preferably in the range 07 le ν le 09 Well-foundeddeviations may be permitted
mdash Up to a thread diameter of 30 mm pretension may be conducted by application of a torque in the case oflarger diameters hydraulic lengthening is required
mdash The contact surfaces require a special surface treatment according to [48233]mdash Casting compound for compensation of unevennesses of the contact areas is not permissible un-less
otherwise stated by slewing bearing makersmdash Only bolts of strength class 88 109 and possibly 129 may be usedmdash Bolts of strength class 129 require a highly accurate layout in the supporting areas under the head and
nut
4913 Forces acting on a flange connection
49131 Figure 4-10 shows a typical flange connection with its essential dimensions and the proportionalexternal axial force Fa per bolt sectorThe external axial force Fa acting on the individual bolt location of the flange connection may normally bedetermined by means of elastomechanics from the operational loads of the gusset connectionIn the case of an excentric load the compensating line of action of the external axial force has the distanceaers from the bolt axis The distance aers shall be determined from the location of the zero point of thebending moment curve of the system which is the nearest to the bolt
49132 The external force Fa in the connecting parts (tension force) acts as an additional load on theprestressed bolt and reduces the surface pressure in the parting line The force ratio Φ governs the portion ofthe external axial force which acts on the bolt additionally to the prestressing force as well as the remainingportion which discharges the tensioned structural elements
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DNV GL AS
Figure 4-10 Flange connection
The force ratio Φ depends on the resiliences of the bolt and the tensioned structural elements theexcentricity of the tensioning andor the external operational force as well as the leading-in of the force Thereliable determination of Φ is therefore complex and shall in principle be conducted by way of measurementtechniques or based on recognized calculation procedures
Provided that the bending of the bolt due to the excentricity of the tensioning and the bending of the bolt dueto the excentricity of the external axial force Fa do not superimpose each other in the same direction Φ maybe approximately calculated as follows
Φ = α for proofs in [49141] [49143] [49151] and [48235]
= 0 for proofs in [49142] and [4915]
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DNV GL AS
δs = axial resilience of the bolt [mmN]δp = axial resilience of the tensioned structural elements [mmN]lk = clamping length [mm]ds = shaft diameter of the bolt [mm]Es = Youngs modulus of the bolt [Nmm2]Ep = Youngs modulus of the tensioned structural elements [Nmm2]dw = head bearing diameter [mm]g = flange dimension according to Figure 4-10 [mm]f = bolt distance [mm]
4914 Proofs for the external tension force F of the boltThe proofs described in the following apply to bolt connections with an external axial force Fa according to[49131] provided that
mdash Tensioned structural elements form simple prismatic bodiesmdash The load on the bolt is proportional to the external axial forcemdash Where external loads are absent the surface pres-sure in the parting line of the prestressed bolt
connection is to a large extent evenly distributed
A surface pressure in the parting line of the prestressed bolt connection to a large extent evenly distributedmay normally be assumed if the dimensions of the parting line are as follows
g lt dw+tf
tf = thickness of the thinner flange plate
Bolt connections which are in addition to an external axial force or solely loaded by an external bendingmoment shall be proven separately
49141 Proof of yield strength of the boltIn the mounted condition the following condition shall be observed
FMmax le FMzul
Where torsion-free tightening procedures are applied the permissible installation force FMzul is as follows
FMmax = maximum installation force
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DNV GL AS
FMzul = permissible installation forceReHs = yielding strength of the boltν = predefined degree of utility of the yield strength in the mounted conditionAσ = stress cross-section of the bolt according to Table 4-13dσ = stress diameter of the boltd2 = effective diameter of the boltP = pitch of threadμG = friction coefficient in the thread
If there is no information about the friction coefficient μG in the thread the friction coefficient shall beestimated conservatively eg according to VDI-Richtlinie 2230 Blatt 2 with consideration of surfaceproperties and lubricants used
In service the equivalent stress of the bolt shall not exceed the permissible value
In the case of torsion-free tightening procedures or in the case of complete reduction of torsion stresses inthe thread in service proof of operational stress of the bolt may be conducted as follows
σvd = design value of the maximum equivalent stress of the bolt in operationσzd = design value of the maximum tensile stress of the bolt in operationτredd = design value of the reduced maximum torsion stress of the bolt in operationFSd = design value of the maximum bolt force in operation
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DNV GL AS
49142 Proof against open gapThe following condition shall be met for the proof against open gap (see Figure 4-10)
FVmin = FMmin ndash ΔFSetz
FMmin = FMmaxαA
FVmin = lowest pre-stressing force of the boltFMmin = smallest installation forceαA = tightening factor of the tightening procedure used (see [48234])ΔFSetz = loss of pre-stressing force due to setting [N]
A 2-fold pre-stressing with time-lag reduces the setting to a residual value which may possibly bedisregarded
δs δp = resilience of the bolt and the tensioned structural elements according to [49132] [mmN]aers = distance between the compensating line of action from Fa and the bolt axis according to
[49131]feff = the smaller value of f or (dw + tf)geff = the smaller value of g or (dw + tf)
z = the smaller value of 0 or ((geff 2) - e) for g le dw + tf
the smaller value of 0 or (g - (geff 2) - e) for g gt dw + tf
In the case of through-bolt connections for tf the thickness of the thinner gusset plate shall be assumed inthe case of screw-in connections the thickness of the gusset plate with the through-bore
Minor one-sided gapping of the parting line is accepted in the above condition Large-area gapping of theparting line may be accepted if the bolt connection by means of measurement techniques or based onrecognized calculation procedures while considering the progressive increase of the bolt stress due toremoval of tensioned structural elements is proven separately
49143 Proofs of fatigue strengthIn the case of dynamic loads proof of fatigue strength of the bolts shall be conducted as stated in thefollowing
Stress range spectra shall be determined according to [46]
The maximum stress range of the normal stress Δσmax shall be determined according to [46] for the stresscross-section of the thread of the bolt
For a proof of fatigue strength of gaping bolt connections eg by numeric calculation methods Δσmax shallbe determined for the lowest prestress force of the bolt FVmin
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DNV GL AS
When the stress range of the normal stress Δσmax is calculated tensile and bending stresses in the stresscross-section of the thread of the bolt shall be taken into consideration For the bending stress in the cross-section of the threads stress cross-section the following applies
σb = bending stress in the stress cross-section of the thread of the boltds = shaft diameter of the bolt
The design S-N curves for proofs of fatigue strength of prestressed bolts are shown in Figure 4-11
The proof of fatigue strength may be conducted on the basis of calculated cumulative damage ratiosaccording to [46]
Alternatively the proof of fatigue strength may be conducted based on permissible stress ranges for thestandard spectra S0 to S7 according to [46] as follows
Δσmax le fnmiddot ksmiddot fimiddotΔσR
ks = 1 for d le 30 mm(30d)025 for d gt 30 mm
Δσmax = maximum stress range of the normal stress in the stress cross-section of the boltΔσR = reference value of the stress range of the normal stress at 2 middot 106 stress cyclesΔσR = 71 Nmm2 for bolts either tempered or rolled as final treatmentΔσR = 50 Nmm2 for all other boltsfn = factor for shape and extent of the spectrum according to Table 4-15fi = influence of importance of structural element according to Table 4-4ks = influence factor for sized = nominal thread diameter
Figure 4-11 Design S-N curves for prestressed bolts
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DNV GL AS
Table 4-15 Factor fn for standard stress range S0 to S7 according to [465] and design S-N curveaccording to Figure 4-11
Number of stress cycles nmaxStressspectrum 2middot104 5middot104 105 3middot105 6middot105 106 3middot106 6middot106 107 5middot107 108
S0 1654 1294 1068 784 644 555 406 333 287 182 151
S1 1263 970 787 568 461 397 284 229 195 123 103
S2 1025 775 623 443 357 304 215 172 146 089 076
S3 836 623 500 352 282 240 168 134 114 068 058
S4 693 516 412 288 230 195 136 108 092 054 046
S5 592 438 348 244 194 164 114 091 077 045 037
S6 513 378 302 209 166 140 098 078 066 039 031
S7 467 345 273 189 151 127 088 070 059 035 028
4915 Proof of transmissible forces in the clamping gapThe statements in [48234] apply where nr = 1Normally this proof shall not be conducted for the connection of large diameter slewing rings
49151 Proof of surface pressure below head and nut of boltThe statements in [48235] apply
49152 Construction and calculation of flanges491521 Construction
The dimensions a b and c in Figure 4-10 shall comply with the following requirements
mdash a mdash not larger than necessary for clamping toolsmdash b mdash sufficiently large for generating the supporting forcemdash c mdash sufficiently large for the weld including the excess length required for the welding process
ba ge 075
The workmanship of the weld next to the connecting bolts requires special diligence
491522 Calculation of flange thickness
The gusset thickness tf may simplified be calculated as follows
αe = coefficient for the construction of the wall50 for cylindric walls60 for flat walls
σw = existing stress in the wallσFzul = permissible stress in the flange according to [4422]
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DNV GL AS
492 Hydraulic cylinders4921 General notesFor compression and tension loaded hydraulic cylinders the following proofs shall be conducted for theoperating conditions loading gear in operation and loading gear out of operation
mdash proof of structural safety according to [44]mdash proof of fatigue strength according to [46]mdash proof of suitability for use according to [47]
4922 Simplified dimensioning of cylinder pipes
49221 For thin-walled cylinder pipes the required wall thickness twerf may be calculated as follows if therequirement according to [49222] is complied with
Da = outer diameter [mm]pc = setting pressure of the relief valves according to [10622] [bar]fyr = calculated yield strength according to [4332] [Nmm2]
49222 The formula in [49221] for the required wall thickness is based on the shear stress hypothesisTherefore the following condition shall be complied with if the cylinder pipe is dimensioned using thisformula
σ ℓ = longitudinal stress in the cylinder pipe (characteristic value without partial safety factor γp)
49223 The wall thickness tw of the cylinder pipe shall comply with the following requirement
tw = wall thickness of the cylinder pipetwerf = required wall thickness according to [49221]
49224 Cylinder pipes not complying with the condition according to [49222] shall be proven accordingto [44]In this case the partial safety factor for the internal pressure (= setting pressure pc of the safety valves) is
γp = 134
49225 A calculated strength analysis shall be conducted for the connecting welds of the pipes
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DNV GL AS
49226 In order to avoid local bending stresses the head and bottom plate of the cylinder pipes shall notfall below the following minimum thickness
tp = thickness of head or bottom plate respectivelytw = wall thickness of the cylinder pipe
4923 Notes regarding the proof of stability
49231 The proof of stability is according to [4423] to be conducted for the most unfavourablecombination of buckling length ℓki and respective pressure (depending on the kinematics of the loading gear)
49232 The dimensioning force shall include the partial safety factors γp as well as any dynamic coefficients(ψ) and shall be calculated for the most unfavourable load combination
49233 As an imperfection for the proof of stability a distortion of the hydraulic cylinder of ℓki 300 shall betaken into consideration
49234 At the ends of the cylinder the following moment shall be assumed due to friction of the carrierbolts
Nd = dimensioning force (pressure) in the hydraulic cylinder including the partial safety factors γp
micro = 008 (= friction coefficient)dB = bolt diameter
4924 Notes regarding the tensile stressesIn the case of tensile-stressed hydraulic cylinders particular attention shall be paid to the thread of thepiston rod during strength analysis
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DNV GL AS
493 Large cylindric pipes4931 Dimensions and loadsFigure 4-12 shows the dimensions and loads of circular cylinder shells
Figure 4-12 Dimensions and loads of circular cylinders
rm = radius related to the middle of wall thickness [mm]tw = Wall thickness [mm]
r = pipe length [mm]Da = outer diameter (nominal diameter) [mm]σx = longitudinal stress [Nmm2]τ = shear stress [Nmm2]σφ = circumferential stress [Nmm2]
49311 The longitudinal and shear stresses are calculated as follows
σx = longitudinal stress [Nmm2]τ = shear stress [Nmm2]Fx = force in x-direction [N]Fz = force in z-direction [N]Mz = bending moment [Nmm]Mx = torsional moment [Nmm]
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DNV GL AS
4932 Proofs of stability
49321 Proofs against buckling shall be performed according to [4423] Proofs against shell buckling maybe conducted according to EN 1993-1-6
49322 Regarding the application of the proofs of stability according to EN 1993-1-6 the following shall beobserved
mdash Instead of safety factor γM1 according to the Euro-code the value γm according to [43743] shall beused
mdash Instead of the yield strength the calculated yield strength fyr according to [4332] shall be used
49323 Proofs against shell buckling need not be conducted if the following requirements are compliedwith
a) pipes loaded by stress in circumferential direction 2
E = Youngs modulus [Nmm2]206 middot 105 Nmm2 for steel
ReH = yield strength according to material standards [Nmm2]
b) pipes loaded by compression in longitudinal direction
c) pipes loaded by shear
d) very long pipes loaded by compression
ℓki = buckling length of the pipe [mm]
49324 The requirements according to a) to d) apply provided that the imperfections according to[4933] are not exceeded during manufacture
2 These proofs apply provided that the edges are radially undisplacable
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DNV GL AS
4933 Imperfections due to manufacture
49331 CurvaturesIn the case of outward or inward curvatures caused by manufacture the depth gauge f according to Figure4-13 shall not exceed 1 of the smallest gauge length The following gauge lengths apply
mdash gauge length in longitudinal direction of the pipe [mm]
ℓm x = (in the unwelded area)
= (in the area of welds)
mdash gauge length in circumferential direction [mm]
ℓmφ = (in the unwelded area)
= (in the area of welds)
tmin = thickness of the thinner plate adjacent to the weld
Figure 4-13 Curvature including designations
49332 Out-of-roundness493321 The out-of-roundness is defined as follows
[]
Figure 4-14 Measurement of the diameters for determination of out-of-roundness
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DNV GL AS
493322 The permissible out-of-roundness Uadm may be calculated as followsUadm le 20 for dnom le 500 mm
Uadm le [] for 500 lt dnom lt 1250 mm
Uadm le 10 for dnom ge 1250 mmProof format U le Uadm
49333 Excentricities in x-directionPlanned eccentricities or eccentricities due to manufacture located at the centerline of joints of plates withequal or differing wall thickness tw shall not exceed the following values ex
ex le 02 middot tmin le 3 mm
tmin = the smaller of the two plate thicknesses
494 Shear connection of circular structural elementsRegarding the connection of circular masts posts and crane columns with eg deck plates the requiredplate thickness of the deck plating tp and the required weld thickness a may be determined according to thefollowing formula
[mm]
tp = required minimum thickness of deck platesa = required minimum thickness of weldD = connection diameter [mm] (Da or possibly Di)fyr = calculated yield strength according to [4332] [Nmm2]γm = partial safety factor for resistance values according to [43743] [-]Fz = maximum horizontal force to be transmitted [N]Mx = torsional moment of the connection [Nmm]
The internal forces Fz and Mx are dimensioning values and include the partial safety factors γp for loadsaccording to [4374]
Regarding the designation of axes see Figure 4-12
495 Local loads due to wheel loads4951 General notes
49511 Local loads due to wheel loads occur mainly with rails girders of crane rails and girders of trolleysStructural elements which are eg loaded by wheels of fork lift trucks shall be treated analogously
49512 Local loads shall be taken into consideration when the proof of structural safety according to [44]as well as the proof of fatigue strength according to [46] are conducted
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DNV GL AS
4952 Girders of crane rails
49521 For the calculation of the local compression stresses the relationships as shown in Figure 4-15apply
Figure 4-15 Pressure distribution of wheel loads
ℓd = length of pressure distribution [mm]= 2 middot hs + ℓf
hs = distance between contact area of the wheel and intersection line considered [mm]
f = length of contact area of the wheel [mm]= 02 middot rℓ le 50 mm
rℓ = running radius [mm]FR = wheel load [N]
49522 Regarding the connecting welds of crane rails made of square steel bars and welds joining web andflange it shall be assumed that the transmitted pressure takes place solely through the welds
4953 Girders of trolleys
49531 In Figure 4-16 typical local deformations are shown highly magnified
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DNV GL AS
Figure 4-16 Local deformation of girders of trolleys (highly magnified) F
FR = wheel loadσx σy = local and global stresses
49532 Calculation of local stresses in the lower flanges of girders for trolleys may be conducted inaccordance with a recognized calculation method or standard
mdash Federation Europeenne de la Manutention (FEM) Section IX book 9341
49533 For general strength analysis local and global stresses shall be superimposed with the localstresses reduced to 75
49534 In the case of lower flanges welded to the web for the connecting weld a proof of fatigue strengthmay possibly be required
496 Bolt connections
4961 Bolts shall be secured against falling out Outer bearing plates and gussets shall be secured againstgapping
4962 Bolt connections shall be proven according to [482]
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DNV GL AS
497 Eye plates and eye rods
4971 Proof of eye plates may be conducted according to [7343]
4972 Eye rods according to Figure 4-17 may be dimensioned as follows
F = dimensioning value of the tensile force (including partial security factor γp according to [4374])
fyr = calculated yield strength according to [4332]γm = partial safety factor for resistance values according to [43743]
Figure 4-17 Example of an eye rod
498 Joints of hollow profile girdersDimensioning of hollow profile girder joints may be performed according to EN 1993-1-8Alternatively a shape strength analysis for the joints of hollow profiles to other hollow profiles or openprofiles may be conducted based on another recognized calculation method
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DNV GL AS
499 Stairs ladders platforms and railings4991 Load assumptions
49911 Accesses platforms etc shall be dimensioned for a distributed load of at least 3000 Nm2 or for amovable single load of 1500 N
49912 Guard-rails and toe boards shall be dimensioned for a lateral load in the form of a movable singleload of 300 N
49913 The loads according to [49911] and [49912] need not be considered for the global calculationof lifting appliances
4992 Proof of structural safety
49921 Proof of structural safety shall be conducted according to [44]
49922 The partial safety factor for the loads is γp = 134
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DNV GL AS
SECTION 5 CRANES AND SUPPORTING STRUCTURES
51 General
511 Description of contents
5111 This section contains requirements for design and dimensioning of cranes and their supportingstructures onboard ships which are also correspondingly applicable to other lifting appliances and theirsupporting structures according to Sec1 [131]
5112 The type of design is not subject to restrictions However the requirements given in [57] shall betaken into account
5113 The dimensioning is based on Sec4 and distinguishes between the conditions in service and out ofservice for all proofs
512 Influences caused by the ship and the shiprsquos operation
5121 Apart from special tasks such as eg handling of hatch covers or offshore activities the shiprsquosinfluence shall also be considered for the design and dimensioning of cranes on board ships predeterminedeg by the form of the hull its bending and torsional stiffness or the shiprsquos operationPossible influences to be considered may be
mdash arrangement of the cranes on the shipmdash stability of the shipmdash area of operation of the shipmdash high ship speedmdash sea lashing of the cranesmdash special operating conditions
5122 The increase of load radius of cranes due to the existing heel of the ship andor the heel generatedby the lifting of load may be taken advantage of upon approval by the Society The values of Table 4-1 shallbe complied with
513 Dimensioning of cranesThe cranes listed in the following shall be dimensioned according to different criteria
5131 Shipboard cranes
51311 Cranes for harbour operation
51312 Cranes for sea operation
5132 Floating cranesDepending on their use floating cranes shall be dealt with like shipboard cranes for harbour or sea operationrespectively
5133 Lifting appliances not handling cargoShipboard lifting appliances not handling cargo shall be dealt with like shipboard cranes for harbouroperation taking into consideration their service or environmental conditions
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DNV GL AS
514 Dimensioning of supporting structures
5141 The principal supporting structures are
mdash crane columnsmdash crane foundationsmdash runways for mobile cranesmdash crane boom supportsmdash structural transits into the shiprsquos hull
5142 Crane columns and crane foundations shall be dimensioned similarly like the allocated cranes whereapplicable also according to [5412]
5143 When dimensioning runways the requirements given in [495] as well as according to [5744]shall be observed
5144 Crane boom supports shall be dimensioned according to [566]
52 Crane groups
521 General notes
5211 The allocation to crane groups may be of influence on the determination of hoist load coefficientsthe main aspect however is the fatigue strength
5212 Non-distinct allocations shall be agreed with the Society This applies in particular to side andauxiliary hoists
5213 The following allocations to crane groups in each case refer to the main hoist of a crane
522 Crane group A
5221 Crane group A includes mainly cranes which do not handle cargo and which with the exceptionof hatch cover cranes and hose cranes are not always exposed to the full nominal load Such cranes arecharacterized by irregular use and longer rest periods
5222 Cranes of group A1 which also launch and recover life-saving appliances shall be dimensioned inaddition according to the LSA-Code
5223 Crane group A is further subdivided as follows
52231 Crane group A1 includes cranes for the operation of the ship in the harbour such as eg
mdash provision cranesmdash engine room cranes workshop cranesmdash hatch cover cranesmdash hose cranes
52232 Crane group A2 includes cranes for the operation of the ship at sea such as eg
mdash service cranesmdash engine room cranes (used at sea state)
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DNV GL AS
52233 Crane group A3 includes floating cranes not used for cargo-handling like eg
mdash mounting cranes
523 Crane group B
5231 Crane group B primarily includes cranes used for cargo-handling and which are not always exposedto the full nominal load These cranes are characterized by regular use and longer rest periods
5232 Crane group B is further subdivided as follows
52321 Crane group B1 includes shipboard cranes for cargo-handling in the harbour using spreaders orhooks such as eg
mdash container cranesmdash general cargo cranes
52322 Crane group B2 includes cranes for cargo-handling at sea using hooks such as eg
mdash general cargo cranes
52323 Crane group B3 includes floating cranes for cargo-handling using hooks such as eg
mdash floating cargo cranes
524 Crane group C
5241 Crane group C primarily includes cranes for cargo-handling and which are regularly exposed to thefull or nearly full nominal load
5242 Crane group C is further subdivided as follows
52421 Crane group C1 includes shipboard cranes for cargo-handling in the harbour using grabs hooks orspecial loose gear such as eg
mdash grab cranesmdash pallet cranes
52422 Crane group C2 includes ship cranes for cargo-handling at sea using grabs such as eg
mdash grab cranesmdash lighter cranes
52423 Crane group C3 includes floating cranes for cargo-handling using grabs such as eg
mdash grab floating cranesmdash lighter floating cranes
525 Change of crane group
5251 In the cases of a change of crane group change to the nominal load or change to the load radiusin addition to an examination of drawings the manufacturer shall calculate the estimated residual lifetimewhere applicable
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DNV GL AS
53 Design loads
531 General notes
5311 The loads acting on the structural components of cranes and their supporting structures aresubdivided as follows
mdash regular loadsmdash irregular loadsmdash special loads
5312 Cranes for the conveyance of persons shall comply with the requirements given in [4251] and[4252]
5313 If necessary loads not addressed in the following shall be properly taken into account The rating ofsuch loads and considering them in the corresponding load combinations shall be agreed with the Society
532 Regular loads5321 Dead loads LDead loads shall be determined in accordance with [4242] A distinction should be made between loadingand unloading dead loads acting on each structural element
5322 Hoist load LThe definition of hoist load (working load) is given in [11562] Regarding the crane dimensioning thenominal load shall be regarded as part of the hoist loadDepending on the type of operation the following hoist loads exist
mdash harbour operation LH = (LEA + LNe)mdash sea operation LHsee = (LEA + LNsee)
LNsee shall be calculated according to [54321]
5323 Loads from driving over an uneven runwayWhere the design conditions according to [5744] are met the application of vertical dynamic forces causedby driving over an uneven runway may be omitted Or else the application of the load shall be agreed withthe Society
5324 Dynamic forces due to drive systems
53241 General notes532411 The dynamic forces to hoist loads and to components of lifting appliances caused by drivesystems may be determined in a simplified manner using the method described in the following The set-down of a load corresponds arithmetically to the lifting of a resting load and is not mentioned explicitly in thefollowing532412 The designations vertical and horizontal refer to the coordinate system of the cranes
53242 Vertical dynamic forces due to lifting of a load532421 The acceleration forces generated by the lifting of a resting load during harbour operation areallowed for by using the hoist load coefficient ψ to be determined according to [5431]532422 The acceleration forces generated by the rising of a resting or moving load during sea operationare allowed for by using the hoist load coefficient ψsee to be determined according to [5432]
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DNV GL AS
Guidance noteThe hoist load coefficients ψ and ψsee are abbreviated as DAF in GL Noble Denton guideline 0027ND - Guidelines for Marine Liftingamp Lowering Operations
---e-n-d---o-f---g-u-i-d-a-n-c-e---n-o-t-e---
53243 Vertical dynamic loads due to suspended loadGenerally for a suspended load no lifting or braking forces need to be considered This also applies forbraking a crane boom with suspended load
53244 Horizontal dynamic forces due to lifting of a load532441 In the case of lifting a resting load during harbour operation the horizontal components of theload LH middot ψ resulting from the shiprsquos heeling angle according to Table 4-1 shall be assumed as horizontaldynamic forces see also [53262]532442 In the case of lifting a resting or moving load during sea operation the horizontal componentsof the loads LHsee middot ψsee or LHu middot ψu resulting from the shiprsquos heeling angle according to Table 4-1 and thecargo runner deflection angle according to [53263] shall be assumed as horizontal dynamic forces
53245 Horizontal dynamic forces due to suspended load532451 The accelerations at the crane boom peak due to rotating slewing pivoting and telescopingmotions shall be indicated by the manufacturer
532452 If no other proof is given the radial acceleration br for rotating and slewing cranes may becalculated as follows
ω = (π middot n) 30 = angular speed [1s]
r = rotatingslewing radius [m]v = ω middot r = circumferential speed [ms]n = rpm [1min]
In the case of rotating cranes for hoists on the ship or on the installation half of the circumferential speedmay be assumed
532453 In the case of rotating or slewing cranes the tangential acceleration bt may be assumed to beequal to the radial acceleration br according to [532452] if no other proof is given
532454 The horizontal forces of the useful load and the dead load of the crane boom due to the shipacutesheeling ε and the rotating or slewing acceleration may be added vectorially For ε see [424414]
53246 Horizontal dynamic forces with mobile cranesHorizontal dynamic forces caused by starting and braking in the direction of travelling shall be indicated bythe manufacturer If such manufacturerrsquos information is not available at least 16 of the loads of powered orbraked wheels shall be assumedThe wheel loads are calculated from the dead loads of the crane and the hoist load Oscillatingly suspendedhoist loads may be disregardedIn the case of an off-center location of the center of gravity the horizontal side forces which occursimultaneously shall be considered as well
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DNV GL AS
5325 Dynamic forces generated by ship motions
53251 General noteThe following requirements apply exclusively for the dead loads LE of cranes For a more accuratedetermination of the dynamic forces the requirements given in [547] apply
53252 Cranes in service532521 Vertical dynamic forcesGenerally vertical dynamic forces during operation of cranes at sea need not be allocated any loadcombination according to [552] and they also need not be explicitly proven532522 Horizontal dynamic forces due to the inclination of the crane baseFor the sea operation of cranes the horizontal forces resulting from the ship inclinations according to Table4-1 may be assumed unless not deviant indicated by the operatorThe inclination of the crane base may be considered to be an obliquely positioned system or by distribution ofthe forces into components532523 Horizontal dynamic forces due to the acceleration of the crane basisFor the sea operation of cranes in addition to the horizontal forces according to [532522] the followinghorizontal accelerations bh shall be assumed if cranes are operated at significant wave heights of H13 gt 2m
mdash barges and catamarans bh = 075 middot (H13 ndash 2) ge 0 [ms2]mdash shipsmdash bh = 05 middot (H13 ndash 2) ge 0 [ms2]mdash semi-submersibles bh = 025 middot (H13 ndash 2) ge 0 [ms2]
H13 = significant wave height [m]
53253 Cranes out of serviceIn the condition out of service at sea the vertical and horizontal dynamic forces may be calculatedaccording to AppA
5326 Diagonal pull forces due to cargo runner deflection angles
53261 General notes532611 Diagonal pull forces may be generated when a load is hoisted due to a relative shift betweenload and crane boom peak They shall be superimposed to the ship inclinations of Table 4-1532612 Cargo runner deflection angles in the longitudinal and transverse direction of a crane boom shallbe considered as occurring simultaneously in the dimensioning process
53262 Harbour operationIn general diagonal pull forces due to cargo runner deflection angles need not be taken into considerationduring harbour operation
53263 Sea operation532631 Shipboard cranes
When not determined more precisely the cargo runner deflection angle shall be assumed as
φl = φq = H13 [deg]
φl = deflection angle in longitudinal direction of the crane boomφq = deflection angle in transverse direction of the crane boomH13 = significant wave height [m]
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DNV GL AS
For cranes with a slewing mechanism the deflection angle in transverse direction may be halved if therequirement given in [573212] is met
532632 Floating cranes
For floating cranes with a nominal load LNe le 60 t the requirements given in [532631] apply In the caseof higher nominal loads the requirements given in [57322] shall be met additionally
5327 Partial dropping of the useful load during normal operation
53271 When a part of the useful load LN is dropped during normal operation as eg by cranes with grabsor load magnets this may be accounted for by application of a dropping factor fa
53272 The load FSa which shall be used for dimensioning see Figure 5-1 shall be calculated as follows
FSa = fa middot LN
fa = 1 ndash (1 + φ) middot
φ = 05 for grabs or slow load dropping= 10 for load magnets or fast load dropping
Figure 5-1 Dropping of a part of the useful load
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DNV GL AS
Figure 5-2 Hoist load torn off (see
53273 When the dropping factor is fa lt 0 the load FSa may become negative as well This corresponds toa load directed upwards
5328 Tie-down force of the cargo hooksWhen cargo hooks are tied-down for the load condition crane out of service this load shall be considered asthe tie-down force This load shall be indicated by the manufacturer If no information is available this loadmay be assumed to be 10 of the nominal load LNe
533 Irregular loads5331 Wind loadsWind loads shall be assumed according to [4245]The total wind load acting on a crane structure is the sum of the single wind loads acting on its variousstructural components
5332 Snow and ice loadsFor snow and ice loads the requirements given in [4246] apply
5333 Temperature loadsFor temperature loads the requirements given in [4247] apply
5334 Side forces when driving (diagonal drive)
53341 The side forces occurring when the crane or trolley is being driven shall be taken into consideration
53342 When 2 wheels or wings are mounted for 1 rail the two forces generated by one-sided guidancemay be calculated by multiplying the wheel or wing load with the side force coefficient γSk according to Figure5-3 The side force coefficient γSk depends on the ratio between span bs and wheel spacing ℓr
53343 Two-sided guidances or more than 2 wheels or wings on 1 rail shall be considered separately
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DNV GL AS
Figure 5-3 Side force coefficient γ
534 Special loads5341 Dynamic test loadsThe dynamic test loads LPdyn for cranes shall be taken from Table 13-2 The hoist load coefficient ψ may bereduced using the following formula
ψP = (1 + ψ) 2
5342 Buffering forces
53421 At the ends of carriage ways of cranes and trolleys arrestors shall be mounted with buffersattached either to them or to the cranesBuffers shall be dimensioned such that they are capable to absorb 70 of the kinetic energy of the loadinggear driving at maximum speed The mass of oscillatingly suspended hoist loads are not considered
53422 The impact force on the buffer shall be determined from the buffer characteristic and - in order totake into consideration the dynamic effect of the buffering force - to be multiplied with the following factor fp
fp = 125 for buffer with linear characteristic= 160 for buffer with rectangular characteristic
53423 Lower speeds than according to [53421] may be assumed if reliable (redundant) appliancesreduce the speed in way of the runway ends
5343 Loads on stairs ladders platforms and railingsFor access loads see the requirements given in [499]
5344 Loads due to safety systemsThe loads LS due to safety systems such as eg
mdash AOPS (Automatic Overload Protection System)mdash MOPS (Manual Overload Protection System)mdash ELRS (Emergency Load Release System)
shall be indicated by the crane manufacturer
5345 Tear-off of the hoist loadIn the catastrophic case of the hoist load torn off this results in fa = - 1 according to [53272] and Figure5-2 fa and with this the calculated load directed upwards becomes minus LH
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DNV GL AS
54 Hoist load coefficients
541 General notes
5411 The hoist load or the loads resulting from it shall be multiplied with an allocated hoist load coefficientfor the lifting of the resting load If the crane has several hoisting appliances or differing hoisting speedsindividual hoist load coefficients shall be allocated to each of them
5412 For the strength analysis of load-bearing structural elements as far as its fastening to the ship hullreduced hoist load coefficients may be applied if the corresponding dampening in the load-bearing system isproven by calculation or measurement
542 Hoist load coefficient ψ as a function of crane group and hoistingspeed
5421 For harbour operations the hoist load coefficient may be simplified taken from Table 5-1
5422 An individual calculation of the hoist load coefficient according to [543] may be necessary oradvisable
Table 5-1 Hoist load coefficient for different crane groups
Crane-group Hoist load coefficient ψ ψmin
A1 105 + 034 middot vh 117
B1
C1 115 + 051 middot vh 135
For descriptions of crane groups see [522] to [524]vh acc to Table 5-2
Table 5-2 Hoist load coefficient for different crane groups
Lifting gear type and hoisting speed vhLoad combination
HD 1 HD 2 HD 3 HD 4
LK I + LK II vhmax vhF vhF 05vhmax
LK III 1 minus vhmax minus vhmax
1) For lifting gear types HD 2 and HD 4 the hoist load coefficient ψ calculated from vhmax shall be proven as loadcombination III1
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DNV GL AS
HD 1 = creep hoist not possibleHD 2 = creep hoist selectable by the crane driverHD 3 = creep hoist switched on automatically until the load is lifted from the groundHD 4 = hoisting speed is infinitely variable by the crane drivervhmax = maximum constant hoisting speed of the allocated load [ms]vhF = constant creep hoisting speed [ms]
543 Calculation of the hoist load coefficient ψ as a function of the cranestiffness5431 Harbour operation
54311 Calculation of the hoist load coefficient ψThe hoist load coefficient shall be calculated as follows
ψmin = minimum value according to Table 5-1vh = hoisting speed in the course of lifting of the nominal load according to Table 5-2 [ms]cs = crane stiffness according to [5433] [kNm]LNe = nominal load [t]
54312 Simplified calculation for jib cranes with hoisting and luffing ropesIn the case of jib cranes with hoisting and luffing ropes only the hoisting and luffing ropes as well as thecrane boom need to be included in the simplified calculation The hoist load coefficient ψ is then calculated asfollows
5432 Sea operation
54321 Calculation of the hoist load coefficient ψ
vr = relative speed between load and hook in the course of lifting the load [ms] according to[54322]
cs = crane stiffness [kNm] according to [5433]LNsee = nominal load at sea [t]ψ = hoist load coefficient for harbour operation
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DNV GL AS
With the exception of cranes dimensioned only for sea operation the following condition shall be observed
LNe middot ψ ge LNsee middot ψsee
54322 Relative speed between load and hookvr = 05 middot vh + vsee [ms] for LCI [55211]
vr = vh + vsee [ms] for LCIII [55231]
vh = hoisting speed in the course of lifting the respective nominal load LNsee according to Table 5-2 [ms]
The minimum hoisting speed according to [57311] shall be taken if larger than vh
vsee = speed induced by seastate according to Table 5-3
Table 5-3 Speed induced by seastate v
From thelocationof thecrane(va)
to the cargo deck or to the sea surface (vd)
Fixedinstallation
Semi-submersible FSO FPSO Large barge Small barge Supply ship Sea surface
Fixedinstallation 0 025middot(H13)
075 032middot(H13)075 038middot(H13)
075 050middot(H13)075 070middot(H13)
075 085middot(H13)067
Semi-sub-
mersible025middotH13 035middot(H13)
090 040middot(H13)088 047middot(H13)
087 060middot(H13)083 073middot(H13)
080 090middot(H13)070
FSOFPSO 040middotH13 045middotH13 053middot(H13)
088 062middot(H13)090 070middot(H13)
090 080middot(H13)087 (H13)
078
Largebarge 060middotH13 065 middot H13 070middot(H13)
094 075middot(H13)094 085middot(H13)
094 090middot(H13)094 120middot(H13)
080
Smallbarge 110middotH13 111 middot H13 116middot(H13)
094 118middot(H13) 097 120middot(H13)
097 130middot(H13) 094 140middot(H13)
091
va = vertical speed of the crane boom peak [ms]
vd = vertical speed of the cargo deck or sea surface [ms]
H13 = significant wave height [m]
5433 Calculation of the crane stiffness cs
54331 Principals of calculation544311 The stiffness of a crane depends on the load radius and the height of the load hook
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DNV GL AS
544312 For calculation of the crane stiffness besides the ropes all load-bearing structures as far asthe fastening of the crane column or the crane base shall be taken into consideration with the exception of[54312]544312 Regarding the approach of the rope stiffness the Youngacutes modulus indicated by the ropemanufacturer shall be taken
54332 Permissible simplification for the calculation543321 For round strand ropes without a more precise proof a Youngrsquos modulus of 10 middot 105 Nmm2based on the gross cross-section may be taken543322 Curve-shaped load gradingIn the case of a uniform curve-shaped useful load vs load radius diagram the crane stiffness shall becalculated at least for the end points and the one-third points of the regarded range of load radius Based onthese values a continuous curve may be determined543323 Step-shaped load gradingIn the case of a step-shaped grading of the useful load vs load radius diagram the stiffness shall becalculated for each load level according to [543322] As an alternative the stiffness may be calculated forthe minimum load radius of each load level These values apply then for the whole range of one level543324 Height of the cargo hookFor operations in harbour conditions it may be assumed that the cargo hook is at the altitude of the craneboom pivot point For operations in seastate conditions it may be assumed that the cargo hook is 6 m abovethe water surface except for underwater operations
544 Calculation of the hoist load coefficient for hoists onboard the shipFor hoists onboard the ship the simplified hoist load coefficient for sea operations may be assumed to be
ψsee = 115 + 051 middot vh ge ψ
vh = hoisting speed in the course of lifting the nominal load according to Table 5-2 [ms]ψ = hoist load coefficient for harbour operation
545 Calculation of the hoist load coefficient for auxiliary hoistsThe hoist load coefficient for auxiliary hoists is calculated (simplified) to be
ψ = 120 + 068 middot vh ge ψmin = 145
546 Calculation of the hoist load coefficient by means of hydrodynamicanalysis
5461 Using model tests or stochastic and hydrodynamic calculation methods the hoist load coefficient canbe determined more accurate These methods generally apply for all service conditions of the crane
5462 The calculation shall be performed under consideration of the motion behavior of the floating bodiesinvolved and the stiffness of the crane Influences of special appliances such as rope-spindling devices orheave compensators may be taken into account in the process
5463 The calculation shall include at least the following influences if applicable
mdash vertical and horizontal motions of the cargo deckmdash motion behavior of the floating body on which the crane is mountedmdash load-bearing structure of the cranemdash hydrodynamic properties of a floating or submerged load
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DNV GL AS
mdash influence of anchoring systemsmdash environmental conditions agreed
5464 The calculation shall be submitted to the Society for the examination of the crane as a document forinformation In particular the influences listed in [5463] shall be represented clearly in the document
55 Load combinations and partial safety factors
551 General notes
5511 The load combinations regarded as essential for cranes and their supporting structures are listed inthe Table 5-4 (Cranes in service) and Table 5-5 (Cranes out of service)Further load combinations may be relevant if necessary
5512 Only those load combinations from Table 5-4 Table 5-5 and further load combinations if necessarywhich are essential or necessary for the actual structural element under consideration shall be verified
5513 Regarding load combinations for operation at sea instead of ψ the hoist load coefficient ψsee forunderwater operations the hoist load coefficient ψu shall be taken
5514 The load combinations for the proof of stability against overturning are listed in Table 5-6
5515 The partial safety factors γpi shall be taken from Table 5-4 to Table 5-6
552 Explanations regarding load combinations for cranes in serviceaccording to5521 Load combinations IThe load combinations I include regular loads in normal service
55211 I ndash Lifting and setting-down of the nominal loadAll regular loads which occur during lifting and setting-down of a load shall be superposed as required forthe load combination I1For vertical and horizontal dynamic forces the requirements given in [5324] and [5325] apply
55212 I ndash Suspended loadAll regular loads which are generated by acceleration and deceleration forces of lifting gear luffing gear andtravelling gear when a load is positioned shall be superposed as required for the load combination I2 takinginto consideration static ship inclinations and possible diagonal pull
5522 Load combinations IIThe load combinations II include regular loads during normal service combined with non-regular loads
55221 II ndash Load combination I with wind loadsLoad combination II1 results from load combination I1 plus appropriate wind loads Snow ice oretemperature loads are only to be assumed upon agreement
55222 II ndash Load combination I with wind loadsLoad combination II2 results from load combination I2 plus appropriate wind loads Snow ice oretemperature loads are only to be assumed upon agreement
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DNV GL AS
55223 II ndash Constant drive including diagonal pullFor load combination II3 all loads shall be superimposed as required which occur at constant drive includingdiagonal pull Snow ice or temperature loads are only to be assumed upon agreement
5523 Load combinations IIILoad combinations III include special load combinations
55231 III ndash Hoisting of the nominal load at maximum hoisting speedComplementing load combination I1 load combination III1 includes operating errors during hoisting of theload The hoist load coefficient shall be determined for the maximum possible hoisting speed relative speedbetween load and hook and the respective load level
55232 III ndash Test loadsLoad combination III2 includes hoisting of the dynamic test load at 20 wind load
55233 III ndash Buffer forcesLoad combination III3 comprises the impact of a crane with hoist load against the end buffers
55234 III ndash Safety systemsLoad combination III4 comprises loads which may result from activated safety systems
55235 IIIndash Failure of hydraulic cylinderLoad combination III5 contains special load combinations covering a cylinder failure of a lifting applianceconveying persons
553 Explanations regarding load combinations for cranes out of serviceaccording to5531 Load combination ILoad combination IA includes regular loads for cranes out of service
55311 I ndash Combination of regular loadsFor load combination IA1 all regular loads shall be superimposed as required
5532 Load combination IIILoad combination IIIA includes special load combinations for cranes out of service
55321 III ndash Special load combinationFor load combination IIIA1 the wind loads out of operation shall be superimposed with the regular loads asrequired Snow ice or temperature loads are only to be assumed as non-regular loads upon agreement
Standard mdash
DN
VG
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ay 2016Page 114
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DN
V G
L AS
Section 5
Table 5-4 Load combinations and partial safety factors for cranes in service
Load Combinations
I II IIILoadcate-gories
Loads i Reference
γpi I1 I2 γpi II1 II2 II3 γpi III1 III2 III3 III4 III5
Dead loads LE (including inclination ofcrane base) 1 4 321 122 1 10 10 116 1 10 10 10 1101 102 10 10 10 10
Hoist load LH 6(including inclination of
crane base) 2 4 322 134 ψ 10 122 ψ 10 10 110 mdash mdash 10 mdash 10
Dynamic forces due to drives 3 3 4 324 134 mdash 10 122 mdash 10 mdash mdash mdash mdash mdash mdash mdash
Regu
lar
load
s
Diagonal pull 4 4 326 134 ψ 10 122 ψ 10 mdash mdash mdash mdash mdash mdash mdash
Wind loads in operation 5 4 331 122 10 10 10 110 mdash 02 mdash mdash 10
Snow and ice loads 6 4 332 122 10 10 10 mdash mdash mdash mdash mdash mdash
Temperature loads 7 4 333 116 10 10 10 mdash mdash mdash mdash mdash mdash
Non
-reg
ular
load
s
Side forces during drive
8 4 333 116 mdash mdash 10 mdash mdash mdash mdash mdash mdash
Hoisting of hoist load at vhmax 9 4 Table5-2 110 ψmax mdash mdash mdash mdash
Dynamic test load Lpdyn(includinginclination of crane base) 10 4 341 110 mdash ψp mdash mdash mdash
Buffing forces 11 4 342 110 mdash mdash 10 mdash mdashSpe
cial
load
s
Loads caused by safety systems 4 5 12 4 344 110 mdash mdash 10 mdash
Drag coefficient γm 110 110 110
Global safety coefficient γs 148 134 122
Standard mdash
DN
VG
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ay 2016Page 115
Standard for shipboard lifting appliances
DN
V G
L AS
Section 5
Load Combinations
I II IIILoadcate-gories
Loads i Reference
γpi I1 I2 γpi II1 II2 II3 γpi III1 III2 III3 III4 III5
1) When load components have a favourable effect γpi = 095 If masses and centres of gravity are determined by weighing 095 middot γpi may be assumed2) Components caused by inclination of crane base may be neglected3) Applicable for load components from dead load and hoistload4) Emergency stop shall be verified by a practical test with a test load of LPdyn see Sec11 [24223]5) Loads which may be generated by activated safety systems shall be indicated by the manufacturer6) For load combination III5 LH = SWL (M)
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DNV GL AS
554 Explanations regarding load combinations for the proof of stabilityagainst overturning according to5541 Load combination ILoad combination I includes regular loads under normal operation
55411 I- Combination of regular loadsFor load combination I1 all regular loads shall be superimposed as necessary
5542 Load combination IILoad combination II includes regular loads in normal operation together with non-regular load
55421 II - Load combination I with wind loadsLoad combination II results from load combination I plus allocated wind loads
5543 Load combination IIILoad combinations III comprise special load combinations
55431 III - Test loadsLoad combination III1 considers the hoisting of the dynamic test load at a 20 wind load
55432 III - Buffer forcesLoad combination III3 comprises the impact of a crane with hoist load against the end buffers
Table 5-5 Load combinations and partial safety factors for cranes out of service
Load combinations
IA IIIALoadcategories Loads i Reference
γpi IA1 γpi IIIA1
Dead loads LE 1 4 321 122 1 10 110 1 10
Dynamic forces due to ship motions 2 4 3253 134 10 110 10Regular loads
Tie-down force of the cargo hook 3 4 328 122 10 110 10
Snow and ice loads 4 4 332 110 10Non-regularloads Temperature loads 5 4 333 105 10
Special loads Wind loads out of operation 6 3 331 110 10
Drag coefficient γm 110 110
Global safety coefficient γs 148 122
1) Where load components have a favorable effect γpi = 095
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DNV GL AS
Table 5-6 Load combinations and partial safety factors for proof of stability against overturning
Load combinations
I II IIILoadcategories Loads i Reference
γpi I1 γpi II1 γpi III1 III2
Dead loads LE (including inclinationof the crane base) 1 4 321 110 1 10 110 1 10 110 1 10 10
Hoist load LH (including inclinationof the crane base) 2 4 322 134 10 122 10 110 minus 10
Dynamic forces due to drives 2 3 4 324 134 10 122 10 110 minus 10
Regular loads
Diagonal pull 4 4 326 134 10 122 10 minus minus minus
Non-regular loads Wind loads in operation 5 4 331 122 10 110 02 10
Dynamic test load Lpdyn (includinginclination of the crane base) 6 4 341 116 10 minus
Special loads
Buffer forces 7 4 342 110 minus 10
1) Where load components have a favourable effect γpi = 0952) Applicable for load components from dead load and hoist load
56 Proofs
561 General
5611 The following proofs shall be conducted for all structural elements connections and supportingstructures of cranes for the conditions in service and out of service
mdash strength analysis according to [44] and [48]mdash proof of stability according to [44]mdash fatigue strength analysis according to [46]
5612 The following proofs shall be conducted for a complete crane as required
mdash proof of stability against overturning according to [45]mdash proof of suitability for use according to [47]
5613 For the proof of crane boom supports and rectan-gular crane columns the requirements given in[566] and [567] apply
562 Strength analyses and proofs of stability
5621 Strength analyses and proofs of stability shall be conducted using the partial safety factors of Table5-4 or Table 5-5 respectively for the load combinations of [55]
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 118Standard for shipboard lifting appliances
DNV GL AS
563 Fatigue strength analyses
5631 In general fatigue strength analyses shall be conducted for the load combination I of Table 5-4 andTable 5-5 with the partial safety factors γpi = 10As a basis for dimensioning regarding fatigue strength analyses the crane manufacturer shall provide loadcycles and the respective load spectrum (see also Table 5-7)
Table 5-7 Load spectra and load cycles (examples for a service life of 20 years) for ships andfloating cranes in harbour operation
Crane groupacc to [52] Crane type
Load spectrumacc to Sec4
[465]No of load cycles
Hatch cover crane
Engine roomworkshop crane
Provision crane
S6
S2
S2
20000
10000
20000
A1
Cranes operatingon ships
Hose crane S6 50000
A3
Floating cranes
Mounting crane SWL le 60 t
Mounting crane 60 t lt SWL le 500 t
Mounting crane SWL gt 500 t
S2
S3
S4
80000
50000
20000
B1
Ship cranes
Container crane SWL le 60 t
General cargo crane SWL le 60 t
General cargo crane 60 t lt SWL le 250 t
General cargo crane 250 t lt SWL le 500 t
General cargo crane SWL gt 500 t
S3
S2
S3
S4
S4
350000
250000
100000
70000
50000
B3
Floating cranes
Cargo-handling crane SWL le 60 t
Cargo-handling crane 60 t lt SWL le 250 t
Cargo-handling crane 250 t lt SWL le 500 t
Cargo-handling crane SWL gt 500 t
S2
S3
S4
S4
300000
125000
80000
60000
C1
Ship cranes
Grab crane SWL le 60 t
Gab crane SWL gt 60 t
Pallet crane
S5
S5
S6
600000
450000
600000
C3
Floating cranes
Grab crane SWL le 60 t
Grab crane SWL gt 60 t
Lighter crane
S5
S5
S5
700000
500000
2000000
5632 For cranes with load cycle numbers le 20000 a fatigue strength analysis may be dispensed with
5633 The fatigue strength analysis for the condition out of service shall be conducted for a load cyclenumber of 5 middot 107 This assumes a straight-line spectrum A according to Figure 4-3
5634 Superposition of in service and out of serviceA superposition of the fatigue damage due to the conditions in service and out of service is not necessaryas long as the maximum stress in the condition out of service does not exceed 10 of the maximum stress
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 119Standard for shipboard lifting appliances
DNV GL AS
in the condition in service Or else the load spectrum applicable for the analysis and the allocated load cyclenumbers shall be agreed with the Society
564 Proof of stability against overturning
5641 The proof of stability against overturning shall be conducted with the partial safety factors and loadcombinations according to Table 5-6 unless not shown in practice see [45213]
565 Proof of suitability for use5651 Proof procedures
56511 Proofs of suitability for use may be performed in the course of the initial testing on boardmathematically or as a combination of both procedures
56512 In general the mathematical proof of suitability for use shall be conducted for the load combinationI according to Table 5-4 and Table 5-5 using partial safety factors γpi = 10
5652 Proof of permissible deflection of crane boomsThe maximum deflection of pressure-loaded crane booms shall correspond to the crane boom length dividedby 350 if the dead weight alone is considered and to the crane boom length divided by 250 if dead weightplus hoist load are consideredThe peak of crane booms under bending stress which are held by luffing cylinders shall in general not exceeda vertical lowering of the maximum crane boom length divided by 100
5653 Proof against remaining in the highest crane boom position
56531 Where no restoring or warning devices according to [1221122] are provided a proof ofsuitability for use shall be shown for crane booms handled by luffing ropes under the following boundaryconditions
mdash dead load coefficient φe = 095 for all load components of the crane boom unless they are confirmed byweighing Else φe = 10
mdash static ship inclinations according to Table 4-1mdash hoist load coefficient ψ = 10mdash wind load acting unfavourably calculated from 80 of the mean dimensioning wind speed in service
according to [4245]mdash consideration of all friction and guide losses
56532 For crane booms handled by cylinders the requirements given in [122113] apply
566 Proof of crane boom supportsCrane boom supports shall be proven for the load combinations in Table 5-5 and the allocated partial safetyfactors In addition the following shall be observed
mdash The dead load also includes the dead load component of the crane boommdash Where a relative movement is possible between the crane boom and the crane boom support additionally
an alternating friction force shall be considered with a friction coefficient of at least μ = 015mdash tie-down force of a cargo hook (see [575])
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 120Standard for shipboard lifting appliances
DNV GL AS
567 Proof for rectangular crane columnsA general strength analysis shall be conducted regarding the maximum corner stress This is done byallocating the maximum crane moment MKmax to the main axes of the crane column in the most unfavourabledistribution
57 Requirements for design and equipment
571 General noteThe following statements complement the requirements given in this and other sections of this standardStructural elements details of equipment and design which are not covered shall be dealt with according tothe Generally recognized rules of good practice
572 Supporting structures5721 Design requirements for crane columns
57211 Access to cranesRegarding the accesses to cranes inside or outside of crane columns the statements in [10622] and[12214] apply
57212 Notes on design and calculation572121 In the case of tapered transition components which transit from a cylindrical crane connectionto a rectangular column special attention shall be paid to the knuckle line between the cambered parts andthe plane gussets If necessary thicker plates shall be provided572122 In way of connections of tapered or trapezoid transitions of crane columns knuckle linesespecially of even plates shall be stiffened if necessary by bulkheads in order to absorb the deviation forces572123 The transition parts and their connection areas described above require special care regardingfabrication and suitable mathematical proofs572124 The connection of container supports to crane columns requires special care regarding designand calculation
57213 Execution of cylindrical crane columns weldsIn the case of cylindrical crane columns all transverse and longitudinal welds shall be the full penetrationtype
57214 Execution of rectangular crane columns weldsAll transverse welds of rectangular crane columns shall be the full penetration type Regarding longitudinalwelds the following applies
a) Longitudinal welds in the plates shall be the full penetration typeb) The connecting welds at the corners may be dimensioned for the maximum shear force and may be
executed as fillet welds
57215 Connection to the ship hull572151 Wherever possible crane columns should be linked to the hull over a full deck height ifnecessary eg in the case of crane columns located at the shiprsquos side even to a greater depth into thestructure of the ship572152 Supporting structures interrupted by decks shall have well aligned connections If necessarycontrol bores shall be provided which shall be welded up after the control
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 121Standard for shipboard lifting appliances
DNV GL AS
572153 For the shear connection of inserted cylindrical crane columns the required plate thickness ofthe connecting deck or of the connecting weld may be calculated according to [494]572154 Crane columns which due to their location act as stiffness-discontinuities in the longitudinal andtransverse structures of ships such as eg laterally arranged crane columns with outer longitudinal wallswhich are attached to the shell plating of the ship shall have suitable taper brackets as required572155 Crane columns shall not be connected to hatch coamings if possible Where the connection tohatch coamings cannot be avoided suitable measures are required like eg tapered brackets and strengthanalyses for the additional loads
5722 Requirements for the design of the stowage trough of crane boom supports
57221 If possible the stowage trough shall embrace the stowage spur or a stowage holm without majorclearance (10 to 20 mm at maximum) and be lined with wood or other suitable material
57222 The gripping effect in the stowage trough caused by torsion of the shiprsquos hull in particular withcrane booms which are not stowed lengthwise shall be counteracted by a suitable design
57223 Where a luffing rope operated crane boom is not fixed downwards by tying-down of the cargo hooklocking devices shall be provided in way of the stowing trough in order to prevent of the crane boom comingoffThese devices shall not restrain the relative motions between stowing trough and crane boom
57224 Each stowing trough shall be accessible by means of ladders or climbing irons and locally provide asuitable area for operating control andor maintenance purposes
573 Hook speeds when operating under sea state5731 Minimum hoisting speed
57311 Cranes with a nominal load le 60 t573111 When operating under sea state conditions the hoisting speed shall be high enough to avoidrepeated contact between load and cargo deck after hoisting573112 The uniform minimum hoisting speed vhmin shall not fall below the following value
mdash multiple- reeved cargo runnervhmin ge 03 middot vsee [ms]
mdash single-reeved cargo runner
vhmin ge 05 middot vsee [ms]
vsee = sea state-induced speed according to Table 5-3 [ms]
57312 Cranes with a nominal load gt 60 tWhen operating under sea state conditions the hook speed resulting from superimposing the hoisting andthe luffing speed as well as the ballast speed of the floating body shall be high enough to avoid damage tothe crane or the load from repeated contact between load and cargo deck
5732 Horizontal hook speed
57321 Revolving cranes with a nominal load le 60 t573211 During loading and unloading of floating bodies it is important that the crane hook is capable offollowing the horizontal movement of the cargo deck
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 122Standard for shipboard lifting appliances
DNV GL AS
573212 The uniform slewing speed vω at the crane boom peak at about frac34 of the maximum load radiusshall not fall below the following value
vω ge 060 middot vsee [ms]
vsee = sea state-induced speed according to Table 5-3 [ms]
57322 Revolving cranes with a nominal load gt 60 t573221 The luffing speed and luffing acceleration shall be sufficient to ensure control of transverse loadoscillation573222 Load arresting ropes which limit the swinging of the load may be taken into considerationaccording to their effectiveness
5733 Luffing speedThe uniform vertical luffing speed vW at the crane boom peak at about frac34 of the maximum load radius shallnot fall below the following value
vW ge 010 middot vsee [ms]
574 Design details5741 Connection of slewing bearings
57411 Proof of bolts574111 The bolt connection shall be dimensioned according to recognized guidelines calculationprinciples or standards according to which if need be also a fatigue strength proof for the bolts can beconducted eg VDI-Guideline 2230The global safety factors according to [4382] shall be proven574112 Special care shall be taken over the determination of the maximum bolt force as eg anopening of the gap increases the bolt force non-linear574113 The stiffness of the slewing bearing can have a significant influence on the stress distribution inthe connecting structure The sector force Fa for the maximum loaded bolt according to Figure 5-4 shall bedetermined according to a recognized calculation procedure (eg FEM calculation under consideration of theconnecting structures stiffness) or by measurement574114 A simplified bolt proof according to [57412] can be conducted on condition the restrictions forapplication according to [74121] are complied with
Figure 5-4 Bolt sector and sector force
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DNV GL AS
57412 Simplified bolt proof574121 Restrictions for application
The simplified bolt proof can be applied if
mdash the outer bolt circle diameter does not exceed 35 mmdash stiffness of connecting structures (eg crane house crane pedestal) is approximately equal over the
circumferencemdash foot bearings of jibs and if applicable bearings of hydraulic cylinders on the crane house sufficiently
distant from the base plate of the crane housemdash the bolts of the standing and of the rotating ring are even distributed over the circumference and their
quantity per ring is not less than 12mdash the following relations are kept
a le 2 middot dℓ
b ge 15 middot dℓ
ba ge 075
a b dℓ according to Figure 5-6
d = thread diameter of bolt
574122 Format of proof
The following relations shall be kept
Zmax Zlimit le 1 or Zmax le Zlimit
Zmax = maximum tensile force in bolt according to [574123] [kN]Zlimit = limit value of tensile force in bolt according to [574128] [kN]
574123 Maximum tensile force in bolt
The maximum tensile force in the bolt is calculated as follows
Zmax = f middot Znom [kN]
Znom = nominal tensile force of the highest loaded bolt of a multiple bolt connection according to[574127] [kN]
f = form factor according to Table 5-8 [-]
574124 Forces on a large slewing bearing
For the terms and forces in Figure 5-5 the following abbreviations are valid which apply to the outer ringanalogously
Dr = roller circle diameter [mm]Dt = pitch circle diameter [mm]Dm = middle diameter of pedestal [mm]a = distance between pitch circle and middle of pedestal wall [mm]br = vertical force lever [mm]
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DNV GL AS
e = distance between bolt centre and start of chamfer (constraint lever) [mm]hr = horizontal force lever [mm]tf = flange thickness [mm]tw = wall thickness of pedestal [mm]
574125 Load from the crane
The following loads shall be determined including the global safety factor γs according to [4382] for themost unfavourable load combination according to Table 5-4 and Table 5-5
MSd = tilting moment [Nmm]VSd = vertical force [N]HSd = horizontal force [N]
574126 Forces acting on the ring per bolt sector
According to Figure 5-5 the following forces are valid in case VSd is pointing in that direction shown in Figure5-5 (compressive force)
[N]
[N]
[N]
Table 5-8 Form factors
Tensile class of boltKind of flange connection
88 109 129
Tensioning procedure with torsion 13876 13592Ball bearing
Tensioning procedure without torsion 11563 1132713451
Tensioning procedure with torsion 12923 12659Roller bearing
Tensioning procedure without torsion 10769 1055012528
D = lowest value of Dm Dt and Dr
ns = number of boltsFhd = Fvd middot γh [N]
Fhz = Fvz middot γh [N]
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DNV GL AS
Figure 5-5 Forces on a large slewing bearing
Fhd Fhz forces between the rings with influence to the bolt forces
γh = horizontal force coefficient= 0 for multi row bearing= 0577 for single row ball bearing= 1 for single row cross roller bearing
574127 Calculation of maximum nominal tensile force
Based on the dimensions acc to Figure 5-5 and on the forces acting on the bearing ring acc to [574126]the maxi-mum nominal tensile force is calculated as follows
Znom =
574128 Limit value of tensile force of bolt
The limit value of tensile force of the bolt shall be calculated as follows
Zlimit = σlimit middot Ak 1000 [kN]
σlimit = limit stress acc to Table 5-10 [Nmm2]Ak = core section of bolt acc to Table 4-13 [mm2]
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DNV GL AS
Table 5-9 Limit stresses of bolts
Tensile class 88 109 129
Limit stress σlimit [Nmm2] 560 768 912
57413 Requirements for the flange574131 Flange connection
In general the upper part of crane columns which are provided with a flange for connection to a slewingbearing shall be designed according to Figure 5-6 In the case of an inner bore circle the same conditionsapply
Figure 5-6 Upper part of crane column
574132 Dimensioning of the flange
Dt = partial circle diameterDa = outer cylinder diametertf = flange thicknessdℓ = bore diameterr = corner radius
a = external partial circle
a = internal partial circle
h = height of connection areatw1 = cylinder wall thickness in the connection areatw2 = cylinder wall thickness below the connection area
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DNV GL AS
The flanges shall be designed and dimensioned according to [49152] As far as no proof by FE-computation has been conducted in addition the following conditions shall be met
tf ge 3 middot tw1
tw1 ge 15 middot tw2
574133 Facing
The flange thickness according to [574132] shall still be warranted after the facing
574134 Flange evenness
The evenness of the connecting areas on a slewing bearing shall meet the requirements given by themanufacturer of this bearing
574135 Use of compounds
The use of compounds in order to achieve the evenness required by the manufacturer of the slewing bearingis only accepted in exceptional cases for repair purposes upon agreement by the Society and slewing bearingmanufacturer
57414 Requirements for the cylinder wall in the connection area574141 DimensioningThe wall thickness t1 and the connection weld shall be dimensioned with regard to fatigue strength574142 Height of connectionAs far as no proof by FE-computation has been conducted the height of the uppermost cylinder sectionaccording to Figure 5-6 shall at least be 02 middot Da where the upper limiting point is formed either by the loweredge of the flange or by the lower edge of brackets
57415 Revolving circle diameter of the slewing bearings574151 The diameter of the revolving circle shall correspond to the mean diameter of the upper andlower connection cylinder if possible in order to avoid additional measures such as eg welding of brackets574152 Where brackets shall be attached they shall not be spaced further than two bore distances
57416 Requirements for bolts and bores574161 In general the span length of bolts shall be at least 5 middot ds574162 At least 6 thread turns shall remain free574163 The connecting bolts of slewing bearings of cranes of the groups B2 B3 and C shall have rolledthreads574164 The size of bolt bores shall be indicated by the bearing manufacturer (in general according to[4912])
5742 Doubling platesDoubling plates for the transmission of tension forces and bending moments are not permissible
5743 Cruciform jointsRegarding cruciform joints for the transmission of forces perpendicular to the roll direction the requirementsgiven in [48124] apply
5744 Joints of runwaysRunways shall be welded continuously and the welds shall be executed such that no vertical dynamic forcescan be induced when travelling
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DNV GL AS
575 Securing of the hook in the condition crane out of serviceThe swinging of cargo hooks in the condition crane out of service shall be prevented by design unless theyare tied-down The tie-down force may exceed 10 of the nominal load LNe only in cases where this was abasis for the dimensioning
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DNV GL AS
SECTION 6 SPECIAL LIFTING APPLIANCES AND MEANS OFTRANSPORT
61 General
611 This section deals with the requirements for the design and dimensioning as well as for the manufacture andoperation of special lifting appliances and means of transport
612 As regards requirements for the materials to be used as well as for manufacture and welding therequirements given in Sec3 and Sec11 apply
613 Calculation and dimensioning shall be based on Sec4 and Sec9 as well as further sections as requiredDeviating requirements given in this section shall be observed
614 For machinery components and the electrical fittings on special lifting appliances and means of transport therequirements given in Sec9 and Sec11 shall be complied with if applicable
615 Accessories shall be selected using recognized standards The dimensioning of non-standard accessories canbe carried out in accordance with Sec7
62 Rope and chain hoists
621 General notes
6211 The requirements that follow apply to rope and chain hoists regardless of drive mode which are notused for handling cargo They only apply to manually operated devices however where relevant
6212 Handling of goods for ship operation is not regarded as cargo handling
622 Manufacture6221 MaterialsIn addition to the steels and materials generally used for machinery components special steels aluminiumplastics and other materials can be used if they are appropriate for the intended use
6222 DimensioningThe requirements given in [613] also apply to foundations or runway girders of rope and chain hoistsproduced in series
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DNV GL AS
623 Equipment and safety regulationsFor all types of drive the requirements given in Sec12 shall also be observed if applicable In addition thefollowing applies
6231 Overload protection
62311 Series production623111 For hydraulic pneumatic and electrical hoist drives effective overload protection devices shall beprovided623112 In the case of hydraulic hoist drives pressure relief valves are permissible up to a nominal loadof 1000 kg623113 As regards response limits and response tolerances of overload protection devices the settingsor parameters given by the manufacturer apply
62312 Individual productionFor rope and chain hoists manufactured by individual or special production the requirements given in[12411] apply
6232 Hook travel limits
62321 General requirements623211 Rope and chain hoists shall have limit switches for the upper and lower hook position623212 In the case of power-operated rope and chain hoists the limit switches shall act mechanicallyandor electrically on the hoist drives
62322 Series production623221 For hydraulic pneumatic and electrical hoist drives effective limit switches for the hook travelshall be provided
62323 Individual productionFor rope and chain hoists manufactured by individual or special production limit switches for the upper andlower hook position shall be provided which function electrically
6233 Runway limitAs regards runway limit the requirements given in [5342] and [1242] apply if applicable
6234 Slack rope limitIn special cases slack rope monitoring and limitation may be required eg at high hoist speeds withmultiple coils or if required by the mode of operation
6235 Eye plates for load testsIt is recommended suitable eye plates be fitted to the shiprsquos hull for load tests on hoisting ropes and hoistingchains located below deck For this kind of load test the application of the test load shall be conducted with aseparate manual hoist only but not with the power drive of the rope or chain hoist itself
624 Means of suspension6241 Hoisting ropes
62411 General notes624111 Hoisting ropes and their end attachments are covered by the requirements given in Sec8624112 Wire-ropes made of stainless materials as well as fibre ropes may be allowed for specialpurposes if suitable and if the design of the hoist rope is verified accordingly
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DNV GL AS
62412 Safety against fracture624121 Safety against fracture is defined by the coefficient of utilization γ D1 or γ F according to Table8-2 and Table 8-4 and this shall be applied to the maximum static hoisting rope force
624122 When using rope hoists below deck γD1 may be le 40624123 For the use of rope hoists above deck the following applies
a) In the case of rope hoists manufactured by series production γD1 may be le 40 unless nationalregulations dictate otherwise
b) For rope hoists manufactured by individual or special production the values in Table 8-2 and Table 8-4shall be used without limitation of γD1 or γF
6242 Hoisting chains
62421 General notes624211 Hoisting chains shall comply with recognized standards624212 Chain wheels of hoisting chains as well as their end links or fasteners for leading-in the towchain shall conform to standards
62422 Safety against fractureThe breaking load of hoisting chains shall be at least the γK-fold of the chains maximum static towing forceThe following coefficients of utilization γK shall be applied
γK ge 50 (power-driven)
γK ge 40 (operated manually)
6243 Accessories
62431 Accessories such as eg cargo hooks shackles and rope sockets shall comply with recognizedstandards and shall be dimensioned for test loads according to Table 7-4
62432 The dimensions of the eye plates on normal strength and high strength shackles shall comply withthe Tables in Sec7
62433 Regarding the use of detachable rope end attachments (rope sockets or rope clamps) therequirements given in [8423] apply
625 Examination of drawings and supervision of construction6251 Series production
62511 Manufacturers of rope and chain hoists made by series production are permitted to produce undertheir own responsibility and to certify their products themselves if the manufacturing processes and productsare certified in a legally-binding and recognized manner eg by type approvalFor those in addition to drawings of foundations or runway girders including fastenings the followinginformation at a minimum shall be submitted if applicable
mdash designation of manufacturer and typemdash nominal load(s) and dead weight(s)mdash hoist speed and operating speed if applicablemdash type of drivemdash type(s) of electrical protection see [10617]mdash further information as required
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DNV GL AS
62512 For the Societys type approval see DNVGL CP 0338 applies
6252 Individual production
62521 Rope and chain hoists manufactured by in-dividual or special production are subject to examinationof drawings and supervision of construction by the Society
62522 For the examination of drawings the list of documents to be submitted for examination inSec2 shall be applied as and where relevant In addition the following drawings and information shall besubmitted if applicable
mdash housingmdash rollers including fastening to housingmdash form-locking drive devices such as eg rack bars and pinionsmdash runway limitsmdash details of hoisting ropes and hoisting chains including end attachmentsmdash rope-sheaveschain wheelsmdash foundations or runway girders including fasteningsmdash stowage position including fastening devicesmdash further documents as required
62523 For supervision of construction the requirements given in [132] apply
626 Tests and examinations on board
6261 For the initial test and examination the requirements given in [133] apply
6262 For the periodic testing and examinations the requirements given in [134] apply
627 Documentation6271 IdentificationFor the identification of rope and chain hoists the requirements given in [132421] [1325] and [1326]and [1335] apply
6272 Certificates
62721 Certificates for production627211 Series productionRope and chain hoists manufactured by series production shall be delivered with a test report as well as withtest reports for all means of suspension such as ropes chains and accessories627212 Individual productionFor rope and chain hoists manufactured by individual or special production the Societys product testcertificate Form 2092a based on an examination before delivery is requiredThe Societys test certificates shall be submitted for all means of suspension such as ropes chains andaccessories
62722 Certificate for load tests627221 Certificates to be issued after every load test due to national regulations are described in[137]627222 For rope and chain hoists which shall not be subjected to ongoing control by the Society theSociety may recognize deviating forms or certificates not issued by the Societys surveyor
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DNV GL AS
6273 Register book
62731 All certificates for means of suspension and load tests investigation reports as well as informationfor operation (manuals maintenance protocols etc) where applicable shall be compiled in a register bookand stored For details see [137]
63 Ramps and car decks
631 General notes
6311 Testing investigation and certification of ramps and car decks fixed to the ship is part of theclassification of the ship
6312 As regards naval-architectural concerns such as ships strength water-tightness impact stress bythe sea etc the requirements given in RU SHIP Pt3 apply
6313 The following requirements relate to mobile shipboard ramps and car decks operated under load
632 Production6321 MaterialsIn addition to ship structural steels other steels and aluminium may also be used for load-bearingconstructions if they are suitable for the intended purposeFor machinery components materials shall be selected in accordance with the DNV GL rules
6322 Dimensioning
63221 The dimensioning of steel or aluminium ramp or car deck construction shall comply with therequirements given in [6312]
63222 For the dimensioning of structural or machinery components of rope or chain drives a hoist loadcoefficient of ψ = 115 shall be applied to moved masses
633 Equipment and safety regulations6331 Scratch boards railings and barriers
63311 Ramps and car decks shall be fitted with scratch boards railings and barriers as necessary For thedimensioning of railings [4992] appliesScratch boards for motor vehicles shall be designed to meet the line loads according to Table 6-1
Table 6-1 Loading scratch boards
Vehicle type Line load Height of load application
Passenger vehicles 2 kNm 03 m
Trucks 5 kNm 05 m
63312 The construction of scratch boards railings and barriers including their associated safety devicessuch as eg colour markings photoelectric barriers and warning signals are subject to drawing examinationby the Society
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DNV GL AS
6332 Anti-slip safeguardsRamps shall be fitted with welded-on or bolted-on anti-slip safeguardsIn special cases anti-slip paint may be permitted in lieu
6333 Ramp inclinationRamp inclination shall not in general exceed the ratio 110
6334 Permissible deflection
63341 The permissible deflection of ramps and car decks under nominal load in the stowed position shallnot exceed
f =
where
f = deflection (depth gauge)bs = spacing of supports (span)
63342 In the stowed position the deflection may not endanger either the water-tightness of the ship orany cargo (eg vehicles) underneath
6335 Stowage positions
63351 In the stowage positions provided ramps and car decks shall not be hung on ropes or chains butshall have mechanical supports and locks
63352 Supports and locks shall be dimensioned according to the requirements given in [6312] andsafeguard the water-tightness of the ship where ramps are part of the shell
634 Means of suspension6341 Hoisting rope and suspension rope
63411 General notes634111 For hoisting ropes and suspension ropes and their end attachments the requirements given inSec8 apply634112 Wire ropes of stainless materials as well as fibre ropes may be permitted for special purposes inindividual cases if they are suitable and if the design of the rope drive is adjusted accordingly634113 Fibre ropes for the transport of persons are only permitted under special conditions
63412 Safety against fracture634121 Safety against fracture is defined by the coefficient of utilization γD1 or γD2 according to Sec8Table 8-2 and shall be applied to the maximum static towing rope force634122For hoisting ropes the following safety factors shall be applied depending on the mode of operation inaccordance with Table 8-2
mdash operation without useful load = γD1 ge 36mdash operation with useful load = γD1mdash operation involving persons = γD1 middot 20
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DNV GL AS
634123 Ramps which are not supported at their free end when used by vehicles may apart from chainsalso be fixed by hoisting ropes or special suspension wires In this case the following safety factors shall beused
mdash hoisting ropes or guided suspension ropes = γD1 middot 20mdash suspension ropes not guided = γD2 middot 20
6342 Hoisting chains and suspension chains
63421 General notes634211 Hoisting chains and suspension chains shall comply with recognized standards634212 Chain wheels as well as their end links or fasteners for leading in the tow chain shall be selectedin conformance with standards
63422 Safety against fractureThe breaking load of hoisting chains and suspension chains shall be at least the γK-fold of the chainsmaximum static towing force Depending on the mode of operation the following coefficients of utilization γKshall be applied
mdash operation without useful load = γK ge 28mdash operation with useful load = γKge 40mdash operation involving persons = γK ge 80
6343 Accessories
63431 The requirements given in [62431] and [62432] shall be observed
63432 Detachable rope end attachments (rope sockets or rope clamps) are not permitted for rope drivesof ramps and car decks
6344 Hydraulic cylindersHydraulic cylinders shall be dimensioned in accordance with [492]
635 Examination of drawings and supervision of manufactureRamps and car decks are subject to examination of drawings and supervision of manufacture
6351 Examination of drawingsFor the examination of drawings the list of documents to be submitted in [21] shall be applied as and whererelevant In addition the following drawings and information shall be submitted if applicable
mdash overview drawing with layout and numbering of ramps and car decks where applicablemdash complete rope drives and chain drivesmdash guide blocks including fasteningsmdash scratch boards barriers and railingsmdash rigging plansmdash additional documents as required
6352 Supervision of manufactureFor the supervision of manufacture the requirements given in [132] apply
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DNV GL AS
636 Tests and investigations on board6361 Initial test and investigation
63611 For the initial test and investigation the requirements given in [133] apply
63612 The load tests with test loads according to Table 13-2 shall be performed statically in the stowagepositions and dynamically for the movable installations
6362 Periodic testing and investigations
63621 As part of the shiprsquos Classification ramps and car decks are subject to annual Class surveys and 5-year Class Renewal surveys Instead provision is made for annual performance tests but not for 5-year loadtests
63622 Where required by national regulations ramps and car decks shall be treated like cargo gear Therequirements given in [134] apply in this case During the 5-years load tests [63612] shall be observed
637 Documentation6371 IdentificationFor the identification of ramps and car decks the requirements given in [1325] [1326] and [1335]apply
6372 Certificates
63721 Manufacturing certificates637211 The manufacturer of ramps and car decks shall supply the Societys test certificates for allmeans of suspension such as ropes chains accessories and hydraulic cylinders as well as for winches637212 As confirmation of investigation before deli-very the Societys test certificate Form 2092a isrequired for every ramp and every car deck or for every series of such ship components
63722 Certificates for load tests637221 As a confirmation of the load tests the Societys test certificate Form 208 is required for everyramp and every car deck or for every series of such ship components637222 Where due to national regulations ramps and car decks shall be treated like cargo gear therequirements given in [1336] and [1346] apply
6373 Register book
63731 All certificates for means of suspension and load tests investigation reports as well as informationabout operation (manuals maintenance protocols etc) where applicable shall be compiled in a registerbook and stored For details see [137]
63732 Confirmation of the class surveys according to [63621] is effected within the scope of shipclassification Relevant excerpts of the survey report for the ship may be added to the documentation file
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DNV GL AS
64 Lifting appliances for research work
641 General notes
6411 Lifting appliances for research work are employed for the extraction of seabed samples and watersamples for towing and for general handling of research equipment In the process ropes cables or acombination of both are utilized
6412 Exceptional loads may result from large rope or cable lengths from ship movements or fromextraction devices getting caught as well as being pulled out of the sediment
6413 Lifting appliances for research work are eg
mdash stern gantry cranemdash slewing gallowsmdash lateral outriggermdash hatch beammdash loading gear with special functionsmdash A-frames
642 Treatment of loading gear for research workLifting appliances for research work is treated like lifting appliances not intended for the handling of cargoThe following specific features however shall be considered
643 Special features6431 Dimensioning
64311 Lifting appliances for research work shall be dimensioned for the breaking loads of ropes or cablesFor the dimensioning the following load combination shall be assumed following Table 5-4 load combinationIII
mdash dead loads γpi = 110mdash ropecable breaking load γpi = 110mdash diagonal pull γpi = 110mdash resistance coefficient γm = 110
In general for this purpose the diagonal pull shall be assumed for the most unfavourable direction as follows
mdash lifting 15degmdash towing longitudinally to the ship 30degmdash towing transversely to the ship 45deg
64312 Where lifting appliances for research work are also intended for handling goods for ship operationit shall also be dimensioned accordingly
64313 Accessories shall be selected in such a way that the breaking load of ropes or cables corresponds tothe test loads of the accessories stated in Table 7-4
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DNV GL AS
6432 Marking
64321 When marking lifting appliances for research work the requirements given in [1325] applyInstead of SWL and a quantity in kg or t the minimum breaking load of the rope as MBLRope and a quantity[kN] shall be used
64322 Where several ropes or cables are attached to one lifting appliance marking is required on everysingle rope or cable
64323 Where lifting appliances for research work are also intended for handling goods for ship operationit shall also be marked with SWLWhen determining the quantity to be indicated the breaking load of the rope shall be divided by thecoefficient of utilization γD1 in accordance with Table 8-2 and then to be converted into kg or t
6433 Operating manual
64331 An individual operating instruction shall be prepared for every lifting appliance for research work inwhich the special features of operation and control are described
64332 Operating manuals are subject to examination and shall remain permanently on board as part ofthe lifting appliance documentation
65 Industrial cargo-handling vehicles
651 General notes
6511 The following requirements apply to industrial cargo-handling vehicles in series production which arecertified in a legally-binding or recognized manner unless otherwise provided by national regulations
6512 Prerequisites for use on board are proofs of stability against overturning see [4522] and at aminimum the existence of test reports
6513 The requirements given in [653] and [654] apply only to industrial cargo-handling vehicles whichremain in permanent employment on board
652 Safety regulations
6521 The employment of industrial cargo-handling vehicles on board presupposes that decks and hatchcovers are adequately dimensioned to be run over
6522 Where industrial cargo-handling vehicles remain permanently on board fastening arrangements(eg eye plates) for securing for use at sea shall be fitted both to the vehicle and to the hull
6523 The use of industrial cargo-handling vehicles powered by IC engines or by non-explosion-proofelectric motors is not permitted in hazardous locations and areas
6524 Industrial cargo-handling vehicles run on fuel may only be used in cargo spaces if there is adequateventilation Otherwise only battery-powered vehicles shall be employed
6525 The use of fuels with a flash point below 60degC is not permitted
6526 In general fork-lift trucks to be used on board shall have a tiltable lifting frame
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DNV GL AS
653 Control measures6531 Initial controlBefore start of operation the following measures are required at a minimum
mdash check the information documents included with deliverymdash function check with nominal loadmdash test run over the operational areas with nominal load as proof the deck or hatch covers are sufficiently
strong
6532 Regular controlsIndustrial cargo-handling vehicles are subject to supervision and regular control by the ships management atintervals not exceeding 6 monthsThese controls shall be confirmed in a suitable manner and added to the documentation
654 Documentation6541 CertificationFor the control as per [6531] the Societys surveyor issues a certificate Form 2092a
6542 IdentificationFor stamping correlating to the test certificate the requirements given in [1335] apply
6543 Register book
65431 All certificates for load tests investigation reports as well as information about operation (manualsmaintenance protocols etc) where applicable shall be compiled in a register book and stored For detailssee [137]
65432 In addition to the certificate as per [6541] the manufacturerrsquos documentation shall be includedin the register book This also applies to all confirmations of control measures by the ships management see[6532]
66 Means of conveying persons
661 Shipborne working baskets
6611 Newly-manufactured working baskets shall meet the requirements given in EN 14502-1
6612 Shipborne working baskets shall be treated in all respects similarly to lifting appliances not handlingcargo Their dimensioning and testing shall however be subject to the static test loads according to Table 7-2
662 Requirements for lifting appliances for conveying personsLifting appliances for conveying persons shall comply with the requirements given in [425] with respect todimensioning operation and control
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DNV GL AS
663 Landing booms6631 General notes
66311 The provision and the arrangement of landing booms (swinging booms for conveying persons) arerequired by the St Lawrence Seaway Authority
66312 Landing booms shall only be used for conveying one single person at a time
66313 Landing booms shall be treated as lifting appliances not handling cargo except where otherwisedetermined in what follows
6632 Dimensioning
66321 Landing booms together with the associated posts shall be designed for a static test load LPstat of300 kg (Table 7-1 load condition III2 without wind and hoist load coefficient)
66322 Ropes and interchangeable components shall be designed in addition to the dead loads for a staticboom load of 150 kg at a minimum
66323 The slenderness ratio of a landing boom may not exceed a value of 200
The following equations apply
IL = moment of inertia of boomAL = cross-section area of boom
6633 Construction and layout
66331 The load radius of landing booms shall be about 9 m
66332 If landing booms are equipped with several span ropes (eg a second span rope about halfwayalong the boom) the length of these intermediate span ropes shall be adjustableThe length adjustment of the intermediate span rope shall be effected in such a way that no unfavourablestress may arise under load (cantilever effect)
66333 Landing booms shall be operated exclusively by hand The lowering system shall allow gentle set-down
66334 Landing booms shall be located in the forward portion of the ship roughly at the point where thebow has widened to the full beam and shall swing forward from aft
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DNV GL AS
6634 Examination of drawings and supervision of construction
66341 Landing booms together with the associated posts shall be constructed according to the drawingsapproved by the Society
66342 Because all components are normally easily accessible for subsequent controls supervision ofconstruction is not required in general Test reports shall be included in the delivery
6635 Tests and investigations on board
66351 For the tests and investigations on board the requirements given in [133] and [134] apply withthe following deviations
66352 Landing booms shall be tested before start of operation and periodically every 5 years eitherstatically by swinging a test load of 300 kg or by swinging lowering and braking a test load of 200 kg
6636 DocumentationWith respect to identification certification and documentation the requirements for lifting appliances nothandling cargo apply see Sec13
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DNV GL AS
SECTION 7 LOOSE GEAR AND INTERCHANGEABLE COMPONENTS
71 General
711 This section deals with the requirements for design and calculation as well as production and employment ofloose gear and interchangeable components
712 With respect to requirements for the materials to be used as well as for production and welding theprovisions in Sec3 and Sec11 apply
713 For machinery components and electrical loose gear equipment the requirements given in Sec9 and Sec11shall be complied with where relevant
72 Loose gear
721 General notesThe following requirements apply to loose gear according to [1151] and [11531]
722 Design principles7221 General notesThe requirements given in Sec4 shall be observed as appropriate In addition the following applies
72211 Suspension ropes rope slings and their rope attachments shall comply with the requirements givenin Sec8If a test certificate (CG4) for the rope is submitted and proof is provided that the rope connections havebeen produced by manufacturers with the Societys approval then further requirements for interchangeablecomponents may be dispensed withRegarding the rope deflection the reduction of the minimum breaking load which depends on the ratio Ddshall be taken into account
72212 Suspension chains and their end attachments shall comply with recognized standards
72213 Regarding the suspension height of loose gear it shall be pointed out that the opening angle ofsuspension ropes or chains shall not exceed 120deg and of ramshorn hooks shall not exceed 90deg
72214 In order to warrant balance (safety against turn-over) of the total system or parts of it consistingof loose gear andor load it is assumed in the requirements given in this section that both the loose gear andthe loads have a positive stability height see illustration in Figure 7-1
72215 SuspensionsSuspensions are loose gear consisting of tension elements which are directly connected to the liftingappliance hook or to other loose gear (eg a traverse or frame-type traversespreader) For examples oftypical suspensions see Figure 7-2
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DNV GL AS
Regarding 4-leg suspensions without load equalisation it shall be taken into consideration that these systemsare statically indeterminate The individual legs of the suspension are stressed depending on the rigidityof the load or the loose gear to be handled Where the load or the loose gear has high rigidity the loaddistribution on each leg of the suspension shall be verified by static calculation Without verification of theactual load distribution in the complete system (suspension and load or loose gear) only 2 legs shall beassumed as load-bearing
7222 Traverses
72221 Traverses may only be loaded symmetrically to the centre of gravity of the load unless they aredimensioned for asymmetric loading and marked accordinglyWhen there are more than 2 attachment points between the loose gear and the load the strength testcorresponding to the rigidity of the load (statically indeterminate system) shall be conductedAlternatively devices may be fitted which indicate the load
72222 Where longitudinal lifting beams have under-slung transverse lifting beams using tension elementsthis system shall be designed for safe operation in accordance with the static degrees of freedom Suf-ficientstrength shall be proven by a strength analysis
72223 Telescopic traverse parts shall be lockable in their working positions
7223 Frame traversesspreader
72231 In the case of adjustable container spreaders the movable beams shall either lock into the desiredworking positions or constructional measures shall be taken to ensure that the beams are accurately placedand held in these positions
72232 Container spreaders shall be equipped with indicators showing in a suitable manner whether thetwist locks are locked or unlocked
72233 Locking pins which automatically unlock when unloaded are not acceptable
7224 Grabs and lifting magnets
72241 The structural design and operating mode of grabs and lifting magnets shall be suited to theintended type of cargo
72242 The mechanical strength and electrical equipment of grabs and lifting magnets shall company withthe requirements given in this standard
72243 Closing ropes of grabs shall be protected in a suitable way against excessive wear
72244 Lifting magnets shall comply with the requirements given in EN 13155
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DNV GL AS
Figure 7-1 Balance conditions
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Figure 7-2 Suspending systems for typical suspensions
G1 = 3-leg suspension (statically determinate load connecting points are not in one vertical plane)G2 = 4-leg suspension symmetrical (statically indeter-minate with rigid load) The total load is carried
either by leg S1 and S3 or by S2 and S4 The center of gravity of the load (SP) is located in both ofthe planes spanned by S1S3 and S2S4
G3 = 4-leg suspension asymmetrical (statically indeter-minate with rigid load) see also notes under G2G4 = 4-leg suspension with load compensation on one side (statically determinate with sufficient
geometry of load compensation)G5 = 4-leg suspension with frame spreader (sta-tically indeterminate see also notes under G2)G6 = 4-leg suspension with two spreaders (statically determinate)
723 Calculation principles7231 General notes
72311 Calculations and dimensioning of loose gear are subject to the requirements given in Sec4 andSec6
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DNV GL AS
72312 Regarding the loads to be considered and the proofs to be provided the following requirementsshall be observed
7232 Dimensioning loads
72321 General723211 The loads acting on loose gear are subdivided as follows
mdash regular loadsmdash irregular loadsmdash special loads
723212 If necessary loads not addressed in the following shall be considered additionally in a suitableway The grading of such loads and the consideration of them in the corresponding load combinations shall beagreed with the Society
72322 Regular loads723221 Dead load LEDead loads shall be determined in accordance with [4242]723222 Useful load LNThe useful load is defined in [11559] When dimensioning the loose gear this is assumed to be the nominalload723223 Dynamic forces caused by drivesRegarding the dynamic forces caused by drives the provisions of [5324] apply including the followingadditions
mdash For dimensioning in general only those vertical dynamic forces shall be considered which are covered bythe hoist load coefficient ψ Therefore the useful loads according to [723212] shall be multiplied bythe maximum hoist load coefficient ψ for this application of the allocated lifting appliances
mdash LNe shall be always relevant for dimensioning This shall be ensured by the conditions in [5432]mdash If loose gear or interchangeable components cannot be allocated to lifting appliances the following hoist
load coefficient shall be used
SWL ψ SWL ψ
le 10 t 16 le 1000 t 12
le 160 t 14 gt 1000 t 115
le 500 t 13
This is only permissible if the lifting appliance is used in harbour operations When used under seawayconditions the increased requirements given in the lifting appliance used thereby shall be considered
72323 Irregular loads723231 Wind loadsWind loads shall be assumed acc to [4245]723231 Snow and ice loadsIf snow loads shall be considered these shall be provided by the manufacturerIf ice loads shall be considered these shall be determined acc to [4246]
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DNV GL AS
72324 Special loads723241 Test loadsLoose gear shall be dimensioned for a static test load LPstat acc to Table 7-2 or if more unfavourable for thedynamic test load of the lifting appliance acc to [5341] including the reduced hoist load coefficient ψP
max (LPstat LPdynmiddotψP)723242 Lateral impactFor frame-type traversesspreader a lateral impact of 110 of the maximum vertical load in the frame levelshall be assumed
HS = (LNe + Le)10
7233 Load combinations and partial safety factors
72331 General notes723311 The load combinations deemed to be essential for loose gear in operation are compiled in Table7-1723312 For the condition cranes out of operation the load combinations and partial safety factorsaccording to Table 5-5 shall be assumed regarding strength analysis723313 According to circumstances further load combinations may arise723314 From the load combinations in Table 7-1 and where required further load combinations onlythose combinations which are prevailing or necessary for the structural element being considered shall beproved
72332 Comments on the load combinations for loose gear under operating conditions723321 The load combinations I1 II1 III1 and III2 correspond to those given in [552]
Table 7-1 Load combinations for loose gear under operating conditions
Load combinations
I II IIILoadcate-gories
Loads i Reference
γpi I1 γpi II1 γpi III1 III2 III3
Dead loads LE 1 7 [23221] 122 1 10 116 1 10 110 1 10 10 10Regularloads Useful load LN 2 7 [23222] 134 Ψ 122 Ψ 110 - - Ψ
Wind loads underoperating conditions 3 7 [23231] 122 10 110 - 02 -Irregular
loadsSnow and ice loads 4 7 [23232] 122 10 - - - -
Hoisting the hoistload at vhmax
5 4 Table 5-2 110 ψmax - -
Test load 6 7 [23241] 110 - ψp -Specialloads
Lateral impact 7 7 [23242] 110 - - 10
Resistance coefficient γm 110 110 110
Global safety coefficient γs 148 134 122
1) Where load combinations have a favourable effect γpi = 095 may be assumed If the components masses andcentre of gravity is determined by weighing 095 middot γpi may be assumed
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DNV GL AS
723322 Consideration of the deviation of the loads centre of gravityDue to an unexpected and not precisely determinable deviation in the centre of gravity stresses on the loosegear shall be considered assuming an inclined position deviating 6deg from the ideal location in relation to bothmain axes This load condition shall be examined additionally723322 III3 - Lateral impactThe load combination comprises the loads due to hoisting of the hoist load including a lateral impact
7234 Proofs
72341 GeneralThe loose gear shall be dimensioned taking into consideration the following points723411 The centre of gravity is located in the axis of symmetry of the suspension723412 Regarding frame-type traverses or spreaders the bending rigidity of the load shall also beevaluated with respect to load transfer and possibly to be included in the static strength analysis Withoutproof of the static strength of the frame-type traverse or spreader as an overall system complete with theload only two load attachment points may be assumed to be load-bearing
72342 Strength analysesRegarding the strength analyses In general the statements in [44] and [48] apply The load combinationsshall be formed using the values for the partial safety factors according to Table 7-1723421 Telescopic parts of traverses or spreadersIn the case of the telescopic parts of traverses or spreaders careful attention shall be paid to the transverseforce in the overlapping area and to the force transferred at the outlet as well as at the inner end of themovable part
72343 Proof of stability (buckling lateral torsional buckling warping)For proof of stability the statements in [44] apply in general The load combinations shall be formed usingthe partial safety factors according to Table 7-1723431 Special boundary conditions for traversesRegarding the proof of stability of traverses special boundary conditions shall be assumed for thedetermination of the critical buckling load It shall be considered that there is no fork bearing ie the proofsof stability used in the general steel engineering to determine the critical buckling load are not applicableFor the determination of the minimum potential energy due to outer and inner forces only the restoringmoments between the traverses suspension and the loads suspension can be applied which are activatedby the eigen mode of the traverse In determining the ideal lateral torsional buckling moment (Mki) theseboundary conditions shall be applied
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DNV GL AS
723432 System assumptions for the determination of M
Figure 7-3 Eigenmode of the transverse
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DNV GL AS
Figure 7-4 Eigenmode of the transverse
Figure 7-5 Eigenmode of the transverse
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DNV GL AS
723433 Boundary conditions for the proof of tra-verses
mdash determination of the section forces and deformations in accordance with 2nd order theorymdash application of the geometrical replacement imperfections using ΔS = L150 (maximum ΔS of the eigen
mode) see Figure 7-3mdash limitation of the torsional angle Φ le 03 rad see Figure 7-4 and Figure 7-5
72344 Fatigue strength analyses for loose gear723441 For fatigue strength analyses in general the statements in [56] apply Generally they shall beconducted for the load combination I of Table 7-1 using a partial safety factor of γpi = 10723442 For loose gear with stress cycles le 20000 a fatigue strength analysis may be dispensed with
72345 Proofs of suitability for useFor proofs of suitability for use in general the statements in [47] apply Generally they shall be conductedfor the load combination I of Table 7-1 using a partial safety factor of γpi = 10723451 TraverseThe maximum deformation shall be limited to le L500 related to the traversesrsquo length723452 Frame-type traversespreaderThe maximum bending deformation due to the dead weight shall be limited to le L1000 related to thespreadersrsquo length the maximum bending deformation shall be limited to le L500 related to the spreaderslength723453 Container spreaderThe maximum bending deformation (bending stiffness) of the spreader shall be limited such that the liftlocks cannot unlock under operational conditions
724 Examination of drawings and supervision of construction7241 Examination of drawings
72411 The general requirements given in Sec13 shall be observed
72412 Regarding the documents to be submitted for examination the lists in Sec13 shall be applied asand where relevant In addition the following documents shall be submitted for examination
mdash overview drawings showing all variations of functions loads and load fasteningsmdash workshop drawings of all steel componentsmdash strength analyses for all load-bearing components (static dynamic fatigue strength as required)mdash stowage and fastening devices for shipborne loose gearmdash additional documents as required
7242 Supervision of construction
72421 The general requirements given in Sec1 shall be observed
72422 The supervision of construction and acceptance testing before delivery is required in principle
72423 For loose gear which is still accessible for comprehensive examination after completion supervisionof construction may be dispensed with subject to the consent of the Societys surveyor Acceptance testing isrequired in every case where appropriate together with the first load test
72424 The requirements to be met by the manufacturer are set out in [112]
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DNV GL AS
725 Tests and examinations7251 Tests
72511 Before being put into use and after every major modification or repair to load-bearing parts loosegear shall be subjected to a functional and load test in the presence of the Societys surveyor
72512 Regularly repeated load testing of loose gear is not prescribed internationally by ILO It shall benoted however that various flag administrations do have regulations on this
72513 The static test loads given in Table 7-2 are applicable to loose gear according to the definition in[11531]
Table 7-2 Static test loads for loose gear
Nominal loads LNe of loose gear Static test loads 1 LPstat
up to 10 tabove 10 t up to 160 t
above 160 t
2 times SWL(104 times SWL) + 96 t
11 times SWL1if applicable to be multiplied with fd according to [7334]
7252 Examinations
72521 Before being put into use after each load test and after each modification or repair to load-bearingparts all loose gear shall be subjected to a thorough examination by the Societys surveyor and wherenecessary a functional test under his supervision
72522 In addition to the regulations according to [72521] all loose gear shall be subjected to a visualexamination by the Societys surveyor at least every 12 months as well as a thorough examination every 5years and where necessary a functional testFor due dates of examinations the provisions in [1342] are applicable
726 DocumentationFor marking see [74]
7261 Certification
72611 After each load test using the prescribed test load according to Table 7-2 the supervising theSocietys surveyor issues one of the two following certificates Functional tests are not specially certified
72612 For ships loose gear a test certificate Form CG3 will be issued For use on board more than oneship additional copies may be issued
72613 For loose gear which cannot be allocated to a particular ship a test certificate Form 2092a will beissuedFor use on board certificate Form 2092a requires to be transcribed by the Societys surveyor into FormCG3 in order to warrant international acceptance In addition the loose gear shall be stamped with the newcertificate number
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7262 Register book
72621 As described in [137] the test certificates Form CG3 are added to the register book of liftingappliances carried on boardUpon request by the operator an individual register book for each piece of loose gear can be issued for useon board more than one ship
72622 For all examinations according to [7252] the Societys examination report will be compiled Inaddition the examinations are confirmed in the register book of lifting appliances
72623 Certificates Form 2092a will be handed out to the operator without a register book The operatorshall add these certificates and examination reports according to [72624] to his own documentation
72624 The confirmation of examinations of loose gear for which a test certificate Form 2092a has beenissued is effected by the examination report
73 Interchangeable components
731 General notes
7311 Accessories according to [1151] are regarded as interchangeable components
7312 Although not stated in [1151] eye plates and bolt connections shall be treated as interchangeablecomponents
732 Design and construction
7321 Block frames shall be designed in such a way that ropes cannot get caught between the sheave andthe block cheeks
7322 Cargo hooks shackles swivels and rings shall be forged Exceptions to this rule require the consentof the Society
7323 Grades of cast steel shall be selected according to recognised standards The consent of the Societyis required in every instance for other grades of cast steel
7324 Galvanization is permitted only with forged components of fully killed steels Galvanization of forgedinterchangeable components may take place only after the load testing of the componentsWhere delivery is carried out by a recognised manufacturer it shall be documented that a stress test hasbeen conducted at the manufacturer under application of the minimum test loads in accordance with DNV GLrules including crack test
7325 The galvanizing of cold-formed components is permitted only if the suitability of the material for thispurpose has been proved
733 Interchangeable components conforming to recognized standards
7331 Verification by calculation is not required in respect of interchangeable components which conform torecognized standardsDeviating from Table 3-1 and [7334] the materials of their load bearing components can be attested byinspection certificates 31 as per ISO 10474
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7332 Determination of the nominal loadThe nominal load is determined depending on the location of service without partial safety factors and hoistload coefficients
mdash in the loading gear acc to Sec5 load combination Imdash in the loose gear acc to [7233] load combination I
Where applicable the nominal load determined as above shall be multiplied additionally by a dynamic factorfd acc to [7334]
7333 For interchangeable components conforming to standards a choice shall be made according to theindicated nominal sizes The nominal sizes correspond to the nominal load acc to [7332]
7334 In all cases where the hoist load coefficient ψ is greater than the value of ψzul the permissible loadon which the choice of the nominal size is based shall be increased by the following dynamic factor fd
ψ = hoist load coefficient acc to [52]ψzul = permissible hoist load coefficient acc to Table 7-3
Table 7-3 Permissible hoist load coefficient ψ
LNe ψzul
up to 60 t 16
above 60 t to 160 t
above 160 t 11
734 Basic principles for proofs for interchangeable components notcorresponding to a recognized standard7341 General notes
73411 For the calculation and the dimensioning of interchangeable components the requirements given inSec4 and Sec6 apply
73412 The load for dimensioning is determined depending on the location of service taking intoconsideration partial safety factors and hoist load coefficients
mdash using load combinations for the lifting appliance acc to [55]mdash using load combinations for the loose gear acc to [7233]
Additionally the static test load LPstat acc to Table 7-4 with a partial safety factor of γpi = 110 shall beobserved for the determination of the load for dimensioning
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7342 Proofs
73421 General734211 Basis for the dimensioning is the applicable design load for dimensioning which shall bedetermined acc to [73412]734212 The calculation of non-standardized interchange-able components may be carried out usingsuitable calculation methods acc to the provisions in Sec4734213 A method to determine the strength of non-standardized eye plates is given in [7343]734214 Proof of bolt connections may be provided acc to [482]
73422 Strength analyses and proofs of stabilityFor strength analyses generally the statements in [44] and [48] apply They shall be conducted using thedesign load for dimensioning
73423 Proofs of fatigue strength734231 For the proofs of fatigue strength the statements in [46] apply In general they shall beconducted using the load combination I of Table 5-4 or Table 5-1 with the partial safety factor γpi = 10734232 For interchangeable components with load cycles le 20000 the proof of fatigue strength may bedispensed with
7343 Non-standardized eye plates
73431 The determination of the dimensioning stress for eye plates which correspond to Figure 7-6 andto the boundary conditions acc to [73432] may be performed using the following method unless a moreprecise proof is provided
Figure 7-6 Eye plate
R = outer radius of head [mm]r = bore radius [mm]c = cheek width [mm]e = change of head height [mm]t = plate thickness [mm]
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β = inclination angle of flanks [deg]ϑ = angle of force attack [deg]rB = bolt radius [mm]T = clearance between bolt and bore [mm]a = head height [mm]S(γpi middot Li) = design load for dimensioning [kN]
73432 Boundary conditionsFor the dimensioning the following boundary conditions shall be adhered to
a) I) Radii ratio ρ of the eye
b) II) Clearance T boltbore
T = 2 (r ndash rB) le 02 middot r le 3 mmFor bolt diameters of 50 to 300 mm a clearance between bolt and bore of 3 to 6 mm can be permittedHowever in this case the design load shall be increased by 5
a) III) For moving bolt connections a wear of DT = 2 mm shall be taken into consideration in the strengthanalysis
b) IV) Inclination angle of flanks 0deg le β le 45degc) V) Angle of attack 0deg le ϑ le β
73433 Determination of the stress for dimensioning and stress proofThe stress for dimensioning is calculated as follows
σd max = α middot σN
α = form factor as per [73435]σN = nominal stress as per [73434]
It shall be proven that
σd max le Rd
with
73434 Nominal stress due to design loadThe nominal stress due to design load without friction component is calculated as follows
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with
(see also Table 7-1)
FN = nominal load on eye plate
c = R + e sin β - r
The nominal stress component due to friction (friction coefficient micro) between bolt and bore is calculated asfollows
Consequently the nominal stress due to the design load including friction component is calculated as follows
73435 Determination of form factorIn general the form factor is calculated as follows
with
(base value)
(components due to inclination of flanks)
(components due to change of heat height)
(components due to angle of attack)
and (radii ratio)
(change of head height ratio)
73436 Connection to supporting structureThe connection to the supporting structure (see Figure 7-6 cross section ko-ck) shall be proven separately inaccordance with Sec4
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735 Examination of drawings and supervision of construction7351 Examination of drawings
73511 Examination of drawings is not required in respect of interchangeable components and eye plateswhich conform to recognized standards
73512 Details or drawings shall be submitted for examination in respect of interchangeable components oreye plates which are made of materials andor to designs which do not conform to a standard
73513 Where such interchangeable components or eye plates shall be repeatedly manufactured therelevant drawings may also be approved as works standards Where reference is made to such worksstandards in the documents submitted the date and journal number of the Societys approval shall also beindicated
7352 Supervision of constructionThe supervision of construction is not required for interchangeable components and eye plates
736 Tests and examinations7361 Tests
73611 Interchangeable components736111 Before being assembled or put into use interchangeable components in the unpainted and asfar as possible ungalvanized condition shall be subjected to a static load test in the presence of the Societyssurveyor performed on a calibrated and approved testing machine using the test loads given in Table 7-4736112 Where the origin of interchangeable components is unknown or certificates for the materialsare unavailable the Societys surveyor is entitled to demand that one specimen of the interchangeablecomponent undergo a tensile test at 4 times the permissible loadThe specimen shall withstand this load without breaking A further increase to the load until the specimenbreaks is not generally required However the Societys surveyor is entitled to demand a test to establish theactual breaking loadSpecimens which have undergone tensile testing at 4 times the permissible load are overstressed and shallbe destroyed or recycled after the test736113 After changes or repairs to interchangeable components a load test according to [736111]shall be repeated736114 Regularly repeated load testing of individual parts of interchangeable components is notprescribed internationally by ILO They are load tested together with the lifting appliance or loose gear towhich they are fastened
73612 Eye plates736121 Eye plates which are integral parts of lifting appliances and loose gear are included in the loadtests of them736122 Eye plates for assembly and maintenance work as well as for transportation purposes require astrength analysis with respect to their welding joints and the supporting structures These analyses will bechecked within the scope of examination of drawingsLoad tests with agreed static test loads may be conducted on request of the ships owner
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7362 Examinations
73621 Interchangeable components736211 The manufacturer and dealer shall present all interchangeable components to the Societyssurveyor in an unpainted and if possible ungalvanized condition for examination of the dimensions andworkmanship together with the certificates covering the materials used736212 After the static load test each component is thoroughly examined by the Societys surveyor andshall if the surveyor considers it necessary be taken apart for closer scrutiny736213 After start of operation every interchangeable component shall be subjected to an examinationby the Societys surveyor at least every 12 months as well as to a thorough examination every 5 years Forhighly stressed components non-destructive tests may be carried outComponents shall if the surveyor considers it necessary be taken apart for closer scrutiny
73622 Eye plates736221 Eye plates which are integral parts of lifting appliances and loose gear are examined togetherwith them736221 Eye plates according to [736122] including their joints are examined before their firstemployment after every load test and at agreed intervals736223 Examinations of eye plates may be complemented by crack and ultrasonic tests uponagreement These examinations are mandatory if the visual inspection during the examination gives reasonto do so
737 Documentation7371 Interchangeable componentsFor marking see [74]
73711 Certificates737111 The Societys surveyor issues a certificate for each interchangeable component which hassuccessfully undergone a load test and a thorough examinationThis certificate gives details of the manufacturer or supplier the date of the test special materials (extra highstrength low temperature) the size of the test load and the permissible load737112 The Societys Form CG3 is used for shipboard lifting appliances gear or interchangeablecomponents and the Societys Form 7103a for all othersFor the transcription of Form 7103a into Form CG3 for use on board the requirements given in [72613]apply as and where relevant737113 For closer definition of tested and examined components the following details are entered onthe certificates
mdash shacklesbolt diameter where the inside width is non-standard the following dimensions shall be indicated in theorder shown diameter of the shackle in the middle of the bow bolt diameter and inside width
mdash cargo hooks and swivelsnominal size
mdash blocksgroove diameter of the sheave and the sheave pin diameter together with the type of head fitting and anindication of whether or not a becket is fitted
mdash double yoke piecesbolt diameter and length of the double yoke piece between the bolt centres
mdash rope socketsnominal size and details of the material test
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mdash cable jointsnominal size
mdash rigging screwsnominal size or thread diameter and the type of bolt head (oval eye round eye or fork eye)
mdash chainsdiameter of the round steel bar external width of the chain link and length of the chain
737114 Where interchangeable components are manufactured to approved drawings the certificatesalso indicate the relevant drawing together with the date and the Societys reference number of theapproval
73712 Register book737121 In accordance with the requirements given in [137] the test certificates Form CG3 are added tothe register book of lifting appliances on board737122 Interchangeable components which are integral parts of lifting appliances or loose gear areexamined together with themFor the devices examination reports are compiled and the examinations are confirmed in the register book oflifting appliances737123 For interchangeable components which are certified by Form 2092a the requirements given in[72623] and [72624] apply as and where relevant
7372 Eye plates
7373 Eye plates in accordance with [736121] are included in the documentation of the devices statedthere
7374 The tests and examinations of eye plates in accordance with [736122] are confirmed byexamination reports
Table 7-4 Static test loads for interchangeable components
Line Interchangeable components Permissible loads SWL 1 Static test loads LPstat 2
1 chains rings hooksshackles swivels etc
up to 250 tover 250 t
2 times SWL(122 times SWL) + 20 t
2 single-sheaved blockswith and without becket
up to 250 tover 250 t
2 times SWL(122 times SWL) + 20 t
3 multi-sheaved blocksup to 250 t
over 250 t up to 1600 t
over 1600 t
2 times SWL(0933 times SWL) + 27 t
11 times SWL
1) The permissible load SWL of single and multi-sheaved blocks is equal to the permissible load on the suspension2) If need be to be multiplied with fd according to [7334]
74 Marking of loose gear and interchangeable components
741 Manufacturers plateLoose gear according to [11531] shall be fitted with a manufacturers plate which shall include at least thefollowing information if applicable
mdash manufacturers name
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mdash type of loose gearmdash serial numbermdash year of constructionmdash characteristics where applicable such as eg nomi-nal pressure nominal voltage filling volume etcmdash nominal load(s)mdash dead loadmdash with lifting beams traverses and spreaders a symbol for the inclination angle of the allocated suspension
ropes or chains
742 Stamping7421 General notes
74211 Stamping is regarded to be the proof of a test andor examination Loose gear and interchangeablecomponents shall therefore undergo (renewed) load testing if a certificate is required in this regard
74212 The stamp height shall be at least 6 mm
7422 Loose gear
74221 Scope of stampingAll loose gear which has successfully undergone testing and thorough examination is stamped as follows
mdash certificate number together with the code letters of the examining inspection officemdash stamp 3 with the month and year of testingmdash Safe Working Load in tonnes or kg preceded by the letters SWLmdash dead load in t or kg preceded by the letters WT
74222 The stamp shall be applied on one side in a prominent position if possible in the centre but not concealedby the marking
74223 742231 Loose gear subjected to supervision of construction at the manufacturers premises is double-stamped (see Table 7-5)742232 After periodic load tests and re-issuing of test certificates stamping is not repeated
7423 Interchangeable components
74231 Scope of stamping742311 Each interchangeable component which has successfully undergone testing and thoroughexamination is stamped as follows
mdash certificate number together with the code letters of the examining inspection officemdash stamp 3 with the month and year of testingmdash permissible load in tonnes or kg preceded by the letters SWLmdash permissible rope hoist in tonnes or kg with blocks eg
mdash single-sheaved block without becket SWL 6 trope 3 t
mdash single-sheaved block with becket SWL 15 trope 5 t
mdash multiple-sheaved blocks SWL 64 twith 4 sheaves rope 8 t
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Table 7-5 Examples of stamping and marking
Documentation Loose gear Interchangeablecomponents
CertificateForm7103a Acceptance testing L 8924 H03 3 15
StampingCertificate FormCG3 or 7103a Load test L 2429 H04 3
15SWL 30 tWT 5 t
L 6743 H02 3 15SWL15 trope 5 t(single-
sheaved block with becket)
Marking Rigging plans SWL 30 tWT 5 t ---
Abbreviations Nominal loadSWL Weight WT Permissible loadSWL
742312 With interchangeable components made of special materials the stamp is extended with thefollowing letters if applicable
mdash H for extra high strength materialmdash T for low-temperature materials
Where interchangeable components are composed of several single parts which may be disassembled suchas eg shackle hook and shackle round nut each part will get this special stamp
74232 Stamp locationThe stamp shall be applied to the following locations for the parts given below
mdash shacklesto one of the limbs close to the eye
mdash cargo hooksto the side of the hook close to the suspension
mdash swivelsto the traverse the oval eye only gets the anchor stamp
mdash blocksto the side bar if any otherwise to the side plate close to the point of suspension of the block
mdash double yoke piecesto the middle of one side
mdash rope socketsto the conical section opposite the existing stamp for material testing
mdash cable jointsto the middle of one side
mdash rigging screwson the body to every eye head fitting or double lug head fitting plus the Societys stamp
mdash suspension ropes and slingsto a permanently fastened small metal plate
mdash chainsto the last link at each end
74233 742331 With a permissible load up to 15 t the figure on the stamp shall be rounded to one decimalplace With values of 15 t and over the figure shall be rounded to a whole number742332 For the galvanization of forged interchangeable components the requirements given in [7324]apply The stamp shall still be recognizable after galvanization or where required it shall be re-stamped
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742333 The stamp height shall be at least 6 mm or 4 mm for small parts742334 On small parts to which it is difficult or impossible to apply the whole stamp the month and yearof testing may be omitted followed if necessary by the certificate number and the permissible load whererequiredThe following is applicable for stamping of small parts
mdash components with a SWL of 16 t and overThese are stamped in full as described in [74231]
mdash components with a SWL between 025 t and 10 tThese only receive the Societys stamp and where required also the permissible load
mdash components with a SWL of less than 025 t SWLThese only receive the Societys stamp and where required the stamp shall be waived
743 Marking of loose gear
7431 Loose gear shall be permanently marked in a prominent position on both sides in the mannerdescribed in [7432] and [7432]The inscription shall comprise characters at least 80 mm in height the permanence of which shall be assuredby punching by applying weld seams or small metal plates adequately fastened The fatigue strength of themarked components shall not be unduly impaired by these measuresGlued-on lettering foils are not permitted
7432 Lifting beams traverses and spreaders shall be marked as follows
mdash nominal load SWL in t or kgmdash dead load WT in t or kg (mandatory if over 100 kg)mdash special types of fastening or loading
7433 Grabs and lifting magnets shall be marked as follows
mdash nominal load SWL in t or kgmdash dead load WT in t or kgmdash capacity in m3 for grabs
75 Wear damage repair
751 Loose gear
7511 With respect to tolerable reduction in the plate thickness due to rusting or wear the requirementsgiven in [1362] apply
7512 With respect to a reduction in the nominal load of loose gear covered by [11531] as an alternativeto removal from service in the event of damage inadmissible wear or other causes the requirements givenin [1369] apply
752 Interchangeable components
7521 Interchangeable components such as bolts chains rings etc as well as eye plates shall bereplaced if the parts are visibly deformed if the diameter is reduced by 10 at some points or if the area ofthe load-bearing cross-section is reduced by 20
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7522 The use of welding to repair cracks in or worn portions of interchangeable components is generallynot permitted The same applies to bolts and other removable elements of loose gearThe Society reserves the right to approve such repairs in special cases Then the following shall be observed
75221 After repair of forged interchangeable components evidence shall be provided that heat treatmenthas been carried out
75222 After repair of interchangeable components a load test in accordance with [736111] isrequired
75223 Renewal of axes bolts and rope-sheaves in general does not require rerunning of the load tests
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SECTION 8 ROPES AND ROPE ACCESSORIES
81 General
811 Scope
8111 The following requirements apply to wire and fibre ropes used as running and standing rigging forshipboard lifting appliances and loose gear as well as for rope slings
812 Approval for manufacture
8121 With regard to manufacture and quality assurance rope manufacturers shall have been approved bythe SocietyThe Societys approval is given provided that the requirements for the manufacture testing and marking ofwire ropes set out in RU SHIP Pt2 is complied with
8122 For approval the manufacturer shall amongst other things prove during a tour of the works thatthe necessary equipment is available for the proper manufacture and testing of ropes The Society reservesthe right to demand that a qualification test be performed on specimen lengths of rope
8123 Approved rope manufacturers can also be approved for testing and certificating ropes on theirown authority Upon receiving this extended approval the Society assigns the manufacturer a special codenumber
82 Wire ropes
821 General requirements
8211 Wire ropes shall conform to recognized standards such as eg EN 12385
8212 For employment on deck wire ropes for running rigging shall be drawn galvanized and wire ropesfor standing rigging shall be fully galvanizedAfter being galvanized the ropes shall be impregnated and conserved with non-thermosetting and acid-freegrease in order to avoid penetration of water and subsequent corrosion
8213 Galvanized wire ropes with diameters of less than 8 mm are not permitted for shipboard liftingappliances and loose gear exposed to the weather
8214 Free rope ends shall be sized tapered or socketed to prevent fraying of the rope ends or to preventchanges in the lay lengths of the rope and strands
8215 Special rope designs Lang lay ropes ropes with a nominal tensile grade of more than 1960 Nmm2 and ropes of austenitic or stainless materials may on application be approved provided that they aresuitable for the proposed use
8216 Wire ropes of stainless materials shall be suitable for use in marine atmospheresTo avoid crevice corrosion the materials used for the wires shall have a sufficiently high chromium andmolybdenum content
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Steels are regarded as resistant to crevice corrosion in a marine atmosphere if the sum W is 29 or overwhere
W = Cr [] + 33 middot Mo [] ge 29
8217 Ropes with a nominal diameter exceeding 5 mm shall at least consist of 100 single wires runningrigging shall at least have 6 strands
822 Definitions
8221 Running rigging refers to all ropes passing over rope sheaves or guide rolls or wound on winchesirrespective of whether or not the ropes are moved under load
8222 Standing rigging refers to all wire ropes which are not turned round or wound on to winches suchas shrouds stays pendants etc Standing rigging shall be fitted with thimbles or rope sockets
8223 Rope slings refer to ropes not forming an integral part of lifting appliances or loose gear which areused to attach loads and can be employed without special adaptation or fitting operations
8224 The calculated breaking load Fr of a rope is the product of the theoretical metal cross-section and thenominal tensile strength of the wires
8225 The minimum breaking load Fmin of a rope is the product of the calculated breaking load Fr and theSpinning Factor ks
8226 The actual breaking load Fwi of a rope is the load determined by a tensile test to destruction of thecomplete rope
8227 The proven breaking load Fn of a rope is the product of the measured aggregate breaking load Feand the spinning factor ks
8228 The measured aggregate breaking load Fe of a rope is the sum of the individually determinedbreaking loads of all the wires in the rope ascertained by tensile tests
8229 The spinning factor ks is an empirical factor which takes account of the strength reduction due tostrandingThe spinning factors of established types of wire rope are given in relevant standards or manufacturersinformation
823 Dimensioning
8231 The breaking load FBr of wire ropes for loading gear and loose gear shall not be less than the productof the Rope Tension FS and one of the safety factors γDi shown in Table 8-2
FBr ge FS middot γDi
FBr = actual breaking load Fwi or proven breaking load Fn
8232 The Rope Tension FS is the maximum force calculated for load condition I1 disregarding the hoistload coefficient ψ but taking into consideration the losses due to friction and bending in the rope sheaves Inaddition the following shall be observed
82321 For the partial safety factors γpi = 10 may be applied
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82322 The determination of rope tensions taking into consideration the sheave friction and bendingresistance of the ropes is based on a frictional coefficient of 5 per turn for friction bearings and 2 perturn for anti-friction bearingsWhere calculations shall be performed with smaller frictional coefficients special proof of these shall beprovided
82323 Rope deflection angles due to static ship inclinations do not increase the hoisting rope forceEnforced rope deflection angles due to acceleration forces or eg the drift of a vessel result in an increase inthe hoisting rope force They can however within the scope of this standard be ignored when dimensioninghoisting ropes or rope slings
82324 When dimensioning luffing ropes and standing rigging the deflecting angles of hoisting ropes shallbe considered in principle if they effect an increase in rope forces
82325 For shipboard lifting appliances and loose gear where an increased hoist load coefficient (gt ψzulS)shall be applied the rope tension FS shall be multiplied by the dynamic factor fds For ψzulS and fdS see[82326] and Table 8-1 This applies in particular to lifting appliances which will be dimensioned only forsea operation (see [5432]) or for lifting appliances in grab operation
82326 The factor for consideration of an increased dynamic to be used for calculation of the rope tensionshall be determined as follows
ψ = hoist load coefficient according to [54]ψzulS = permissible hoist load coefficient according to Table 8-1
Table 8-1 Permissible hoist load coefficient ψ
LNe ψzulS
up to 10 t 16
over 10 t up to 160 t
over 160 t 15
82327 Where the efficiency of rope end joints is below 80 the loss of breaking force shall becompensated up to 80
82328 Wire ropes for multi-rope grabs shall be dimensioned in addition to the dead weight of the grabfor the following nominal loads LNe
mdash closing rope double lever control LNemdash closing rope single lever control 23 LNemdash holding cable 23 LNe
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8233 Reduction in breaking load of the ropeWhere wire ropes are wound around design elements with a small diameter (eg shackle bolts crane hooksload connecting elements etc) the permissible breaking load shall be reduced
D = diameter of the slung partd = rope diameter
The breaking load of the wire rope shall be reduced for the following range of diameters
1 le Dd le 9
(Dd lt 1 is not permissible)
The reduced breaking load shall be determined according to the following formula
FBr redu = reduced breaking loadFBr = breaking load of the non-deformed rope (no rope bending)
Within spliced sections the rope shall not be slung with small radii
Alternative provisions for the dimensioning of wire ropes for ramps and car decks can be found in [6341]
824 Requirements for rope drives8241 Interaction between ropes and rope drums
82411 In determining the necessary length of wire ropes and the length of drum it shall be borne inmind that at least 3 safety turns shall remain on the drum at all timesThe requirement for 3 safety turns also applies to luffing ropes with respect to the stowing position of thecrane boom
82412 It shall be ensured that ropes are wound up properly on the rope drums The length of rope drumsshall in general be designed such that no more than 3 layers of rope may be wound on top of each otherWhere the number of layers exceeds 3 a special coiling device or other system or equipment shall beprovided
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Table 8-2 Safety factors for wire ropes
Safety factors γD1 1
Nominal load (LNe) of loading gear and loose gear 2 Running rigging
up to 10 t 5
over 10 t up to 160 t
over 160 t 3
Safety factors γD2 1
Nominal load (LNe) of loading gear and loose gear 2 Standing rigging
up to 10 t 4
over 10 t up to 160 t
over 160 t 3
Safety factors γD3 1
Weight of load Rope slings 3
up to 10 t 6
over 10 t up to 160 t
over 160 t 36
1) If applicable to be multiplied with fdS (see [82325]2) For goods lifts lifting platforms ramps and car decks the following loads shall be applied
mdash operation without useful load dead loadmdash operation with useful load dead load + nominal load
3) Rope slings which are not turned round may be treated as wire ropes for standing rigging provided that both endsare fitted with thimbles or rope sockets
82413 Uncut rope drums may only be used with the consent of the Society
82414 Grab cranes shall have a rope-spindling guide in principle if the hoist rope drum cannot be clearlyviewed by the operator at all times Rope-spindling guides are grooved drums and rope-spindling devices andsimilar devices
82415 Design requirements for rope drums are described in [952]
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82416 Wire ropes which are wound on to drums in several layers shall have a steel core For heavy loadsropes with compressed strands are recommended
82417 The first rope layer shall be tension loaded
82418 The direction of rope runout shall be coordinated with the direction of rotation of the drums toavoid twisting of the ropesThe winding direction of ropes on rope drums shall be clearly recognizable at the drums and where requiredthe winding direction shall be indicated
8242 Rope-sheaves
82421 Design features shall prevent ropes from being jammed between rope-sheaves and side plates orleaving the rope grooveThe distance between the upper edge of rope-sheaves and eg side plates shall not exceed 13 with plasticrope-sheaves 14 of the rope diameter or 8 mm at most
82422 With respect to steel materials for assembled rope-sheaves all normal strength steels with provennotch toughness are suitableFor cast rope-sheaves the steel casting type GE200 acc to EN 10293 (previously GS-38 acc to DIN 1681)or cast iron type EN-GJS-400-18-RT with proven notch toughness or EN-GJS-400-18-LT acc to EN 1563(previously GGG-403 acc to DIN 1693 or corresponding types with cast test pieces
82423 Where plastic rope-sheaves are used they shall be type-tested In the case of single layer spoolingon the rope drum at least the sheave which generates most of the alternating bends in the rope shall beproduced from steel Alternatively defined criteria for scrapping or usage periods may be approved
82424 The following requirements apply to the design of rope grooves
mdash depth of groove ge radic2 times nominal rope diametermdash diameter of groove 106 to 108 times nominal rope diametermdash opening angle 45deg to 60deg
Table 8-3 Minimum diameter of rope-sheaves and rope drums
Rope drum diameter 3Applicationcrane group 2
Rope-sheavediameter 3 minimum Ungroovedminimum Groovedminimum
Nominal tensilestrength of wire ropes 4
Wire ropes notoperated under load 9 ds 10 ds 9 ds 1570 Nmm2
A 18 ds 20 ds 16 ds 1770 Nmm2
B 20 ds not permitted 18 ds 1770 Nmm2
C1 22 ds not permitted 20 ds 1770 Nmm2
C2 + C3 25 ds not permitted 22 ds 1770 Nmm2
1) In case of rope-sheaves and machined drums measured in the bottom of the groove2) For crane group definition see [52]3) Where non-rotating or poorly-rotating ropes are used it is recommended that the diameters indicated be increased
by 104) Where ropes with a higher nominal tensile strength are used the prescribed diameters shall be increased
proportionally
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DNV GL AS
8243 Diameter of sheaves and rope drumsThe required rope-sheave and rope drum diameters relative to rope diameter ds shall be as shown in Table8-3For all other types of wire ropes the ratio shall be agreed with the Society in each individual case
8244 Lateral deflection angle of the rope
82441 The lateral deflection of wire ropes relative to the plane of the groove in the rope-sheave or ropedrum shall not be greater than 114 (4deg)
82442 In the case of poorly-rotating ropes the lateral deflection angle shall not be greater than 128 (2deg)
82443 Exceptions to the above requirements are made for unwinding hoist ropes Special wear-reducingdesign measures shall be taken for lifting appliances at sea frequently
8245 Employment of swivelsSwivels shall only be employed with poorly-rotating ropes
83 Fibre ropes
831 General requirements
8311 Synthetic fibre ropes shall comply with DNVGL OS E303Natural fibre ropes shall comply with recognized standards On application special rope designs may beapproved
8312 Fibre ropes (of natural or synthetic fibre) except carbon fibre ropes may be used for standingrigging and for running rigging of special lifting appliances which is stressed moderately subject toagreement with the SocietyFibre ropes may also be used for the cargo tackles of landing booms according to [663] and for rope slingswith the exception of carbon-fibre ropes The agreement of the Society is required for other applications
8313 Synthetic fibre ropes shall be stabilized with respect to light and heat
8314 Free rope ends shall be yarn-wound to prevent disintegration of the rope structure Synthetic fibreropes may be partially melted
832 Definitions
8321 The terms running rigging standing rigging and rope sling as well as the term actual breakingload Fwi are defined in [822]
8322 The proven breaking load Fn of a fibre rope is the load calculated from the breaking load of theyarns contained in the rope multiplied by a reduction factorThe proven breaking load Fn of a synthetic fibre rope is determined by testing in accordance with therequirements of DNVGL OS E303
8323 The reduction factor is an empirical value which takes account of the loss of strength due tostrandingThe reduction factors of the best-established fibre ropes are given in the DNV GL rules listed in [8121]
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833 DimensioningIn the case of fibre ropes used for loading gear and loose gear the breaking load FBr shall not be less thanthe product of the static rope tension FS and one of the safety factors γF given in Table 8-4
FBr ge FS middot γF
FBr = required breaking load of the rope analogous to [8231]FS = rope tension acc to [8232]
Table 8-4 Safety factors for standardized fibre ropes
Nominal diameter of rope [mm] Coeffient of utilization γF
10 ndash 13
14 ndash 17
18 ndash 23
24 ndash 39
40 and over
12
10
8
7
6
For non-standardized fibre ropes γF shall be agreed with the Society
Synthetic fibre ropes shall be dimensioned with respect to their 3-T endurance and shall comply with DNVGLOS E303
Synthetic fibre ropes shall be operated according to their designated service The designated servicefor synthetic fibre ropes shall assure that adequate margins are maintained towards exceeding the 3-Tendurance and other relevant failure modes DNVGL ST E407 can be taken as guidance
The 3-T endurance and other aspect of dimensioning of synthetic fibre ropes are outlined in DNVGL RP E305
834 Requirements for rope drives
8341 Synthetic fibre ropes shall not be used on capstan heads or other devices where a major slippagemay occur
8342 Fibre ropes shall only be wound up in one layer Winding shall be performed under tension
8343 The required rope-sheave diameters relative to the nominal rope diameter ds shall be as shown inTable 8-5For non-standardized fibre ropes the rope sheave diameter shall be agreed with the Society
Table 8-5 Minimum diameter of rope-sheaves for standardized fibre ropes
Rope material Rope-sheave diameter minimum
manila hemp
polypropylene
polyamide
polyester
carbon-fibre
55 ds
4 ds
6 ds
6 ds
14 ds
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8344 The required diameters of rope drums shall be agreed with the Society in each case For carbon fibreropes 12 ds shall be taken
8345 The lateral deflection of fibre ropes relative to the plane of the groove of rope-sheaves or rope drumsshall not be greater than 114 (4deg)
8346 The number of safety turns remaining on rope drums shall not be less than [85] In case ofsynthetic fibre ropes a higher number of safety turns may be required
84 Rope-end attachmentsRope-end attachments shall be designed in accordance with recognized standards eg the following
841 Splices for wire ropes and fibre ropes
8411 Wire ropes and fibre ropes shall not be made up of parts spliced together
8412 Loop splices (eye splices) and thimble splices shall conform to standard EN 13411-2 or be ofequivalent designThe dimensions of thimbles shall comply with standard EN 13411-1 (Shaped steel thimbles for wire ropes)or standard EN DIN 6899 (Steel thimbles for fibre ropes) as appropriate
8413 Provided that [82411] and [8346] are met rope ends connected to winches may be splicedwithout thimbles see [9526]
8414 Splices of any kind are not permitted for cranes of types B and C because of their inadequatefatigue strength
8415 Splices shall not be sheathed
842 End attachments for wire ropes8421 Rope sockets
84211 Rope sockets (open and closed sockets) into which wire rope ends shall be socketed shall conformto standard EN 13411 On application other designs may be approved
84212 The socketing process using metal or plastic resin shall be performed as prescribed in standard EN13411-4 and may only be carried out by companies which have been approvedOnly approved cast materials may be used Rope sockets shall be marked with the code letter of themanufacturing company
8422 Wrought ferrules
84221 Wrought aluminium alloy ferrules shall conform to EN 13411-3Flemish eyes as per DIN 3095 shall be used wherever possible for the end attachments of the hoisting andluffing ropes of lifting appliances if the lifting appliances are working with grabs
84222 On application swaged or rolled end fittings (terminals) may be approved
84223 Application of ferrules in accordance with [84221] and [84222] may only be carried out byapproved companies Ferrules shall be marked with the code letter of the manufacturing company
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8423 Detachable end joints
84231 Cable joints (wedge clamps) may only be used if the ropes are permanently under tension Theyshall be clearly visible and readily accessible to facilitate inspectionThe free end of the rope shall be secured from being pulled through eg by rope sockets The safeguardconnection of the rope end to the load-bearing part of the rope shall not be force-transmitting However itshall be capable of bearing 10 of the rope tension FSCable joints shall correspond to EN 13411-6 Up to a rope diameter of 8 mm EN 13411-7 may also beapplied
84232 Rope sockets as per EN 13411-5 are not permitted This does not apply to the securing of free ropeends to cable joints
84233 With regard to the attachment of rope ends to winch drums the requirements given in [9526]and [9527] apply
85 Tests and examinations
851 Supervision of manufacture8511 Wire rope and fibre ropes
85111 General notes851111 With regard to testing and examination of ropes the requirements given in the DNV GL rules asstated in [8121] apply851112 Instructions for the testing and use of ropes and an excerpt from the Societys rules for wireropes and fibre ropes shall be found on the reverse sides of the Societys certificates for ropes
85112 Tensile testsAfter manufacturing ropes shall be subjected to a tensile test which is mandatory for the issue of theSocietys certificate The following applies851121 Ropes shall be loaded to destruction in their entirety Where the tensile force of the testingmachine is not sufficient to perform a tensile test for the whole rope individual wires or yarns shall be loadedto destruction in a prescribed procedure and the breaking load of the rope determined by calculation851122 The results of the tensile tests of the ropes shall achieve the values prescribed in the relevantrope standards851123 Tensile tests of ropes shall be performed in the presence of the Societys surveyor if
mdash the manufacturer is not approved by the Society to test and issue certificates on his own authoritymdash special rope designs are not covered by the Societys approvalmdash the customer requests it
851124 Before each tensile test the protocols on the checks performed by the manufacturer shall bepresented to the Societys surveyor851125 Following every tensile test checking the diameter tolerances method of manufacture andmanufacturers protocols the Societys surveyor will issue a certificate of test and thorough examination ofwire rope or fibre rope using one of the forms stated in [8621]
85113 MarkingRopes shall be marked by woven-in identification bands and coloured identification threads The followingshall be taken into account851131 The identification band shall carry the name or mark of the manufacturer and in the case of theSocietys approval in addition the manufacturerrsquos identification number assigned by the Society
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DNV GL AS
851132 The colour of the identification thread gives information about the nominal tensile strength ofwires or the type of yarn used (identification colour)851133 The coloured identification thread may be dispensed with if the identification band itself carriesthe identification colour
8512 End attachments
85121 End attachments which are not standardized or do not correspond to standards are subject to anexamination of drawings
85122 With regard to tests and examinations of rope sockets cable joints and terminals the requirementsgiven in [735] apply For terminals it may be required to produce specimens connected to a small length ofrope
85123 In the case of short ready-made units the rope sockets and terminals can be load-tested togetherwith the rope
852 Initial testingRopes and their end attachments are subject to a visual examination and a check of the relevant certificateswithin the scope of the initial testing of lifting appliances
853 Periodic testing8531 Wire ropes and fibre ropes
85311 In the scope of the periodic testing of lifting appliances and loose gear the ropes shall be examinedby the Societys surveyor with regard to condition and fitness for use
85312 When ropes are examined attention shall be paid to deformation crushing corrosionrottennessand broken wires If necessary the ropes shall be twisted open for an internal examination
85313 Special attention shall be paid to the end attachments There broken wires or yarns shall beexpected with wire ropes also corrosion especially with downward hanging end attachments Sheathingsshall be removed for examination
85314 Sheaves used for length compensation within tackle where a rope only seems to be resting areparticularly prone to wire ruptures caused by regular compensation motions
85315 Where splices have become loose the ropes shall be shortened and spliced again or whererequired replaced
8532 End attachmentsWith regard to end attachments the requirements given in [85311] apply Attention shall be paid to wearcracks and corrosion
8533 Ropes to be discarded
85331 Wire ropes853311 Wire ropes shall be discarded when over a length equal to 8 times the rope diameter ds thenumber of detected broken wires is greater than 10 with Lang lay ropes 5 of the total number of wiresin the rope
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DNV GL AS
853312 Wire ropes shall also be discarded when
mdash the rope diameter ds being reduced owing to friction or wear by more than 10 of the nominal diameteror in case of wear to the core
mdash corrosion (external or internal)mdash deformations of the rope such as bird caging formation of loops buckling kinking crushing loosening
of individual wires or strands etc
853313 Wire ropes which are regularly employed under water shall be shortened in the vicinity of theloose gear (eg the hook) at least once per year in order to enable the cut-off end which should have aminimum length of 1 m to be thoroughly examined and subjected to a tensile testIf the remaining breaking load is below 80 of the original breaking load the rope shall be discarded Ifthe remaining breaking load is 80 or above the original load an estimate shall be made based on thecondition and the period of employment whether the rope may be employed for another year853314 Wire ropes employed above deck shall be discarded at the latest after the following periods ofemployment even when no external damage is visible
mdash running rigging 10 yearsmdash standing rigging 15 years
Wire ropes may be employed for a longer period of time if a Certificate of Fitness has been issued by arecognized rope company or by the rope manufacturer after a thorough examination
86 Documentation
861 Marking8611 Wire ropes and fibre ropes
86111 Ropes are marked by the method described in [85113]
86112 With regard to ropes the rope tension Fs calculated according to [8232] shall not be less thanthe permissible load SWL stamped on the end attachments
86113 With regard to ropes with splices a small metal plate stamped in accordance with [7423] shallbe fastened near an end attachment
8612 End attachmentsEnd attachments for wire ropes are stamped like interchangeable components see [7423] Whereapplicable this is also possible on ferrules or terminals taking account of [84233]
862 Certificates8621 Wire ropesAfter the tension test approved manufacturers or in cases described in [851123] the Societys surveyorwill issue one of the following the Societys test certificates
mdash wire ropes Form CG4
8622 End attachmentsWith regard to certification of end attachments the requirements given in [73611] apply
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DNV GL AS
863 Storage of rope certificatesAs described in [137] test certificates for ropes and test certificates for end attachments will be addedinitially and after each re-issue to an allocated register book on board
864 Confirmation of examinations
8641 Ropes and end attachments which are integral parts of lifting appliances or loose gear will beincluded in the examination of themFor these devices examination reports will be prepared and the examinations will be confirmed in the registerbook
8642 The confirmation of examinations of ropes and end attachments which cannot be allocated toparticular lifting appliances or loose gear will be effected by an examination report for these parts
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SECTION 9 MECHANICAL PARTS
91 General
911 General notes
9111 This section contains requirements for the mechanical parts of shipboard lifting appliances andwhere required also loose gear
9112 Complementary or more comprehensive require-ments in particular for mechanical parts notcovered hereafter shall be taken from the following rules
mdash DNV GL rulesmdash recognized standards and requirements where applicable to lifting appliances unless contrary to the
provisions in this section
9113 The requirements given in Sec1 shall be observed if applicable
9114 As regards the materials to be used the manufacture and the safety requirements the provisions inSec3 Sec11 and Sec12 apply
912 Scope of application
9121 Table 9-1 is a list of the essential mechanical parts which are subject to examination of drawings asdeemed necessary by the Society and which shall be delivered in the designated manner together with testreports or inspection certificates
9122 The requirement for an examination of drawings and the type of certificate depends on the safetyrelevance of the components with respect to their strength and reliability and on the operational mode andthe type of certification of the lifting appliances
9123 Table 9-1 reflects the general requirements given by the Society The Societey reserves the right toimpose additional requirements or to permit deviations
9124 The Society reserves the right to impose additional requirements for all kinds of mechanical partsshould this be necessary on account of new findings or operational experience
913 Differing designs
9131 Designs differing from the requirements given in this section may be approved if examined by theSociety for their suitability and approved as being equivalent
9132 Mechanical parts developed on the basis of novel technical concepts but not yet sufficiently provenrequire special approval by the Society Such systems may be subjected to more stringent supervision if theprerequisites as per [9131] are not applicable
9133 In the cases mentioned in [9131] and [9132] the Society is entitled to demand presentation ofadditional documentation and performance of special trials
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92 Design criteria and operational requirements
921 General notes
9211 Mechanical parts of shipboard lifting appliances and loose gear shall be designed for theenvironmental conditions agreed on or prescribed and be capable of being operated without problem underthese conditions
9212 The effects of deformation of the supporting structure on machinery and equipment shall beobserved
9213 Mechanical parts shall be designed in such a way that repairs and regular maintenance are easy toperform using on-board tools
922 Dimensioning
9221 Mechanical parts shall be dimensioned in such a way as to provide adequate strength in respect ofdynamic stress peaks plus adequate fatigue strength in relation to the load and service lifeWith respect to dimensioning attention shall be paid particularly to the stress peaks arising duringacceleration and retardation and if applicable the dynamic influences resulting from lifting and lowering ofloadsProof of fatigue strength may be provided in accordance with the Section I of FEM
9222 All mechanical parts shall measure up to the special circumstances of operation on board ships suchas ship movements and acceleration increased corrosion temperature changes etc
9223 With regard to structural design and fastening in general acceleration of 07 g in the frequencyrange from 13 to 100 Hz shall additionally be considered see also [9231]
923 Effects of vibration
9231 Machinery and equipment shall not cause any vibrations and shocks which may unduly stressother components or the structure of the lifting appliance and loose gear The permissible amplitudes andaccelerations are stated in the RU SHIP Pt4 Sec2
9232 If compliance with the permissible values of amplitude and acceleration cannot be ensured bystructural measures damping measures are required
9233 Within the frequency ranges which occur there shall be no resonance phenomena in componentssupport- and suspension arrangements - nor within equipment
924 Lubrication
9241 Lubrication of the moving parts of lifting appliances and loose gear shall be guaranteed under alloperating conditions
9242 Each grease-lubricated bearing shall be provided with its own proven type of grease nipple
9243 Accessibility to manual greasing points shall be ensured
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925 Corrosion protectionComponents at risk of corrosion shall be given suitable corrosion protection
93 Power drivesThe requirements given in [92] shall be observed In addition the following applies
931 Drives in general
9311 Power drives shall be adequately dimensioned for the working conditions laid down to allow trouble-free and low-vibration operation
9312 For electrical drives and electrical controls in general the requirements given in Sec10 areapplicable
932 Main drives
9321 Main drives of shipboard lifting appliances shall be dimensioned in such a way that the installedpower meets the requirements given in [9311] for all combinations of motion and speedWhere the installed power is not sufficient to execute all motions simultaneously at nominal load and at fullspeed the speed shall be reduced automatically
9322 Diesel engines shall not be capable of running at excessive speeds or being stalled
94 Slewing gears and slew rings
941 Slewing gears
9411 Slewing gears shall be designed for maximum operating torque and where the gears are of a self-locking type they shall be equipped with a slewing gear brake
9412 Slewing gears on board ships shall be designed in such a way that in the event of the vesselspermissible inclination being exceeded by 5deg none of the materials employed shall be stressed beyond 90of its yield point
9413 In the case of slewing gears on board ships it shall be taken into account that it might be necessaryin the out of operation condition to reduce the load on the slewing gear brakes by means of locking devices
9414 Slewing gears of shipboard cranes working at sea state shall be dimensioned for at least 13 timesthe design torque based on wind transverse tension and inclination of the cranersquos base and shall have atleast 2 independent drives
942 Slew rings9421 Large roller bearings
94211 The design of large roller bearings shall together with the connecting structures and the bolting besuitable for the intended operation and the intended environmental conditions
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DNV GL AS
94212 The connecting flanges on the loading gear and foundations shall be adequately distortion-resistant their surfaces machinedAccuracy of plane and distortion shall be within the tolerances stated by the manufacturerThe mating surfaces shall be steel to steel Casting of synthetic material is permitted only in exceptionalcases and requires the Societys approval in each individual case see [574124]
94213 Large roller bearings shall be designed in such a way that a failure of important runway elementsdoes not result in a total loss of the lifting appliance
94214 If large roller bearings have to be dismantled during employment for an internal examinationspecial dismantling equipment shall be available which can hold the lifting appliance and raise it after theconnecting bolts have been unscrewedAs an alternative the lifting appliance shall have special eyebolts for lifting by another appliance and a safeplace for setting-down
94215 Where an interchange of seals is intended large roller bearings shall be designed such that this isenabled without dismantling of the bearings or loosening of the connecting bolts
94216 With respect to the materials to be used as well as their heat treatment and proof of mechanicalproperties the requirements given in [134] apply
9422 Bolting of large roller bearingsIn addition to [5741] the following applies
94221 The fixed ring at the foundation or at the crane column shall be bolted at even intervals around itscircumference
94222 For bolting of the rotating ring to the lifting appliance uneven bolt intervals may be applied if thesafety of such bolting is verified by calculation or measurement
94223 The distance between the bolts shall in general not exceed 6 times the bolt diameter
94224 The requirements for the bolts are as follows942241 Up to a diameter of le 30 mm bolts may be preloaded according to the instructions of the slewrings manufacturer by applying a torqueFor larger diameters preloading shall be by hydraulic elongation This calls for increased thread tolerances942242 With respect to the materials to be used for the bolts as well as the proof of their mechanicalproperties
9423 King pins and support rolls
94231 If not safe by design lifting appliances shall be secured against overturning by king pins andsupport rolls also with rolls which engage from below where required
94232 The rotating system shall meet the following requirements
mdash support rolls shall be installed in a stationary positionmdash support rolls and king pins shall be easily accessible for maintenance and inspection support rolls also for
exchange purposesmdash after failure of one support roll even under load the lifting appliance shall still be capable of being turned
into a secure position
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DNV GL AS
95 Winches
951 Design notes
9511 Winches shall be of a reversible type ie the lowering process shall also be motor-controlled
9512 Design features incorporated in each winch shall ensure that the load cannot run back inadvertently(eg by a ratchet wheel self-locking gears non-return valves automatic brakes etc)
9513 The use of belts or friction discs to transmit power between the winch drum and the reverse travelprevention device referred to in [9512] is not allowed
952 Rope drums
9521 The drum diameter shall be determined in accord-ance with the intended purpose of the winch inaccordance with [8243] or a recognized standard
9522 The calculated hoop stress of winch drums σh shall not exceed 85 of the material yield stress
9523 Rope drums shall be provided with flanges whose outer edges extend above the top layer of rope byat least 25 times the rope diameter unless the rope is prevented from overriding the flange by a spoolingdevice or other meansIt shall be ensured that ropes can wind onto drums properly and without excessive deviation
9524 The number of safety-turns left on the rope drum shall not be less than 3
9525 Rope grooves shall comply with the following requirements
mdash groove diameter ge 105 middot rope diameter dsmdash groove depth ge 033 middot rope diameter ds
9526 In the case of multiple winding wedges at the flanges shall facilitate the ropes onto the second layerunless special measures are provided such as
mdash small lateral deflection ge 15degmdash cable guidesmdash Lebus grooving
9527 Rope-end attachments at the winch drum shall be designed in such a way that
mdash the ropes are not pulled over edgesmdash the end fastening cannot be released unintentionallymdash the end fastening is easy to inspect
If the end attachment of wire ropes is based on clamping at least 3 clamping plates shall be usedThe construction of end attachments for fibre ropes shall be agreed with the SocietyFor nominal loads up to 12 t and lifting appliances which are only occasionally loaded spliced rope loops canalso be used
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DNV GL AS
9528 The following conditions shall be met for the minimum required rope tension force Fa at the drum
95281 Shipboard lifting appliances
FS = rope tension as per [8232]γD1 = safety factor for wire ropes as per Table 8-2 (where applicable [8233] shall be observed)μ = coefficient of friction between rope and drum Applicable values are
mdash smooth drum μ le 008mdash grooved drum μ le 010
α = wrap angle For 3 turns isα = 6 middot π
95282 Shipboard lifting appliances working at sea state
FBr = rope breaking load according to [8231]
The Societys may also demand this rope tension for other lifting appliances if this is employed under similaroperational conditions eg for floating cranes operating at sea
953 Brakes
9531 Each winch shall be fitted with a braking device capable of braking and holding the maximumpermitted load safely under all operating conditions and this action shall not generate inadmissible dynamicinfluencesThe minimum friction coefficient of the brake shall not exceed 03 in the design calculationThe winch and its substructure shall be able to safely withstand the forces set up during braking
9532 Having regard to the dynamics of the braking action the braking torque shall exceed the maximumload torque by an adequate safety margin As a guide the maximum braking torque may be set at about80 above the maximum load torqueIf need be fdS according to [82326] shall be considered
9533 The required braking device may take the form of
mdash self-locking gearmdash mechanical brake with brake pads or brake discsmdash a hydraulic or pneumatic device which prevents lowering of the load ormdash electromotive brake
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DNV GL AS
and shall be actuated when
mdash the control returns to the neutral positionmdash a safety device comes into actionmdash the power supply fails ormdash on hydraulic installations a non-scheduled pressure loss occurs
9534 Hydraulic retention brakes shall comply with the following requirements
mdash The shut-off valve of hydraulic motors shall activate at the low-pressure connection in the case ofpressure loss
mdash Hydraulic motors shall have a shut-off valve hydraulic cylinders a valve according to [9624] which shallbe fitted directly at the high-pressure connection
mdash A hydraulic motor and cylinder shall always be fed with a sufficient quantity of working fluid also the fluidsupply in the event of power failure eg by gravity
mdash Shut-off valves and valves according to [9624] shall be capable of absorbing the pressure impactscaused by braking
9535 Electromotive brakes additionally require a mechanical holding brake (drum brake or spring-loadedmotor brake)
9536 Braking devices shall be designed in such a way that on the one hand they may be adjustable onthe other the designed braking effect cannot easily be interfered with Due to humidity oils or impuritiesbraking power shall not decrease below the design valueWhere a gear box is arranged between brake and drum the load-bearing components shall be dimensionedlike the corresponding components of a brakeSpring-loaded braking pads or discs shall be loaded by pressure springsChecking wear to braking pads or discs shall be possible without dismantling the braking unitSelf-blocking brakes are only admissible for stowage or idle positions
9537 The following requirements apply to shipboard cranes and floating cranes operating at sea state andwhich transport persons
95371 In addition to the normal working brake hoisting and luffing winches shall be fitted with asecondary brake which is independent in terms of mechanical and operational layout
95372 Secondary brakes shall have their own independent control circuit and at least be dimensioned towithstand loads as per [425]
954 Winch drives9541 Power drivesFor power drives the requirements given in [93] and [9614] apply
9542 Manual drives
95421 Manual drives shall incorporate the following features
mdash The crank handle turns in the same direction for all gear ratiosmdash Crank handles have a crank radius of approximately 350 mm and a rotatable grip sleevemdash Detachable crank handles are safeguarded against being detached unintentionallymdash The load is hauled in manually with a force of max 160 Nmdash A speed of about 30 revmin-1 is not exceeded
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95422 Where winches are constructed for both powered and manual operation the power- and manualsystems shall be mutually interlocked
955 Couplings
9551 Clutch couplings between the drive and the rope drum are only permitted where one of the means toprevent runback stipulated in [9512] has been provided
9552 Where winches have more than one disengageable drum only one drum shall be in operation at anytime
9553 Control levers shall be safeguarded against unintentional operation
956 Gearing
9561 The design of gearing shall conform to established engineering practice location positioning andmode of operation shall be taken into account
9562 Gearing shall amongst others include the following characteristics
mdash easy access for maintenancemdash facilities for checking the oil levelmdash ventilation- and oil filler pipes appropriate to the locationmdash inspection openings
957 Controls and monitoring instruments
9571 The controls and monitoring instruments shall be clearly arranged on the control platform
9572 Controls and monitoring instruments shall be permanently clearly and intelligibly marked with thedirection or the function of the movements they control see [1242]
9573 The arrangement and direction of movement of controls and monitoring instruments shall match thedirection of the movement which they control
9574 The operating movement range of control levers shall be less than 300 mm and when released theyshall return automatically to the neutral position
9575 In the case of push-button controls there shall be a separate button for each direction of movement
96 Hydraulic systems
961 General requirements
9611 The dimensioning and design of hydraulic systems shall conform to the established rules ofengineering practice Safe operation under all envisaged service conditions shall be ensured by suitableequipment (eg filters coolers control devices and primary pressure control) and by selecting anappropriate hydraulic fluid
9612 Hydraulic systems shall be protected against overpressure and against overspeed of the load by acorresponding limitation of flow rate and pressure
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9613 Instead of pipes high pressure hoses may be used These shall comply with the requirements givenin EN 13135-2 or an equivalent standardThe hoses shall be suitable for the proposed operating fluids pressures temperatures operating andenvironmental conditions and be appropriately laid and of an approved design
9614 For hydraulically-powered winches a standstill brake to prevent slip is required if necessitated by theconstruction of the winchAny slip occurring shall generally not exceed the equivalent of one revolution of the drum or 1 m hooklowering per minute whichever is the lesser
962 Hydraulic cylinders
9621 Hydraulic cylinders shall be dimensioned for 11 times relief pressure pc and dynamic forces which mayoccur in and out of service
9622 The relief pressure pc of the safety relief valves shall be set at a sufficiently high level that dynamicforces which may occur can be absorbed and hoist load coefficients are considered
9623 Piston rods shall be sufficiently rigidly connected to the piston or telescopic rod in order to meet therequirements for calculation given in [4923]The stroke of the piston rods shall be limited by end stops which shall be capable of preventing the pushing-out of the piston rods even at the utmost pressure and dynamic load If necessary devices for terminaldamping or end limitation shall be provided
9624 With telescopic cylinders extending and run-in of the telescopic rods shall be conducted in aspecified order
9625 Load-bearing hydraulic cylinders eg for lifting luffing folding and telescoping of crane booms aswell as for slewing of lifting appliances shall be provided with a device which maintains the position of theload the crane boom or the lifting appliance in the event of pressure loss and failure of a pipe or hose lineSuch a device may be an automatic shut-off brake valve a pilot-operated check valve or a load holdingvalve and shall be installed inside or outside directly at the cylinder
9626 The type of fastening and the design of the bearings shall safeguard that no unacceptable externalbending moments can be transmitted to the hydraulic cylinders
963 Hydraulic tanks
9631 Regarding dimensioning of hydraulic tanks tasks like eg cooling (radiation of heat) eliminating airand depositing contaminants shall be taken into consideration At the same time the container shall be ableto accommodate the total amount of oil in the system
9632 Hydraulic tanks shall be fitted with
mdash fluid level indicator (including minimum and maximum values)mdash access openingmdash outlet valvemdash ventilation
Design operational and environmental conditions may in addition require cooling andor heating of thetanks
9633 Pressure tanks shall be capable of withstanding a 2-fold maximum working pressure and shall have asafety valve against overpressure
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DNV GL AS
97 Protective measures and safety devices
971 Protective measures
9711 Moving parts flywheels rope and chain drives rods and other components which might come toconstitute an accident hazard for the handling staff shall be provided with protection against accidentalcontact The same applies to hot mechanical parts pipes and walls not provided with insulation
9712 Measures shall be taken to provide power supply lines with effective protection against mechanicaldamage
9713 Cranks for starting internal combustion engines shall disengage automatically once the engine startsrunning
9714 Machinery employed in potentially explosive areas shall comply with the requirements given in EN13463-1
972 Safety devices
9721 Winches and drive systems shall be equipped with adjustable protection devices (eg pressure reliefvalves winding and slip clutch thermal overload relays) Following a power failure drives shall not restartautomatically
9722 Devices provided to unlock slewing or hoisting gear are only permissible for special operationalpurposes or as emergency measures eg on offshore cranes
9723 Safety devices shall not be rendered unserviceable by environmental conditions at the point ofinstallation because of dirt or springs breaking There shall be a means of checking the devices
98 Examination of drawings and supervision of construction
981 Examination of drawings
9811 The general requirements given in Sec2 shall be observed
9812 In addition the mechanical parts listed in Table 9-1 are subject to examination of drawings withinthe scope indicated there
982 Supervision of construction9821 General notes
98211 Mechanical parts shall be manufactured by staff qualified in handling the installations and devicesnecessary During manufacture and before delivery the parts shall undergo the quality tests required inaccord-ance with state-of-the-art technology and experience
98212 All materials shall be suited to the intended purpose Proof of the mechanical properties of thematerials used shall be furnished Identification of the materials shall be possible on the basis of testcertificates or reports
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98213 Mechanical parts which require an inspection certificate 32 according to Table 9-1 are subject tosupervision of construction by the Society with the restrictions described in the explanations to Table 9-1where required982131 The Society inspection in charge decides in coordination with the manufacturer on type andscope of supervision of production and certification taking the in-house quality control andor approval forproduction into consideration982132 With respect to assistance by the manufacturer during supervision of production by the Societythe requirements given in [1322] shall be observed
9822 Tests and examinationsThe following requirements contain general test requirements and in addition provisions for the supervisionof production by the Society
98221 General notes982211 For the acceptance tests before delivery and if applicable also for the supervision of productionthe Societys surveyor shall be given material test and internal control certificates test reports andmanufacturing documents in particular approved drawings including the relevant examination reports as aprerequisite for the tests and examinations described below982212 Test reports shall include the following information if applicable
mdash designation of type and nominal dimensionsmdash purchase and order num-bermdash drawing numbermdash results of internal controlsmdash certificate numbers of material tests and non-destructive testsmdash additional details as necessary
982213 For series-production components other test procedures may be agreed with the Society insteadof the prescribed ones if they are accepted to be equivalent982214 The Society reserves the right to extend the scope of testing if necessary and also to subjectsuch components to a test for which testing is not expressly required in this standard982215 Where mechanical parts shall be used for the intended purpose for the first time the Societymay ask for a type approval
98222 Winches982221 After completion winches shall be subjected to an examination and functional test at nominalrope tension by repeated hoisting and lowering of the nominal load During the functional test in particularthe brake and safety devices shall be tested and adjusted982222 Where winches are designed for a holding force greater than the nominal rope tension thenominal rope tension shall be tested dynamically and the holding force statically982223 Where winches are designed with a constant tension device the maintenance of constanttension shall be proven for all levels of tension set by the design982224 The above tests including the setting of the overload protection can also be performed onboard together with the functional testing of the lifting appliance In this case a functional test at availableload shall be performed at the manufacturersTesting of winches at test load will be performed within the scope of initial tests of the lifting appliance see[1333]
98223 Load-bearing hydraulic cylinders982231 Load-bearing or 1st order components are hydraulic cylinders designed for hoisting luffingtelescoping and slewing982232 Load-bearing hydraulic cylinders shall undergo a functional test at relief pressure and a pressuretest at test pressure The test pressure shall be 15 times relief pressure pc however with relief pressuresover 200 bar it need not be higher than pc + 100 bar
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982233 With reference to [9625] in the case of series-production of lifting appliances of the sametype and with multiple cylinders eg with slewing cranes with luffing folding andor telescopic crane boomsa regular check on the cylinders at a minimum of 125 times the relief pressure may be acceptedThe Societys surveyor is entitled to ask for cylinders to be tested which are selected at random inaccordance with [982232]
98224 Large roller bearings982241 The material properties of forged rings shall be tested according to the DNV GL rules formaterials by tensile tests and by notched-bar impact tests and shall comply with the requirements given inthe agreed specificationThe manufacturer shall in addition ultrasonically test the rings for internal defects and certify that thematerials are free from defects which may impair the performance characteristics982242 Rings shall be heat-treated as appropriate to the material and the running surfaces shall behardened additionally After hardening the runway surfaces of the rings shall be crack-tested along theirentire lengthCracks may be removed by grinding if by this measure the functional capability of the slewing ring is notimpaired Residual cracks are not permitted The Societys surveyor may demand the crack test be performedin his presence982243 The hardened runways shall undergo a hardness test at least 8 points equally distributed alongthe circumference The hardness values shall be within the specified rangeWhere there are reasonable doubts about the hardened depth proof shall be furnished using specimenswhich have been hardened under the same conditions as the ring under consideration982244 For the acceptance test before delivery the large roller bearing shall be assembled andpresented to the Societys surveyor The functional capability (slewing without load) the bearing clearanceand the accuracy in plane and round travelling are thereby to be tested In addition the dimensions shall bechecked randomly as deemed necessary by the surveyor
98225 Bolts and nuts for large roller bearingsWith respect to tests and examinations of bolts and nuts the DNV GL rules for metallic materials RU SHIPPt2 applies
98226 Mechanical and hydromechanical parts982261 With respect to tests and examinations of mechanical and hydromechanical parts DNV GL rulesRU SHIP Pt4 apply where relevantParts not covered by DNV GL rules shall be tested and examined using appropriate procedures agreed withthe Societys surveyor982262 Instead of testing at the manufacturers tests can also be performed on board within the scopeof initial tests of the lifting appliance if practicable
99 Documentation
991 Marking
9911 Each mechanical part shall be marked by the manufacturer in a suitable way The marking shall atleast include the following if applicable
mdash manufacturers namemdash year of constructionmdash designation of typemdash purchase order number or serial numbermdash characteristics such as nominal load nominal pressure nominal voltage etcmdash additional details as necessary
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9912 If after the acceptance test before delivery the requirements for issuing a test certificate of Form092a are complied with the tested mechanical part will be stamped in a prominent positionThe stamp shall include the following information
mdash certificate number together with the code letters of the examining inspecting officemdash stamp with the month and year of testing
for hydraulic cylinders additionally
mdash working pressuremdash testing pressure
for winches additionally
mdash rope tension [kN]mdash holding force [kN]
for slewing gear rings additionally
mdash abbreviation for the material typemdash melting charge numbermdash specimen number
9913 The winding direction of ropes on rope drums shall be clearly recognizable on the drumsWhere required the winding direction shall be indicated appropriately on the drum or winch
992 Certificates
9921 Table 9-1 shows the required types of certificates for essential mechanical partsThe lifting appliance manufacturer shall order the stated parts together with the required certificates theparts manufacturer shall include them in the delivery
9922 The inspection certificate 32 shall be issued by the Society The Societys surveyor uses form2092a
9923 The certificates listed in Table 9-1 are not part of the lifting appliance documentation on board
Table 9-1 Examination of drawings and certification of mechanical parts
Shipboard liftingappliances in general
Shipboard lifting appliancesoperating at sea state
Shipboard liftingappliances on vesselswith CRANE notationComponents
Examinationof drawings Certificate Examination
of drawings Certificate Examinationof drawings Certificate
Winch drum Z minus Z minus Z minus
Winch mounting Z minus Z minus Z minus
Winch complete unit I 22 Z PC 1 Z PC 1
Hydraulic cylinderload-bearing Z PC Z PC Z PC
Slewing rings Z PC 2 Z PC 2 Z PC
le M52 I 22 I 31 I 31Bolts and nutsfor slewing rings gt M52 I 22 I 31 I PC
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Shipboard liftingappliances in general
Shipboard lifting appliancesoperating at sea state
Shipboard liftingappliances on vesselswith CRANE notationComponents
Examinationof drawings Certificate Examination
of drawings Certificate Examinationof drawings Certificate
King pinsupport rolls Z 22 Z 31 Z PC
Slewing gear complete unit I 22 Z 31 Z PC
Cylinder Z 22 Z 31 Z PCSlewing gear
Rack bar Z 22 Z 31 Z PC
Luffing gear (Cylinder spindle) Z PC Z PC Z PC
Travelling gear complete unit Z 22 minus minus Z 31
Main drive (diesel) minus 22 I 31 I 31
le 50 kW minus 22 I 22 Z 31Hydromotorsand pumps gt 50 kW minus 22 Z 31 Z PC
le 40 barle 32 DN
minus minus I 22 I 22
Pressure linesgt 40 bargt 32 DN
minus minus I 22 I 31 3
Safety valvesagainst pressure loss I 22 I 22 I 22
Hydraulic hose lines minus 22 I PC 4 I PC 4
Hydraulic fittings minus 22 I 22 I 22
Ventilatorsheat exchangers minus 22 I 31 Z PC
Sheaves I 22 I 31 Z PC
Swell compensators minus minus Z PC Z PC
Damping devices minus minus Z PC Z PC
Explanations
mdash The column Shipboard lifting appliances in general may also be applied to loose gear as and where relevantmdash Z means drawings and calculationsmdash I means documents for informationmdash The designation of the certificate types corresponds to ISO 10474 The numbers mean the following certificatesmdash 22 test report (the Societys designation C-type Certificate)mdash 31 inspection certificates (the Societys designation B-type Certificate)mdash PC DNV GL product certificate (VL) see RU SHIP Pt Ch3 Sec5 [24]
1) At the manufacturers at least 1 functional test is required see [982224]2) Certificate of type 31 if the manufacturer is approved by the Society3) The certificate shall confirm the performance of a pressure test at 15 times the nominal pressure4) Certificate of type 31 if the manufacturers of both the hose as well as the hose line are approved by the Society
and proof is furnished of a pressure test at 2 times the nominal pressure
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DNV GL AS
SECTION 10 ELECTRICAL EQUIPMENT
101 General
1011 General notes
10111 This section contains the requirements for electrical equipment of shipboard lifting appliances andwhere applicable also of loose gear
10112 Additional or more comprehensive requirements eg for switch cabinets and for electricalequipment not covered hereafter can be taken from the following
mdash DNV GL rulesmdash recognized standards and regulations where applicable to shipboard lifting appliances unless contrary to
the requirements given in this section
10113 The requirements given in Sec1 shall be observed where relevant
1012 Scope of application
10121 Table 2-1 is a list of the essential electrical equipment which is subject to examination of drawingsas deemed necessary by the Society and which shall be delivered together with test reports or inspectioncertificates
10122 The requirement for an examination of drawings and the type of certificate depend on the safetyrelevance of the equipment with respect to its suitability and reliability and on the operational mode andorthe type of certification of the shipboard lifting appliances
10123 In case of founded exceptions also the approval and certification of electrical equipment not listedin Table 2-1 to Table 2-3 can be required if they are exceedingly relevant for the safety andor reliablefunction of the lifting appliance
1013 Deviating designs
10131 Designs differing from the requirements which follow may be approved if examined by the Societyfor their suitability and deemed equivalent
10132 Electrical equipment developed on the basis of novel technical concepts but not yet sufficientlyproven requires particular approval by the Society Such equipment may be subjected to more stringentsupervision if the prerequisites as per [10131] are not fulfilled
10133 In the cases mentioned in [10131] and [10132] the Society is entitled to demand presentationof additional documentation and performance of special trials
10134 The Society reserves the right to impose additional requirements for all kinds of electricalequipment should this be necessary on account of new findings or operational experience
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102 Design criteria and operational requirements
1021 The electrical control and switch gear as well as the motors shall be designed or arranged in such a waythat necessary maintenance of contacts contactors collectors slip rings brakes etc can be carried out withmeans available on board
1022 Switch and control cabinets as well as motors arranged on deck shall be provided with adequate heating forthe standstill condition if sufficient internal space is available
1023 When choosing electrical equipment the expected environmental conditions such as humidity heat cold andvibrations shall receive special consideration In addition the following applies
10231 In general acceleration of 07 g in the frequency range from 13 to 100 Hz shall also be taken intoaccount as regards design and mounting
10232 Plug-in cards with electronic controls may have to have extra fastenings
1024 Where special circuits for lighting standstill heating etc are fed through separate power supply switches sothat they can also be operated when the main supply to the lifting appliance is switched off special measuresshall be taken in the switchgear to prevent direct contact with live parts A double feed shall be indicated bylabels
1025 For supply lines fixed laid to shipboard lifting appliances including the external fixed cabling marine cableshall be used as per RU SHIP Pt4 Ch8 see [322]
1026 An adequate power supply shall be provided on board or if applicable onshore Onshore power supply shallbe adapted to the supply system onboard
103 Drives and brakes
1031 Driving power
10311 All motors shall be dimensioned in accordance with their envisaged purpose and expected use
10312 In the case of shipboard lifting appliances the working speeds laid down for the nominal load shallbe maintained also at the vessels prescribed minimum inclinations
10313 The required power for winches is calculated from the rated pull and the rated rope speed of thefirst layer of rope on the drum taking gearing efficiency into account
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1032 Winch drivesFor winch drives the following operating modes Si are defined
10321 For drives up to about 5 t LNe started very frequently (about 160-400 starts per hour) with shortload travel and lifting periods duty type S5 ie intermittent periodic duty with electric braking with thestarting process and electrical braking influencing the heating-up of the motor
10322 For drives with long load travel and lifting periods and less frequent starts (up to about 160 startsper hour) duty type S3 ie intermittent periodic duty without the starting and braking processes having anynoticeable effect on the heating-up of the motor
10323 For heavy loads with prolonged load handling and lengthy intervals duty type S2 ie short-timeduty with an ensuing interval long enough for the driving motor to cool down approximately to the ambienttemperature Preferred duration of duty is 30 min
10324 In the case of hydraulic drives the electric motors driving the pumps shall be matched to the givenconditions Possible operating modes are S1 (continuous running) or S6 (continuous operation periodic duty)In the case of mode S6 particular regard shall be paid to the mode of operation of the hydraulic unit egthe power required during idling
10325 The driving motors shall be capable of running-up at least 13 times against the rated torqueWhen designing the motors the moment of inertia of the gearing shall be taken into account The moment ofinertia of the driven masses shall be based on an inertia factor FJ of at least 12
10326 The duty types S1 to S3 S5 and S6 are defined in IEC 60034-1 In addition the following applies
103261 When operating in type S5 at least 160 starts per hour shall be possible This is based on theassumption that 50 of the starts will be without load
103262 Where the requirements are more stringent than [103261] the drives shall be designed for240 320 or 400 starts per hour
10327 For operating modes S5 and S3 differing duty times shall be assumed depending on the serviceconditions For the operating steps a total operating period of 25 of the overall total shall be considered Inaddition the following applies
103271 In the case of more stringent requirements than given in [10327] (shorter intervals betweenthe separate hoisting operations) duty times of 40 60 or 75 shall be chosen
103272 In the case of pole changing motors where all the speed steps are designed for the rated loadand where generally the top speed step is reached by switching through the individual lower steps theoverall operating period shall be shared out between the individual switching steps
103273 If one of the speed steps is intended for light-hook operation only the overall operating periodapplies only to the operating steps However the light hook step shall be designed for at least 15 of theoverall operating period
1033 Brakes
10331 The frequency of operation of the brakes shall correspond to that of the associated motor It isassumed that when operating braking will only ever be effected from a low-speed stepThe braking equipment shall function automatically and arrest the load with the minimum possible impact
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DNV GL AS
10332 Winches shall as a matter of principle be equipped with safety brakes which brake the load safelyat any speed if the power supply fails
104 Cables and lines
1041 Supply line
10411 As a matter of principle power shall be supplied via suitable cables possibly using cable trolleys orcable drums with integral slip ringsAll cables and lines shall be flame-resistant and self-extinguishing Furthermore all cables shall be approvedby the Society possibly UV-radiation resistant and where hydraulic systems are concerned oil resistant
10412 Devices eg cable drums introduced to prevent the lines dragging on the floor during operationshall be designed in such a way that the inner bend radius of the cables does not remain under the followingvalues unless otherwise stated by the cable maker
mdash in the case of cables with an external diameter up to 215 mm 5 times the cable diametermdash in the case of cables with an external diameter exceeding 215 mm 625 times the cable diameter
1042 Wire cross-sections
10421 Dimensioning shall take the load into account possibly giving consideration to an utilisation factorand the expected ambient temperature
10422 For lifting appliances with only one driving motor particularly with electro-hydraulic drive systemsthe power supply shall be dimensioned as appropriate to the rated current at the maximum operating stagefor continuous operation
10423 For lifting appliances with several motors for calculation of the amperage 100 of the powerof the hoisting unit motor plus 50 of the power of all remaining drives may be used as a basis Theamperage resulting shall be applied as the continuous operation valueThese values also apply to the dimensioning of slip ring bodies and brushes
1043 Laying of cables10431 General notes
104311 Fastening for cables shall measure up to the vibrations expected during loading gear operation
104312 Cables suspended from cable trays or running vertically shall if secured by means of plasticstraps as a matter of principle also be fastened in this area with corrosion-resistant metal clips or metalstraps at intervals of at least 1 m where they pass from one tray to another
104313 Openings for passing through cables shall be deburred and lined so that the cable sheathingcannot be damaged by sharp edges
104314 Leakage of hydraulic oil into control cabinets switchgear and cable boxes shall be avoidedtherefore wherever practicable cables shall be introduced into the boxes or cabinets from below Wherethey are introduced from above they may have to be additionally sealed in areas exposed to the risk of oilleakage in an appropriate way
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10432 Cable trays
104321 Cables shall be laid on adequately strong corrosion-resistant cable trays Exceptions to this arepossible when laying single cables eg to light fittings
104322 Cable trays shall be arranged so that hydraulic oil from hydraulic systems cannot drip onto thecables Where this is not possible oil guards shall be provided
10433 Cable bundles
104331 In revolving cranes or in swing cranes with a limited slewing range all circuitssupply lines maybe led in via flexible cable bundles suitably arranged in the rotational centre of the crane column
104332 Suspended cable bundles shall be appropriately led at both ends over curved cable trays with aradius of curvature not less than 10 times that of the thickest cable and fastened there in such a way thatthe weight of the bundle is distributed as evenly as possible over all the cables depending on their size
104333 Cable bundles shall not strike or rub against anything during slewing and in the event ofmovement of the lifting appliance lifting appliance parts or the ship
1044 Cable drums and cable trolley trays
10441 Drum-wound cables shall be dimensioned in such a way that even with the cable fully wound onand under normal operating power load the cable does not heat up beyond its permitted limit
10442 For cable trolleys minimum bend radii are as follows
mdash cable up to 8 mm outside diametermdash 3 times the conductor diametermdash cable up to 125 mm outside diametermdash 4 times the conductor diametermdash cable over 125 mm outside radiimdash 5 times the conductor diameter
10443 In the case of flat cables the thickness of the cable corresponds to the outside diameter of roundcables
105 Switches
1051 Crane main switchescrane circuit breakers
10511 Shipboard lifting appliances shall be fitted with a manually operated circuit breaking device withwhich all movement can be stopped It shall be possible to isolate all the electric equipment from the mainsusing the circuit breaking device The circuit breaking capacity shall be sufficient to switch off simultaneouslyboth the power of the largest motor when stalled and the total power of all other consumers in normaloperationThe off-position shall be capable of being locked The off position shall only be indicated after havingreached the prescribed air and creepage distances The circuit breaking device shall only have one on andoff position with dedicated arresters
10512 A circuit breaking device may also be used as a load switch if it permits the maximum short-circuit power to be switched off safely Dimensioning shall be carried out in accordance with IEC Publication60947-4-1 Type 2
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10513 In the case of electro-hydraulic lifting appliances the load switch shall also switch off power to thehydraulic pump motor(s)
1052 Limit switches
10521 The control circuits of the safety limit switches shall be designed on the closed-circuit currentprinciple or shall be self-regulating
10522 In the case of automated or programme-controlled motion processes (including use ofmicroprocessor systems) the continued safe functioning of movement limitation systems shall be ensuredeven in the event of a fault or malfunction in the computerThis may be achieved by using separate control elements or additional main frame independent electronicunits insofar as these have been approved by the Society and the switching has been qualified as safe bythe Society as regards its safety aspect (fault elimination assessment)
10523 In programme-controlled movement processes limit switches may not be used for operationalspeed or movement measurement
10524 Where the hazard analysis has shown that a second movement limiter shall be provided failure ofthe first limiter shall be indicated to the crane driver
106 Protective measures and safety devices
1061 Protective measures
10611 In general the operating voltage for motor drives should not exceed 690 volts and for controlsheating and lighting systems 250 volts Insulation shall be all-pole
10612 All equipment with a working voltage exceeding 50 volts connected via movable cable shall beearthed via a protective conductor inside the cable The following shall be observed
106121 For cable cross-sections up to 16 mm2 its cross-section shall match that of the main conductorsfor those exceeding 16 mm2 it shall be at least half that of the main conductors
106122 If power is supplied via slip rings the protective conductor shall be provided with a separate slipring
10613 Any non-earthed conductor shall be provided with overload and short-circuit protection inaccordance with RU SHIP Pt4 Ch8
10614 For motors monitoring of the winding temperatures is recommended as protection againstinadmissible heating If the admissible temperature or load is exceeded power shall be switched off Switch-off due to thermal overload should be indicated Lowering of the load shall be still possible after the electricdrive has been switched off due to overheating
10615 Switches switchgear and control cabinets shall be located in such a way that work on them andoperational tests can be performed safely For arrangements inside the crane column gratings or platformsshall be provided
10616 The service passage in front of switchgear and control cabinets shall not be less than 05 m widewith 180 m headroom If this headroom cannot be maintained it may be reduced to 140 m if the passageis at least 07 m wide
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10617 As a minimum the following protective systems (contact- foreign body- and water protection)shall be provided
106171 For electrical installations below deck or in the enclosed spaces of shipboard lifting appliances theprotective system shall be at least IP 44 in dry spaces at least IP 20
106172 For electrical installations on deck the protective system shall be at least IP 56 under certaincircumstances eg where there is a heightened risk of dust even IP 66
10618 Where required electrostatic discharges shall be prevented by earthing andor connection ofmetallic components
10619 Control stands crane drivers cabins and hand-operated equipment shall be fitted withmechanically locked emergency shut-down switches or push-buttons See also the requirements given in[1243]
106110 Motors in particular for lifting and luffing gear shall be selected and protected in such a way thatin the event of power failure they do not overspeed in the time before the brakes respondEven after the response of the overspeed protection device the speed limits shall not be exceeded
106111 Electrical appliances which are employed in areas with a potentially explosive atmosphere shallcomply with the requirements given in respective international or national regulations regarding explosionprotection eg the directive 949EG and IEC 60079
1062 Safety devices10621 Controls
106211 Control handles shall be constructed in such a way that at the least the stop position engageswithout fail In systems with pole-changing motors a separate notch shall be allocated to each speed stepWhen the control handles are released they shall automatically move to the stop position
106212 Following failure of the electric power supply and when this is restored or following operationof the emergency switch-off button or push-button restarting the drives shall only be possible via the stopposition
106213 Where winch motors are provided with a speed step designed for light-hook operation only thecontrol mechanism shall automatically prevent this step operating when there is a load on the hook This alsoapplies to other part-load operating steps
106214 Radio controls programmed control mechanisms or microprocessor systems shall have been typetested by the Society Alternatively their operational safety may be proved in a different way recognized bythe Society
10622 Lighting
106221 In addition to an adequate main lighting system for the lifting appliance working area anemergency lighting system shall be provided for the cabin and the area of descent where crane columns arehigher than 10 m in the cabin at the crane column and at the switch gear and machinery
106222 Emergency lighting systems should be guaranteed to last about 30 min and shall preferably beconnected to the emergency power supply As an alternative the Society may approve a battery-operatedemergency power supply
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106223 Where emergency lighting is powered by batteries the emergency power supply chargers forthese lamps shall be connected to a separate circuit not switched off by the load-circuit switch
107 Examination of drawings and supervision of construction
1071 Examination of drawings
10711 The general requirements given in Sec13 shall be observed
10712 In addition to the requirements given in Sec13 the electrical equipment listed in Table 2-1 aresubject to examination of drawings in the scope indicated there
1072 Supervision of construction10721 General notes
107211 Electrical equipment shall be manufactured by qualified staff handling the necessary installationsand devices During manufacture and before delivery the parts shall undergo the quality tests required inaccordance with state-of-the-art technology and experience
107212 Electrical equipment which requires a product certificate 32 according to Table 2-2 and Table 2-3is subject to supervision of construction by the Society where required1072121 The Society inspection in charge decides in conjunction with the manufacturer on type andscope of supervision of production and certification taking into consideration the in-house quality controlandor approval for production1072122 With respect to assistance by the manufacturer during supervision of production by the Societythe requirements given in [1322] shall be observed
10722 Tests and examinationsThe following requirements contain general test requirements and in addition provisions for the supervisionof production by the Society
107221 General notes1072211 For the acceptance tests before delivery and if applicable also for the supervision ofproduction the Societys surveyor shall receive certificates for material tests and internal controls testreports and manufacturing documents in particular approved drawings including the allocated examinationreports if required acc to Table 2-2 and Table 2-3 as a prerequisite for the tests and examinationsdescribed below1072212 Test reports shall include the following information if applicable
mdash designation of type and nominal dimensionsmdash purchase and order numbermdash drawing numbermdash results of internal controlsmdash certificate numbers of material tests and non-destructive testsmdash additional details as necessary
1072213 For series-production electrical equipment other test procedures may be agreed with theSociety instead of the prescribed ones if they are accepted as equivalent1072214 Where electrical equipment shall be used for the intended purpose for the first time theSociety may ask for a type approval
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107222 Electrical equipmentElectrical equipment shall be tested according to RU SHIP Pt4 Ch8 and to undergo a functional test ifpossible
108 Documentation
1081 Marking
10811 Any electrical equipment shall be marked by the manufacturer in a suitable way The marking shallat least include the following information if applicable
mdash manufacturers namemdash year of constructionmdash designation of typemdash purchase order number or serial numbermdash characteristics such as nominal speed nominal voltage etcmdash additional details as necessary
10812 If after the acceptance test and before delivery the requirements for issuing a test certificate Form2092a are complied with the electrical equipment will be stamped in a prominent positionThe stamp shall include the following information
mdash certificate number together with the code letters of the examining inspecting officemdash stamp with the month and year of testing
1082 Certificates
10821 Table 2-2 and Table 2-3 show the required types of certificate for essential electrical equipmentThe lifting appliance manufacturer shall order the stated equipment together with the required certificatesand the equipment manufacturer shall include them in the delivery
10822 The inspection certificate 32 shall be issued by the Society The Societys surveyor uses DNV GLForm 2092a for this
10823 The certificates listed in Table 2-2 and Table 2-3 are not part of the lifting appliance documentationon board
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SECTION 11 CONSTRUCTION OF STEEL COMPONENTS
111 General
1111 This section contains requirements for the construction of steel components for shipload lifting appliancesand loose gear with a special focus on welding
1112 Complementary or more comprehensive requirements and special details shall be taken from the following
mdash DNV GL Rules RU SHIP Pt3mdash DNV GL Rules RU SHIP Pt2mdash recognized standards or regulations
1113 The requirements given in Sec1 shall be observed where relevant
1114 With respect to materials to be used the requirements given in Sec3 apply
112 Requirements for manufacturers
1121 General requirements
11211 Manufacturers shall be equipped with installations and devices suitable for professional and properhandling of the individual materials manufacturing methods components etcThe Society reserves the right to check the production shop in this respect and to impose requirementsconcerning this matter or to reduce the scale of operations according to the capabilities of the productionshop
11212 The manufacturer shall have a sufficiently qualified staff of experts The supervising and controllingpersonnel shall be indicated to the Society including their areas of responsibility The Society reserves theright to ask for certified proof of qualifications
1122 Quality control
11221 By means of an effective internal quality control the manufacturing works shall ensure thatconstruction and assembly comply with this standard the approved documents (drawings specificationsetc) or with the conditions stated in the approvals
11222 It is the responsibility of the manufacturing works to observe this standard and to meet the specialrequirements associated with the examination of documents or the conditions imposed with the approvalExaminations carried out by the Society do not release the manufacturing works from this responsibility
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11223 It is the responsibility of the manufacturing works to make sure that production conditions andquality correspond to those of the approval test The Society cannot take any responsibility that productscomply with this standard which have been tested in an approval test or at random during production in allparts or during the entire production process
11224 The Society may reject further use of products processes etc which have proved unsatisfactoryduring application in spite of an earlier satisfactory approval test and may demand they be improvedincluding proper verification
1123 Workmanship11231 Details in the production documents
112311 The production documents (workshop drawings etc) shall include all those details which areessential for quality and functional capability of the component under consideration This includes ndash besidesdimensions ndash eg details on tolerances surface finish quality (reworking) special production processes aswell as tests and requirements as appropriate
112312 All the important details of the welding eg the types of base material configuration anddimensions of the welds welding method welding consumables heat treatment tests to be performed andany special requirements imposed shall be indicated in the production documents (drawings parts listsetc) In special cases the Society may require submission of a welding schedule
112313 Where quality or functional capability of a component is not assured or dubious the Society mayask for suitable improvements This also applies as and where relevant to complementary or additional (egstrengthening) components even if these were not required for the examination of drawings or were notrequired due to poorly detailed presentation
11232 Cut-outs edges of plates
112321 Openings boreholes and other cut-outs shall be rounded with a sufficiently large radius
112322 The face areas (cut areas) of cut-outs shall be finished cleanly and without notches Notchesand the like due to flame-cutting shall not in general be repaired by welding but shall be ground into a flattrough Edges shall be broken or in cases of very high loads rounded
112323 Exposed edges of plates or flanges cut by flame-cutting or a shearing machine shall not besharp-edged and shall be reworked where required as stated in [112322] just as notches and the likedue to flame-cutting This applies as and where relevant to welded joints transitional sections or similardiscontinuities
11233 Cold forming
112331 Where plates are formed at low temperatures (bending flanging beading) the mean bendingradius should not fall below 3 t (t = plate thickness) it shall however be at least 2 t These values refer onlyto ship hull structural steels and comparable structural steels
112332 Before cold formation flame- or shear-cut burrs shall be removed in order to avoid cracksFollowing cold formation the components in particular the lateral ends of bent plates (plate edges) shall bechecked with respect to cracks Cracked components ndash minor cracks excepted ndash shall be set aside Repair bywelding is not permitted
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DNV GL AS
11234 Assembly straightening work
112341 During assembly of single components excessive force shall be avoided If possible majordeformations of single components shall be straightened prior to further assembly
112342 Girders stiffeners and the like which are interrupted by transverse components shall beassembled in a well aligned manner If necessary on essential components control bores shall be made forthis purpose which shall be welded closed again afterwards
112343 Straightening works ndash after completion of welding works ndash shall be conducted in such a way thatno noticeable deterioration of material properties takes place In case of doubt the Society may require atype approval or production test samples
11235 Corrosion protection
112351 All steel components shall be provided with suitable corrosion protection For shop primer see[11514] and [11515]
112352 Hollow spaces eg box girders tubular pillars and the like which are demonstrably or by generalexperience permanently air-tight need not be preserved internally During assembly the hollow spaces shallbe clean and dry
112353 The wall thickness of load-bearing parts shall be at least 4 mm Lower wall thicknessrsquos are subjectto the consent of the Society in each individual case
112354 Welded-on reinforcing rings shall be protected against rusting underneath
112355 Spring washers of corrodible materials shall not be used if exposed to the marine atmosphere
1124 Conditions for welding11241 Approval to weld
112411 All works including subcontracting firms wishing to carry out welding operations on parts ofshipboard lifting appliances and loose gear shall have at their disposal the necessary equipment and qualifiedpersonnel and be approved by the Society for this work see RU SHIP Pt2
112412 Approval for fabrication shall be applied for from the Society with the appropriate documentationExisting approval by other independent testing institutions may be taken into account if the relevantdocuments are submitted
112413 The works shall have at their disposal the necessary workshops equipment machinery anddevices to carry out the welding work properly This includes also eg stores and drying equipment for thewelding consumables and auxiliary material equipment for preheating and for heat treatment test meansand equipment as well as weather-protected areas for the outdoor execution of welding works
112414 The works shall have at their disposal qualified welders or staff sufficiently trained for handlingfully mechanical or automatic welding installations In addition they shall have at their disposal qualifiedwelding supervisors responsible for the professional execution of the welding tasks
112415 The suitability of the welding method used in conjunction with the materials in question shall beproved to the Society in an appropriate way The Society may to this end require method checks (test weldsnon-destructive and mechanical-technological tests) supervised by the Society
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DNV GL AS
112416 For the (non-destructive) testing of the weld connections suitable test procedures shall be usedand appropriately qualified testers The Society may demand a check under its supervision of ultrasonictesters The scope of tests shall be indicated in the test documentation The test reports shall be submittedto the Society
11242 Welders
112421 Welders for manual or semiautomatic welding shall be examined according to recognizedstandards (eg EN 287 or ISO 9606 or ASME Section IX) Regarding the welding method base materialwelding consumable and welding position and the test shall cover the conditions of the type of productionenvisaged
112422 A welders qualification test remains valid for two years with effect from the test date providedthat during this period welding work is constantly performed in the range of approval of the test and the workof the welder is monitored by the welding supervisors at all times
112423 The required number of qualified welders depends on the size of the works and the scope ofwelding tasks to be executed under the Societys supervision At least two qualified welders are required perwelding method
11243 Supervision of welding
112431 Every work carrying out welding shall employ its own welding supervisor This supervisor shallhave a suitable deputy in the welding shop The welding supervisor shall be responsible for supervising thepreparation and execution of the welds and if applicable their testing
112432 Supervisors shall have training and the experience appropriate to the production requirementsand furnish the necessary proofs to the SocietyAccording to the nature and scope of the welding work performed the supervisory function may be exercisedby a welding engineer (welding engineering specialist or comparably-trained engineer) a welding expert orsome other person with adequate specialist qualifications
112433 The names of the responsible welding supervisors and their deputy shall be made known to theSociety
112434 Changes in the personnel responsible for supervising welding shall automatically be reported tothe Society
11244 Welding consumables auxiliary materials
112441 Only welding consumables and auxiliary materials which have been tested and approved by theSociety shall be used with a quality grade corresponding to the base material to be welded
112442 For highly stressed components and parts stressed at low temperatures for high- and extra highstrength steels steel castings and forgings and for low-temperature welding work hydrogen-controlledwelding consumables and auxiliary materials are preferable
112443 Welding consumables and auxiliary materials for special materials may also be tested andapproved together with the welding method Such approvals are however restricted to the userrsquos works andremain valid for at most one year unless repeat tests are performedWelding consumables and auxiliary materials jointly tested in this way may be replaced by other equivalentmaterials approved for the application in question
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DNV GL AS
11245 Welding methods procedure tests
112451 Only those welding methods may be employed whose suitability for the application in question haseither been established by general practice or proved by a procedure test
112452 Procedure tests for the purpose of proving the satisfactory application of the procedure in thewelding shop and adequate quality of the results obtained shall be performed under production conditionson the premises of the company using the method in all cases where materials other than normal-strengthshipbuilding steels A to D or comparable structural steels forging steels and types of casting steel shallbe welded or welding methods other than manual arc welding (E) or partly-mechanised inert gas shieldedwelding (MAG) shall be employedProcedure tests shall also be performed where these processes are applied in a special manner eg in single-side welding using a (ceramic) weld pool support see RU SHIP Pt2 Sec1 [22]
112453 The scope of the test the samples the test specimens and the requirements shall be determinedfrom case to case depending on the proposed application in general accordance with RU SHIP Pt2 In thisconnection account may be taken of procedure tests carried out elsewhere (on submission of the reports)
112454 Welders employed for procedure tests are on successful completion of the test deemed qualifiedfor the procedure employed or the materials concerned
113 Design details
1131 General notes
11311 The materials selected for the design shall in every respect be appropriate to the designrequirements the production and the intended useIf necessary special measures shall be adopted
11312 The design of the structure shall achieve a power flow as undisturbed as possible without localdiscontinuities and steps in rigidity and to be suitable for construction and meet the requirements for long-lasting and reliable operation
11313 The following requirements refer only to welded joints For the design of screw joints therequirements given in [482] apply
1132 Configuration of welded joints11321 Welded joints in general
113211 Welded joints shall be planned in such a way as to ensure that they are readily accessible duringfabrication and can be executed in the optimum welding position and welding sequence
113212 Welded joints and welding sequences shall be designed to minimize residual weld stresses andavoid excessive deformation Welded joints shall therefore not be over-dimensioned
113213 All welded connections shall be configured to achieve a power flow as undisturbed as possiblewithout major internal or external notches or rapid changes of rigidity and without impeding expansion
113214 The requirements given in [113213] apply as and where relevant to the welding of secondarycomponents on primary structures too the highly stressed areas of which and the exposed plate or flangeedges of which shall be kept free from notches caused by welded joints if possible
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DNV GL AS
113215 Welded joints shall be designed to ensure that the proposed weld type and quality (eg completeroot fusion in the case of single- and double-bevel butt welds) can be satisfactorily achieved under the givenfabricating conditions Failing this provision shall be made for welds which are easy to execute and their(possibly inferior) load-bearing capacity shall be allowed for when dimensioning the welds
113216 Welded joints in girders and profiles (especially field joints) shall not if possible be located in anarea of high stresses Welded joints on flanges with cold formed bending positions shall be avoided
113217 Highly stressed welded joints which are therefore normally subject to compulsory inspectionshall be designed to facilitate application of the most appropriate inspection technique (radiographyultrasonic or surface crack inspection possibly in combination) so that tests offering reliable results can becarried out
11322 Welded nodes in tubular structures
113221 Depending on tube wall thickness and angle of intersection nodes linking relatively small tubeseg in tubular-frame crane jibs may be designed either in the form of fillet welds or of single-bevel welds asin [11424]
113222 The nodes of relatively large tubes where the wall thickness of the branches exceeds about 8mm shall be designed in the form of full-penetration single bevel welds as shown in Figure 11-1 Where thestress is lower single-bevel welds with a backing strip as in [11424] may also be used
113223 The weld configuration chosen and the effective weld thickness shall be taken into account in thedimensioning (especially in the proof of fatigue strength) and shown in detail on the drawings Where proofof fatigue strength is required the quality of surface finish required shall also be specified on the drawings
11323 Transitions between differing dimensions
113231 Differing dimensions shall be made to match gradually by means of gentle transitions Wheregirders or sections have web plates of different heights the chords or bulbs shall be brought to the sameheight by tapering or by slitting and splaying or reducing the height of the web plate The transition lengthshall be three times the difference in height
113232 Where the joint is between plates of differing thicknesses thickness differences of more than 3mm (see Figure 11-2) shall be evened out by bevelling the extending edge with a 13 slope or in accordancewith the notch Thickness differences of less than 3 mm may be evened out within the weld
113233 For connection to plates or other relatively thin-walled elements steel castings and forgingsas shown in Figure 11-3 shall be provided with matching tapered elements or cast or forged-on weldingflanges respectively
11324 Localised closely grouped welds minimum spacing
113241 Local close grouping of welds and short distances between welds shall be avoided Adjacent buttwelds shall be separated by at least
50 mm + 4 times plate thicknessFillet welds shall be separated from each other and from butt welds by at least
30 mm + 2 times plate thickness
113242 The width of plate areas (strips) subject to replacement shall however be at least 300 mm or 10 timesplate thickness whichever is the greater
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DNV GL AS
113243 Reinforcing plates welding flanges hubs or similar components welded into plating shall have thefollowing minimum dimensions
Dmin = 170 + 3 (t ndash 10) ge 170 mm
Dmin = minimum diameter of round or length of side of polygonal weld-on parts [mm]t = plate thickness [mm]
The corner radii of polygonal weld-on parts shall be at least 50 mm
Figure 11-1 Single-sided weld connections (tube connections not accessible from inside)
Figure 11-2 Accommodation of different thickness
Figure 11-3 Welding flange on steel castings or forgings
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DNV GL AS
11325 Welding cut-outs
113251 Welding holes for (subsequent) butt or fillet welding following the fitting of transverse parts shallbe rounded (minimum radius 25 mm or twice the plate thickness whichever is the greater) and (especiallywhere the loading is mainly dynamic) shall be provided with ldquogentlerdquo run-outs and appropriately notch-freecircumferential welds see Figure 11-4
113252 Where joints are fully welded prior to the fitting of transverse parts no welding holes are neededprovided any weld reinforcement is machined away before fitting
Figure 11-4 Welding cut-outs
11326 Local reinforcements doubling-plates
113261 Where plating is subject to locally increased loading (eg girder or pipe walls) thicker plates shallwherever possible be used rather than doubling-plates As a matter of principle bearing bushes hubs etcshall take the form of thicker welded-in plating regarding this see also [11243]
113262 Where doubling-plates cannot be avoided they shall not be thicker than twice the plate thicknessDoubling-plates wider than about 30 times the doubling-thickness shall be welded to the underlying platingby welding with cut-outs at intervals not exceeding 30 times the thickness of the doubling-plateWhen welding with cut-outs these shall preferably be designed in form of elongated holes lying in thedirection of the principal stress
113263 Doubling-plates shall be welded along their (longitudinal) edges by continuous fillet welds with athickness
a = 03 times thickness t of the doubling-plateAt the ends of doubling plates as shown in Figure 11-5 thickness a along the terminal edges shall be
a = 05 times thickness t of the doubling platethough it shall not exceed the plate thicknessThe weld transition angles between the terminal edge and the plating shall be 45deg or less
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DNV GL AS
Figure 11-5 Weldings at the ends of doubling plates
Where proof of fatigue strength is required the configuration of the end of the doubling plate shallcorrespond with the detail category selected
11327 Welding in cold-formed areas
113271 Welding is permitted at and close to structural areas cold-formed from ship structural andcomparable structural steels provided that the minimum bending radii specified in Table 11-1 are adhered-to
Table 11-1 Minimum bending radii
Plate thickness Minimum inner 1 bending radius
up to 4 mm 1 times plate thickness
up to 8 mm 15 times plate thickness
up to 12 mm 2 times plate thickness
up to 24 mm 3 times plate thickness
over 24 mm up to 70 mm 10 times plate thickness
1) Edge bending operations may necessitate a larger bending radius
113272 For steels other than stated in [113271] or other materials if applicable the necessaryminimum bending radius shall in case of doubt be determined by tests
113273 In the case of steels with a minimum nominal upper yield point exceeding 355 Nmm2 and platethicknesses of 30 mm and over where cold-forming with 3 or more permanent elongation has beenperformed proof of adequate toughness after welding is required in the procedure test and by means of in-production tests
11328 Bend reinforcements
113281 Bent structural elements eg the chords of girders where the change of direction means thatforces are generated or shall be transmitted perpendicular to the bend shall be adequately supported at thebending location The conditions set out in [113271] shall be complied with
113282 Where welded joints at bending locations cannot be avoided three-plate welds generally as in[11426] may be used Such connections shall be depicted in detail on the drawings
114 Types of weldsThe chosen type of weld shall be suitable and sufficiently dimensioned or favourably designed to transfer thetype (static dynamic) and magnitude of forces
1141 Butt joints
11411 Depending on plate thickness welding procedure and -position butt welds shall take the form ofsquare single- or double-V welds (X welds) in conformity with the standards (eg EN 12345 EN 22553ISO2553 EN ISO 9692-1 -2 -3 or -4)
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DNV GL AS
11412 Where other forms of weld are envisaged these shall be depicted specially in the drawings Weldgeometries for special welding processes (eg submerged-arc single-side and electro-gas or electro-slagwelding) shall have been tested and approved as part of a procedure test
11413 Butt welds shall as a matter of principle be grooved out on the root side and given at least onecapping pass Exceptions to this rule eg in the case of submerged-arc welding or the aforementionedprocesses also require to be tested and approved as part of a procedure testThe theoretical throat shall be the thickness of the plate or where the plates are of differing thicknessthe lesser thickness Where proof of fatigue strength is required the detail category depends on theconfiguration (quality) of the weld
11414 If the above conditions cannot be fulfilled eg where welds are accessible from one side only opensquare-edge joints with back-up bars or permanent machined or integrally cast backing as in Figure 11-6shall be usedThe calculated weld thickness may be taken as 90 of the (lesser) plate thickness t maximum (t-1) mmWhere proof of fatigue strength is required these welds shall be placed in the corresponding detail category
Figure 11-6 Single-side welds with permanent weld pool supports (backings)
1142 Corner- T- and double-T- (cross) welds
11421 Full-penetration corner- T- and double-T- (cross) welds for the full connection to the abuttingplates shall take the form of single- or double-bevel joints with the minimum possible shoulder and anadequate gap as shown in Figure 11-7 The root shall be grooved out and welded from the reverse side
Figure 11-7 Single- and double-bevel welds with full root penetration
The theoretical weld thickness shall be the thickness of the abutting plate Where proof of fatigue strength isrequired the detail category depends on the configuration (quality) of the weld
11422 Corner- T- and double-T- (cross) welds with a defined root defect f as shown in Figure 11-8 shalltake the form of single- or double-bevel welds as described in [11421] with reverse-side welding butwithout grooving-out of the root
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DNV GL AS
Figure 11-8 Single- and double-bevel welds with defined incomplete root penetration
The theoretical weld thickness may be taken as the thickness t of the abutting plate minus f being equal to02 t up to a maximum of 3 mm Where proof of fatigue strength is required these welds shall be placed inthe corresponding detail category
11423 Corner- T- and double-T- (cross) welds with an unwelded root face c and a defined incomplete rootpenetration f to be taken into consideration shall take the general form shown in Figure 11-9
Figure 11-9 Single- and double bevel welds with an unwelded root face and a defined incompleteroot penetration
The theoretical weld thickness shall be the thickness t of the abutting plate minus (c + f) f being equal to02 t up to a maximum of 3 mm Where proof of fatigue strength is required these welds shall be placed inthe corresponding detail category
11424 Corner- T- and double-T- (cross) welds accessible from one side only may as shown in Figure11-10 be made either as butt joints with a weld pool support analogous to those described in [11414] oras one-sided single-bevel welds analogous to those in [11422]
Figure 11-10 Single-side welded T-joints
The theoretical weld thickness shall similarly be determined in accordance with [11414] or [11422]Where proof of fatigue strength is required use of these welds shall be avoided if possible
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DNV GL AS
11425 In the case of flush corner joints ie where neither of the plates projects joint configurations asshown in Figure 11-11 shall be used with bevelling of the plates shown as upright to avoid the danger oflamellar rupture (stepwise cracking)
Figure 11-11 Flush fitted corner joints
11426 Where in T-joints the main stress acts in the plane of the plates shown in the horizontal position inFigure 11-12 (eg in plating) and the connection of the vertical (edge-on) plates is of secondary importancethen (except in the case of mainly dynamic stresses) three-plate welds as shown in Figure 11-12 may beusedThe theoretical weld thickness of the joint connecting the horizontal plates shall be determined in accordancewith [11413] The required a dimension is determined by the joint connecting the vertical (edge-on)plate and shall where necessary be ascertained by calculation as for fillet welds
Figure 11-12 Three-plate welds
1143 Fillet welds
11431 Fillet welds shall as a matter of principle be made on both sides Exceptions to this rule (eg inthe case of closed box girders and in the case of primary shear stress parallel to the weld) require approvalin every instance The thickness a (the height of the inscribed equilateral triangle) shall be determined bycalculationThe leg length z of a fillet weld see Figure 11-13 shall not be less than 14 times the fillet weld thicknessa
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DNV GL AS
11432 The thickness of fillet welds shall not exceed 07 times the lesser thickness of the parts to bewelded (generally the web thickness) The minimum thickness is defined by
amin = [mm] (but not less than 3 mm)
t1 = the lesser plate thickness [mm] (eg the web thickness)t2 = the greater plate thickness [mm] (eg the chord thickness)
11433 The aim with fillet welds shall be to have a flat symmetrical cross-section with good transitionto the base metal Where proof of fatigue strength is required it may be necessary to carry out machining(grinding-out the notch) depending on the detail category The weld shall extend at least to the immediateproximity of the theoretical root point
11434 Where mechanical welding processes are used which produce a deeper penetration going wellbeyond the theoretical root point and capable of being reliably and uniformly maintained under productionconditions it is permissible to take account of the deeper penetration when determining the fillet weld throatThe mathematical dimension
shall be determined by reference to the configuration shown in Figure 11-13 and shall take into accountthe value of min e which shall be established for each welding procedure by a procedure test The weldthickness shall in relation to the theoretical root point not be less than the minimum thickness for filletwelds specified in [11432]
Figure 11-13 Fillet welds with increased penetration
11435 Depending on the welding technique used an increase of the a dimension of up to 1 mm maybe stipulated when laying down welds over production coatings particularly liable to cause porosity Thisparticularly applies when using fillet welds of minimum thickness sizeThe extent of the increase shall be determined on a case to case basis according to the nature andmagnitude of the stress based on the results of the production-coating tests according to RU SHIP Pt2 Thesame applies in turn to welding processes too in which there is a likelihood of insufficient root penetration
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DNV GL AS
115 Workmanship and testing of weld jointsWelding workmanship shall comply with RU SHIP Pt2
1151 Weld preparation and assembly
11511 When preparing and assembling structural parts care shall be taken to ensure compliance with theprescribed joint geometry and root face (air) gaps Where the permissible root face gap is slightly exceededit may be reduced by build-up welding at the weld edges Inserts or wires are not allowed to be welded intothe gap
11512 Plates and profiles shall be aligned accurately especially where joints are interrupted by transverseparts The magnitude of the permissible misalignment of plate edges depends on the particular structuralpart the plate thickness and the stress see RU SHIP Pt2
11513 In the welding zone structural parts shall be clean and dry Scale rust slag grease paint (exceptfor production coatings) and dirt shall be removed carefully prior to welding
11514 If plates profiles or structural parts are given a corrosion-inhibiting coating (shop primer) beforewelding this shall not impair the quality of the welds
11515 Only those weldable production coatings shall be applied for which the Societys report of noobjection exists based on a pore formation tendency test
1152 Protection against the weather preheating
11521 The working area of the welder shall be protected in particular for outside work against winddampness and cold In the case of submerged-arc welding special care shall be taken to protect againstdraughts When working outdoors it is recommended in any case to dry heat the weld edges in unfavourableweather conditions
11522 In low temperatures (component temperatures below 5degC) suitable measures shall be taken (egcovering large-area heating preheating in particular when welding at relatively low heat input eg with thinfillet welds or with thick-walled components) to ensure that the welding work can proceed satisfactorily Ifthe temperature drops below -10degC no further welding should be performed if possible
1153 Welding positions and sequence
11531 Welding work shall be performed in the most favourable welding position Welding in restrictedpositions eg positions PE or PD (overhead) shall be restricted to unavoidable cases
11532 Vertical downward welding of fillet welds shall not be applied to lifting appliance componentsand lifting appliances including supporting structure (eg crane columns) even after a successful weldingprocedure test
11533 Obstruction of weld shrinkage shall be minimized by the choice of a suitable construction andwelding sequence
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DNV GL AS
1154 Workmanship
11541 The welds shall have sufficient penetration and clean regular weld surfaces with soft transitionsto the base material Excessive overthickness and grooves as well as notches at the edges of plates or cut-outs shall be avoided
11542 Cracked tacks may not be welded over but shall be removed by machining In multi-pass weldingthe slag from preceding passes shall be removed completely Pores visible slag inclusions and cracks maynot be welded over but shall be removed by machining and repaired
1155 Repair of defectsRepair of major defects of workmanship may only be undertaken after agreement with the Society Thisapplies similarly to the repair by welding of worn broken or otherwise damaged parts Prior to repair work onload-bearing structural parts (1st order) a sketch of the repair shall be submitted
1156 PreheatingRegarding the requirement for and amount of preheating several decisive criteria exist eg chemicalcomposition plate thickness two- or three- dimensional heat dissipation environmental or componenttemperature heat input due to welding (energy per unit length) see RU SHIP Pt2
1157 Heat treatment
11571 The nature and scope of any heat treatment which may have to be applied to welded structuralparts depends on their residual stress state (weld geometry and thickness rigidity of part) and thecharacteristics of the material concerned ie its behaviour or any change in characteristics to be expectedwhen subjected to heat treatment Generally it is a matter of stress-relieving or annealing treatment Thesteelmakers directions and recommendations shall be followed
11572 Depending on the type of material concerned flash butt welds shall be subjected to normalising orquenching and tempering treatment
11573 The way in which the mechanical properties of the weld are affected by subsequent heat treatmentis one of the factors to be investigated in the weld-procedure test In addition to this the Society may call forproduction tests
11574 Any non-destructive tests required shall be carried out after heat treatment
1158 Non-destructive tests
11581 The nature and scope of non-destructive tests depends on the importance and loading of the partconcerned (its component class) and on the possible weld defects or effects on the base metal which mayarise from the welding technique position etc
11582 By way of example in Table 11-2 the tests required for the important parts of shipboard liftingappliances and loose gear have been compiled Additionally as a guide requirements imposed on weldedconnections in the form of assessment categories according to EN ISO 5817 have been addedWhere proof of fatigue strength is required the test requirements given in the detail category table usedapply The manufacturing documents (drawings welding diagram test schedule) shall contain for eachstructural component comprehensive information concerning the nature and scope of the tests required
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DNV GL AS
11583 Non-destructive tests shall be carried out by suitably qualified personnel
11584 The tests shall be carried out in accordance with accepted practice The results shall be presentedto the Societys surveyor at the latest at the acceptance testing of the components
Table 11-2 Test specifications for welded connections
Test specifications for welded connections
Components 1 1st Order 2nd Order
Notes See Table 13-1 See Table 13-1
Butt welds perpendicular to direction of main stressincluding weld intersectionsRadiographic andor ultra-sonic inspection of 10 of weld lengthin special cases of 100 of weld length Wherenecessary magnetic particle testing
Butt welds perpendicular to direction ofmain stress including weld intersectionsRadiographic andor ultra-sonic inspectionrandomly Where necessary magneticparticle testing
Butt welds parallel to direction of mainstressRadiographic andor ultra-sonic inspectionrandomly In special cases as above Wherenecessary magnetic particle testing
Nature and scope oftests to be applied
Single (HV) or double bevel (DHV-(K)) seams- especially in thicker plates - perpendicularand parallel to the direction of the mainstressUltrasonic and magnetic particle testing ofat least 10 in the case of thicker plates and rigidstructural components as a rule of 100 of theweld length
Other welded connections and componentsas above in cases of doubtRecommended
Magnetic particle testing of single (HV) ordouble bevel (DHV-(K) seams on thick-walled components
Requirements Assessment category B as per ISO 5817 Assessment category C as per ISO 5817
Remarks
mdash With the Societys consent dye penetrant testing may be used instead of magnetic particle testingmdash Deviations from the recommended assessment categories - even in respect of individual criteria - may be agreedmdash As regards ultrasonic tests the assessment criterion will be specified by the Society as part of the process of
approving and authorising testing locations and inspectorsmdash The Societys surveyor retains the right to determine or alter the position of random tests and to increase the scope
of tests particularly if there is an accumulation of defects1) For 3rd order components (see Table 13-1) no tests are prescribed
1159 Production tests
11591 If the manufacturing process or any subsequent (heat) treatment which may be required leadsto the expectation of a substantial change in or indeed deterioration of the properties of the material or thewelded connection the Society may stipulate production tests to prove that the mechanical qualities remainadequate
11592 Production tests during the course of manufacture shall as a matter of principle be performedwhen welding is carried out on cold-formed portions made from materials with a minimum nominalupper yield point of more than 355 Nmm2 with a wall thickness of 30 mm or more and with degrees ofdeformation of 3 permanent elongation ε and over
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DNV GL AS
Elongation in the external tensile zone
r = internal bending radiust = plate thickness
116 Examination of drawings and supervision of construction
1161 Examination of drawingsFor the examination of drawings of steel components the requirements given in Sec13 shall be observed Inaddition to the welding diagrams and test plans stated there the following applies
11611 Details on welded joints in the documents to be examined
116111 In the documents to be examined and to be submitted for approval production details shall beincluded which are relevant to the quality of the welded joint and the examination by the Society Besides thematerials and the weld geometry this requires the following information
mdash weld preparation procedure (mechanical thermal etc)mdash welding method welding positionsmdash welding consumables and auxiliary materialmdash preheating and heat conduction during welding where requiredmdash weld composition and number of layersmdash welding sequence (in special cases)mdash root side grooving (method)mdash possibly finishing (heat) treatmentmdash number and location of production specimens to be welded simultaneously if required
116112 As long as weld preparation and workmanship of the welds (in combination with approved weldingmethods welding consumables and auxiliary materials) comply with the accepted practice of weldingtechnology this standard and other recognized standards the Society may waive a special description ordetails in the test documentation
11612 Description of welded joints
116121 The description of welded joints including the gap and weld geometry shall eg comply with thestandards EN 12345 EN 22553ISO 2553 EN ISO 9692-1 -2 -3 or -4 The designations in the documentsto be examined (drawings etc) shall be well-defined eg by standard symbols
116122 Deviating weld geometries or symbols in the documents to be examined (drawings weldingdiagrams or specifications) shall be presented or commented on in detail and require approval by the Society(eg in connection with the examination of drawings or with a procedure test)
1162 Supervision of constructionRegarding supervision of construction by the Society the requirements given in [133] and the followingrequirements apply
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DNV GL AS
11621 Surveillance of production
116211 Steel components shall be surveyed during production with respect to workmanship andcompliance with the approved drawings The start of production shall be indicated in good time to the Societyinspection in charge in order to enable the Societys surveyor to supervise the complete production process
116212 Professional proper and complete execution of the joining processes shall be ensured by means ofthorough controls by the factory
116213 If the manufacturing process or any subsequent (heat) treatment which may be required maylead to a substantial change in or deterioration of the properties of the material or the welded connectionthe Society may stipulate in-production tests to prove that the mechanical qualities remain adequate
1163 Acceptance test
11631 Before delivery of steel components a suitable date for the acceptance test shall be agreed withthe Society inspection in charge
11632 For the acceptance test before delivery the manufacturer shall have ready the followingdocuments
mdash purchase and order documentsmdash workshop drawingsmdash drawings approved by the Society including examination reportsmdash results of internal checksmdash material test certificatesmdash certificates or protocols of welding testsmdash further documents as required
117 Documentation
1171 Marking
11711 Where the Society acceptance test before delivery has not given reason for complaint the steelcomponent shall be stamped as follows
mdash stamp 3 with the month and year of testingmdash the Societys certificate number as per [11721] together with the code letter(s) of the examining
inspection office
11712 Where the steel components are produced in the lifting appliance manufacturers works a specialstamp and certification of these parts after manufacturing will be dispensed with This will be included in theacceptance test before delivery of the assembled lifting appliance
1172 Certification
11721 The Societys surveyor will issue a certificate Form 2092a for each finished and tested steelcomponent This certificate includes the following information
mdash manufacturers namemdash date and reference number of the approved drawingmdash replica of stamp
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DNV GL AS
11722 The certificate issued according to [11721] is not part of the lifting appliance documentation onboard
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DNV GL AS
SECTION 12 TECHNICAL AND OPERATIONAL SAFETYREQUIREMENTS
121 General
1211 This section contains selected provisions in addition to the previous sections as regards safety of shipboardlifting appliances and the protection of persons based on the following requirements for design fitting andoperation of these devicesFurther requirements or measures shall be taken from the relevant standards and regulations if applicable
1212 A general precondition for the safe operation of shipboard lifting appliances is first of all its dimensioning andits design and equipment in accordance with Sec6 to Sec13 of this standardComplementary details regarding rope drives mechanical parts and electrical equipment are given in Sec8to Sec10
1213 For loose gear the requirements given in this section apply similarly where relevant
122 Design requirements
1221 Shipboard lifting appliances in general12211 Highest boom position
122111 General notesEach boom shall be capable of being lowered in the highest position with or without useful loadCombinations of different influences shall be taken into account
122112 Rope-operated booms1221121 With rope-operated booms the boom weight and the influence of all systems which prevent itremaining in the highest position shall be sufficient to overcome all losses due to friction and turning1221122 To prevent remaining in the highest boom position a restoring device may be provided whichshall be controlled from the crane drivers cabinAlternatively a warning device for the crane driver may be installed which warns of further luffing in duetime This device is only permissible if it is reasonable from a technical and operational point of view
122113 Cylinder-operated boomsWith cylinder-operated booms the cylinder force shall be great enough to comply with the requirementsgiven in [1221121]
12212 Secondary componentsSecondary components and auxiliary structures such as inter alia ladders consoles cable trays shall not ifpossible be welded to highly stressed components Where appropriate a proof of fatigue strength shall befurnished
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DNV GL AS
12213 Access to crane driversacute cabins
122131 Crane drivers cabins shall be designed and arranged in such a way and be of such a size thatthey are easily accessible no matter what the position of the crane An accident-proof standing position for asecond person shall be provided within the area of the crane driverrsquos cabin
122132 If there is a danger that the regular access to the driverrsquos cab can be obstructed (eg in case ofan accident fire etc) an independent emergency exit shall be provided
122133 If normal access is impossible when the cabin is occupied a second entrance of sufficient sizewhich may also be the emergency exit shall be provided
122134 Where the floor of the crane cabin is not more than 5 m above the deck it is sufficient if the cabincan be reached without particular danger when the crane is in one position but can be left via an emergencyexit no matter what the position of the crane
12214 Accesses in general
122141 Unobstructed access to all essential components of the lifting appliance shall be ensured formaintenance and repair purposes by means of suitable accesses platforms ladders and standing spaces
122142 The headroom of entrances shall be at least 2 m the clear width at least 06 m The clear heightof the opening may be reduced by a sill up to 06 m high
122143 Ladder rungs and climbing irons shall be of 2020 square steel bar set edgewise with a footstepwidth of at least approx 30 cm From a climbing height of 25 m and above a safety cage or track for safetyharness shall be provided
122144 Ladders1221441 The inclination of ladders measured from the horizontal shall be at least 65deg1221442 Ladder rungs and climbing irons shall be of 2020 (L = 300) or 2222 (300 gt L le 350) squaresteel bar set edgewise with a footstep width of at least 30 cm The horizontal distance from fixed structuresshall be at least 15 cm1221443 The distance of the lowest ladder rung from the deck or platform shall be between 100 mm and400 mm1221444 Climbing irons shall have a uniform distance of 300 mm from each other1221445 The minimum distances and spaces to be kept clear for movement within the reach of a ladder(see also Figure 12-1 and Figure 12-2) are
mdash 750 times 750 mm in front of the climbing irons excluding obstacles extending into this space(in exceptional cases a limit down to 550 times 550 is permissible however in this case obstacles such asbrackets shall be covered in order to prevent injuries)
mdash 150 mm behind the ladder measured from the axis of the climbing ironmdash 75 mm as an access clearance for the hands on each side of the ladder and around vertical hand grips
1221446 A fall arresting device (safety cage or guide rail for a safety harness) shall be provided if
a) the mounting height exceeds 25 m orb) a falling height of more than 30 m is possible
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DNV GL AS
Figure 12-1 Minimum clearances and movement space
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 223Standard for shipboard lifting appliances
DNV GL AS
Figure 12-2 Safety cage
1221447 For ladders with a height of more than 3 m or of any length (if a falling height of more than 3m is possible) the following requirements also apply
mdash The lowest safety cage retainer shall not be positioned lower than 22 m above the deck or platformmdash The retainers shall have uniform spacing of not more than 900 mmmdash The safety cage shall at a minimum consist of 5 longitudinal strutsmdash The clearance between climbing iron and rear cage shall be between 550 mm and 750 mm
1221448 The maximum vertical length of a ladder between two platforms is 6 m
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DNV GL AS
1221449 The ladder shall stop at intermediate platforms The ladder which arrives ends at the platformand the follow-on ladder is offset (not above the opening in the platform)12214410 The rails of the ladder shall extend past the upper platform by at least 1 m or hand grips shallbe fixed up to this height
122145 Landingsplatforms1221451 Outer edges of platforms or floors shall be provided with a coaming unless people andoritems slipping is prevented by other means1221452 Floors and their coverings respectively shall be skid-proof1221453 Platform openings require a cover if a ladder located above the platform may be adjusted onthe opening (eg if the upper ladder is fastened to rotating crane parts)The cover shall be capable of being held in the open position
122146 Guard rails1221461 The height of guard rails of accesses platforms etc shall be at least 090 m and be providedwith an upper handrail and a rail at mid-height A foot-bar with a minimum height of 010 m shall beprovided1221462 Where guard-rails are used to separate working areas from traffic areas their clearance frommoveable parts shall be at least 010 m
1222 Mobile shipboard lifting appliances12221 General requirements
122211 Rail-mounted cranes and trolleys shall be protected from derailment overturning and dislodgingand against unintentional movement in a seaway and in operation Rail stops as well as warning devices andrail clearers for lifting appliances on deck shall be provided
122212 Cranes and trolleys which can be moved athwartships shall be fitted with a form-locking drive(rack and pinion drive or equivalent) The drive shall be self-locking or fitted with brakes
122213 For cranes and trolleys in engine and pump rooms up to a nominal load of 10 t which can bemoved athwartships the requirement given in [122212] is considered to be complied with if the load canbe safely held also in a seaway by suitable fastening devices (tackles pulleys and the like)
122214 Cranes and trolleys which can be moved fore and aft shall be fitted with a self-locking driveor with brakes For such cranes calculations shall be submitted proving that the cranes are able to moveagainst a 2deg inclination and against a wind load 50 higher than specified in [5331] for operation at seaand with or without load by friction contact
122215 Cranes and trolleys with a nominal load over 10 t which can be moved fore and aft shall befitted with a direct drive as given in [122212] if they shall be employed for working at sea state Thispredominantly includes cranes and trolleys above the main engine
122216 Each crane rail shall be arranged parallel to the design waterline of the ship
122217 Where the operator has to move with the crane or trolley control unit the speed of travel may notexceed 05 ms
12222 Industrial cargo-handling vehiclesFor industrial cargo-handling vehicles the requirements given in [65] apply
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DNV GL AS
123 Equipment
1231 Highest boom position
12311 Shipboard lifting appliances whose booms are held by luffing ropes shall be equipped with buffersfor the uppermost position
12312 The requirements given in [12472] shall be observed when designing buffers
1232 Control stands and controls
12321 Control stands and controls shall be designed and located in such a way that the crane driver hasan unobstructed view of the area of operation or at least of the person guiding him
12322 The control stands of cranes for cargo handling shall be closed driver cabins constructed of fire-resistant material with adequate lighting heating and ventilation They shall be fitted with accident-proofwindow panes sun shields window wipers protective grids and with one suitable fire extinguisher
12323 The controls shall be marked to indicate their function Movement of the controls shall beappropriately related to the corresponding crane movements eg
mdash When a vertical lever is pulled towards the operator a horizontal lever is raised or a swivel lever or hand-wheel turned clockwise the load shall rise or the crane move backwards
mdash When a vertical lever is pushed away from the operator a horizontal lever is pushed down or a swivellever or hand-wheel turned anticlockwise the load shall descend or the crane move forwards
mdash As regards the slewing or rotation of cranes the direction of slewing or rotation of the crane shall agreewith the direction or layout of the controls
12324 Additional requirements for the controls and the control mechanism are given in [10621]
1233 Cranes with load radius-dependent nominal loads shall have a load radius diagram in the drivers cabinThe actual load radius shall be continually visible to the driver
1234 Working hours counterCranes belonging to crane group Band C (see [57]) shall be provided with working hours countingmechanisms
1235 LightingFor the main and emergency power lighting of shipboard lifting appliances the requirements given in[10622] apply
1236 Fresh air supplyFor closed control stands sufficient supply of fresh air shall be provided Air inlets shall be arranged in theopen-air and such that no contamination with exhaust gas dust or fueloil mist may occur
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DNV GL AS
1237 Protection and precautions against fire and explosionNecessary protection and precautions against fires and explosions shall be considered The number capacityand location of fire extinguishers shall be adequate for the type of crane and its intended service
124 Safety devices
1241 Overload protection12411 Load limit
124111 Lifting appliances shall have overload protection devices These shall be activated if the responseof the load being raised or lowered exceeds a pre-determined amount which shall not be greater than theeffect of a static load equal to the SWL times the hoist load coefficient for which the lifting appliance hasbeen designed
124112 Where lifting appliances have variable nominal loads the overload protection device shall adjustautomatically to the actual load radius
124113 For rope and chain hoists manufactured by series production the manufacturers settings andtolerances apply see [62311]
12412 Load moment limitation
124121 Where lifting appliances have variable nominal loads a load moment limitation device is alsorequired in addition to the overload protection device
124122 Devices for limitation of the load moments shall act directly on the luffing andor telescope drivesOn hydraulic systems suitable pressure limitation devices are permissible
12413 Load reduction after an overloadAfter the overload protection devices are activated the load or load moment reducing motions of the liftingappliance and its mobile components shall still be possible
1242 Motion limiter12421 General requirements
124211 The end positions of all motions which can be performed by lifting appliances or their mobilecomponents shall be limited in an appropriate and safe way For rotary motions this is only applicable if theyare restricted by local circumstances
124212 For conventional derrick boom systems exceptions from the requirements given in [124211]can be permitted
124213 It shall not be possible for end positions to be overridden Exceptions eg for maintenance andboom stowage require written approval by the Society
124214 If required motion limiters shall also have an influence on other motions in order to avoiddamage This may eg be required for the highest hook position of booms with luffing ropes see also[12472]
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DNV GL AS
12422 Motion limitation by limit switches
124221 Limit switches shall be designed and positioned in such a way that their efficiency is not affectedby the weather or by dirt accumulation Movement in the opposite direction shall be possible after they areactivated Proximity switches shall preferably be used
124222 Limit switches shall be located and adjusted in such a way that no damage can occur even if theyare approached at maximum speed and with full nominal load If necessary pre-limit switches shall be used
124223 Regarding additional requirements for limit switches see [1052]
12423 Motion limitation by design measures
124231 Limit switches1242311 For hydraulically operated lifting appliances with low operating speeds and nominal loads up to1000 kg limit stops with damping if required may be permitted as a motion limitation1242312 For rope and chain hoists from series-production the requirements given in [62322] apply
12424 Runway limitFor limit stops of movable cranes the provisions in [5342] are applicable
1243 Emergency switcheskeys
12431 On control stands inside cabins or at manual controls an emergency switch or emergency cut-outwith mechanical locking device shall be provided
12432 The emergency shut-down shall cut off the power supply and all motions In the case of hydraulicdrives the emergency shut-down shall also act on the drive of the hydraulic pumpReturn to service shall be solely from the zero position of the respective controls or operating instruments
12433 Emergency switcheskeys shall meet the requirements given in EN 418 and continue to function inthe event of any failure of the control system
1244 Slack rope limiter
12441 In particular cases a slack rope limiter may be required eg with fast hoisting speeds withoutautomatic creep hoist multiple coils or if required for a special mode of operation
12442 For shipboard lifting appliances and floating cranes operating at sea slack rope limiters in the liftingand luffing system as well as a slack rope indication for the crane driver are requiredThe slack rope limitation system of shipboard cargo cranes operating at sea shall stop the winch(es)automatically
1245 Secondary brake for lifting appliancesLifting appliances used for the conveyance of persons or personnel shall be equipped with a secondary brakeat the hoist and luffing winch The requirements given in [425] and [9537] apply
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DNV GL AS
1246 Alarm devices
12461 Outside the driverrsquos cabin on cranes used for the handling of cargo a signal horn shall be providedby which the crane driver can raise an acoustic signal which can definitely be heard in the working area ofthe crane
12462 Mobile deck cranes shall give an optical and acoustic alarm while moving
1247 Strain of shipboard lifting appliances due to safety devices
12471 The movements and dynamic loads occurring following the response of safety devices shall be keptto a minimum if possible
12472 Motion limiters for the highest boom position shall be designed in such a way that after depositingthe load no damage may occur from the unloaded luffing ropes
125 Passive protective measures
1251 Safety distances
12511 In accessible areas the distance between fixed parts of the ship and moving parts of the liftingappliance shall be at least 050 m in all directions and where passageways adjoin at least 060 mIf at certain points a distance of 050 m cannot be provided the area concerned shall be identified withprominent black and yellow paintwork Warning notices shall be fitted
12512 A distance of at least 050 m shall be provided between the lower edge of the boom in its lowestworking position and fixed parts of the ship
1252 Safety of access and transport
12521 Working passages operating platforms stairs and other areas accessible during operation shall besecured by railings
12522 All lifting appliances shall be fitted with a signboard forbidding access or ascent by unauthorizedpersons
12523 In utility spaces (on board ships and in cranes) adequately-dimensioned securing facilities for pull-lift hoists or holding devices shall be fitted at suitable points
12524 To permit load tests on shipboard lifting appliances inside utility spaces eye plates shall beprovided at suitable points see [6235]
1253 Corrosion protection
12531 For general requirements regarding corrosion protection the provisions of [11235] apply for steelcomponents and [8212] for wire ropes
12532 Components which are employed for hoisting services under water eg loose gear shall bedesigned in such a way that as far as possible no seawater can ingress
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DNV GL AS
126 Stowage and lashing devices
1261 General requirements
12611 It shall be possible for all wheeled shipboard lifting appliances and mobile components of shipboardlifting appliances to be positioned or where required supported for sea use as well as to be fastenedsecurely by suitable devices or guys see [4253]
12612 Supporting or fastening devices shall be designed in such a way that inadmissible forces or loadsmay not be transmitted to the lifting appliance or the components thereof caused by deformations of theshiprsquos hull in a seaway
1262 Wheeled lifting appliances
12621 Wheeled lifting appliances shall be located in stowage positions which as far as possible areexpected to suffer the least loads in a seaway
12622 For free-travelling loading gear such as eg industrial cargo-handling vehicles suitable stowagespaces and lashing eyes or other suitable devices shall be provided
1263 Revolving cranes
12631 Revolving cranes with booms or projecting machinery rooms require supporting structures for thesecomponents and a special blocking device to relieve the slewing gear
12632 Where booms or projecting machinery rooms with an out of operation status shall not be stowedor supported written approval by the Society is required
12633 Booms with luffing ropes shall be guyed downwards either hanging free or supported Where thebrakes of the lifting appliance are designed for it this requirement can be complied with by proper fasteningof the cargo hook and prestressing of the hoisting ropes Prestressing shall be specified by the manufacturerSupported booms may also be fastened properly to the boom support see [5722]For booms with luffing cylinders the guy or fastening may be dispensed with provided that a correspondingapproval is at hand
12634 Where not serving to guy the boom cargo hooks shall be stowed in special devices at the boom oron deck Grabs or other large andor heavy loose gear shall be stowed on deck
1264 Design and dimensioning
12641 Boom supports supporting stowage and lashing devices shall be designed and dimensioned withthe same diligence and to the same criteria which apply to lifting appliances
12642 Stowage and lashing devices shall be dimensioned like lifting appliances out of operation accordingto [56]
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DNV GL AS
127 Operational requirements
1271 Shipboard lifting appliances in general12711 Marking of hoisting capacity
127111 All lifting appliances shall be marked permanently and prominently with the nominal load SWLand the corresponding load radiusIn the case of load-radius dependent nominal loads lifting appliances shall be marked in several placesDetailed information regarding marking of shipboard lifting appliances is given in [1325]
127112 All loose gear shall be marked permanently and prominently with the nominal load SWL and thedead load WT the latter if WT ge 100 kgDetailed information regarding marking of loose gear is given in [743]
12712 Ship stability
127121 In the absence of any special measures the shiprsquos stability alone shall suffice to ensuresimultaneous operation of all shipboard lifting appliances for transhipment handling or transport of cargounder all operational conditions of the shipIn doing so the inclinations andor motions of the ship which are the basis for dimensioning the liftingappliance shall not be exceeded
127122 Special measures as per [127121] can be eg
mdash operational restrictionsmdash ballasting by water or weightsmdash supporting the ship ashoremdash utilization of stabilizing pontoons
Special measures always require instructions recorded in writing and supervisory personnel and whererequired also additional supervising devices These requirements also apply to fully automated operation
127123 The influence of loading gear on the shiprsquos stability shall be verified by calculation Thesecalculations shall be included in the stability documentation of the ship
12713 Failure of the drive power
127131 A design shall be employed auxiliary means shall be available and measures shall be taken to setdown suspended loads as safely as possible in the event of a failure of the drive powerMobile lifting appliances andor mobile lifting appliance components may for this purpose possibly betransferred into a more favourable load position
127132 If no other lifting appliances are available the follow-ing auxiliary meansmeasures may eg beemployed
mdash plug-on auxiliary drivesmanual pumpsmdash eye plates attached to the loading gear for use by pull-lift hoists for small loadsmdash mechanical ventilation of brakes or opening of valves
Mechanical ventilation of brakes or opening of valves is only permissible if the design conditions regardingintake of the released energy allow for it Required waiting periods for cooling-down shall be observed
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DNV GL AS
127133 Shipboard lifting appliances used for the conveyance of persons shall be equipped with suitablerescue equipment Descender devices may be employed for the descent from work-baskets
12714 Conveyance of personsShipboard lifting appliances used for the conveyance of persons shall comply with the requirements given in[425] with regard to dimensioning control and operationPersons may only be transported at daylight and under environmental conditions (windseaway) which arecon-sidered to be acceptable by the supervisor in charge
12715 Communication
127151 Crane drivers shall have an unobstructed view of the load and the working area under all workingconditions or else personnel guiding them see also [12321]
127152 If necessary equipment shall be provided or measures taken which allow safe transmittance ofinstructions from the guiding person(s) to the crane driver or the person handling the crane
1272 Wheeled lifting appliancesFor wheeled lifting appliances the operational requirements given in [1222] [12462] and [1251] apply
1273 Floating cranes
12731 Where pontoons carrying floating cranes under load are operated in calm water a safety distance ofat least 050 m shall be maintained between the deck edge at the lowest corner and the surface of the waterWhen working in unprotected waters a safety distance of at least 100 m shall be maintained
12732 The transport of loads suspended from the crane hook across unprotected waters is subject in eachcase to approval by the Society who may for this purpose issue a Conveyance Certificate if necessary
12733 In the event of the floating structure being grounded the cranes located on it may only beoperated if the structure is designed for that situation
1274 Responsibility of the ships management
12741 Special working conditions operational restrictions release and safety measures shall be recordedin writing and included with the corresponding lifting appliance documentation
12742 Maintenance and control measures performed by the ships management andor external personnelshall be confirmed properly in the lifting appliance documentation or added to itIn the Societys register book for lifting appliances Form CG1 Part 4 is provided for entries of this kind see[137]
12743 If the limit values for wind ship inclination ship motion or temperature specified in [424] arereached lifting appliances shall be put out of operation and where required be stowed in a special way andor be lashed for sea see [126]Deviating limit values may be specified for shipboard lifting appliances operating in a seaway or at lowtemperatures
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DNV GL AS
SECTION 13 TESTING AND EXAMINATION OF SHIPBOARD LIFTINGAPPLIANCES
131 General
1311 Description of content
13111 Subsections [132] to [135] contain requirements for testing examination marking andcertification of shipboard lifting appliances used for cargo handlingThese provisions apply analogously to shipboard lifting appliances not handling cargo which are onlyexpressly mentioned if required
13112 The requirements given in [136] apply for the evaluation and treatment of worn-out or damagedlifting appliance components
13113 The lifting appliance documentation described in [137] includes the following items
mdash types and systems of certificationmdash compilation of test certificates in register books (certification of lifting appliances)mdash confirmation of investigations inspections by the ships management replacement of components as well
as repair and maintenance activitiesmdash rigging plansmdash operating and maintenance instructions
1312 Supplementary requirementsSupplementarydeviating requirements apply to the following lifting appliances equipment and means oftransport
13121 Lifting appliances
mdash rope and chain hoists ([62])mdash ramps and car decks ([63])mdash lifting appliances for research work ([64])mdash industrial cargo-handling vehicles ([65])
13122 Equipment
mdash interchangeable components (Sec7)mdash wire and fibre ropes (Sec8)mdash mechanical parts (Sec9)mdash electrical equipment (Sec10)
13123 Means of transport
mdash loose gear (Sec7)mdash shipborne working baskets ([661])mdash landing booms ([653])
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DNV GL AS
1313 DefinitionsIn addition to [115] the following definitions apply
13131 Tests
131311 Function testThe designation function test is applied to testing of all possible movements or functions as well as tocontrol limiting and safety equipmentThis test shall generally be carried out with available weightsTo test and if applicable to adjust load monitoring equipment calibrated weights or if permitted calibratedforce measuring devices shall be made available
131312 Load testThe designation load test is given to the test with the prescribed test load LPdyn or LPstatThe purpose of the load test is to prove adequate strength safety against hidden defects and - if applicable -adequate safety against overturning
13132 Examination
131321 Thorough examinationA thorough examination means a detailed visual examination supplemented if necessary by other suitablemeans or measures in order to arrive at a reliable conclusion as to safetyIf deemed necessary by the Societys surveyor parts of the interchangeable components of the loose gear orof the lifting appliance shall be dismounted and where required dismantled
131322 InspectionThe term inspection means a visual inspection whereby - as far as is possible by this means - it shall bedetermined whether continued use can safely be permitted
132 Supervision of constructionIn addition to the following provisions the general requirements given in Sec1 and for steel constructionthe requirements given in [1162] shall be observed
1321 General
13211 Supervision of construction is required in principle The Society may however dispense with itfor lifting appliances manufactured in series which is not used for cargo handling and which fulfils therequirements for omitting examination of drawings see [132] In this case manufacturerrsquos test reportsmay be accepted deviating from the certificates stated in [13271]
13212 Commencement of construction of a lifting appliance shall be advised to the Society in sufficienttime for the Societys surveyor to attend the construction process from the very beginning
13213 The basis for the supervision of construction at the manufacturer of the lifting appliance is theapproved documentation according to Sec2 plus if applicable further documentation certificates reportsand information from the manufacturer which the Societys surveyor needs for assessment of the parts to beexamined
13214 Regarding supervision of construction and lifting appliance documentation subcontracting firmsshall provide certificates and test reports in the scope specified in Sec6 to Sec10
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DNV GL AS
1322 Participation by manufacturers
13221 As far as necessary and advisable the works shall check all components during and aftermanufacture for completeness dimensional accuracy and proper workmanship
13222 Following checking and if required repair by the works the components shall be presented to theSocietys surveyor for inspection during appropriate phases of construction normally in easily accessible andunpainted conditionCertificates for components and equipment delivered by subcontractors shall be submitted
13223 The Societys surveyor may reject components not adequately pre-checked and stipulate that theybe presented again following checking by the works and if required repair
13224 Components to be tested shall be indicated for the Societys inspection in good time forexamination
13225 In order to enable the Societys surveyor to perform his duties he shall be given access to theworkshops in which components for testing are manufactured and assembled Manufacturers shall makeavailable to the surveyor the personnel and material support required to carry out the prescribed tests
1323 Supervision of construction
13231 The Societys surveyor examines the components constructed at the manufacturers or suppliedwith regard to condition marking and certification He supervises the assembly of the lifting appliance andexamines workmanship and agreement with approved documents and witnesses the test runs and functionaltests as appropriate or agreed
13232 Testing of materials for the manufacture shall be proven to the Societys surveyor in accordancewith the Societys rules for materialsThe certificatesreports for the materials used as well as proofs on welding and non-destructive materialtests shall be submitted
13233 Components which are not type-tested but subject to tests and examination shall as far aspossible be tested at the manufacturers test plant in the presence of the Societys surveyor in an agreedscope or as prescribed by this standardRegarding series production instead of the prescribed tests other testing methods can be agreed with theSociety provided that they are accepted to be equivalent
13234 Where machines devices or electrical equipment are provided for the intended purpose for the firsttime the Society may demand a type-test
1324 Acceptance testing13241 General notes
132411 Shipboard lifting appliances assembled ready for operation or completely equipped assemblygroups shall be presented to the Societys surveyor before they leave the manufacturers works
132412 After completion of agreed test runs or tests lifting appliances or lifting appliance assemblygroups shall be subjected to a thorough examination The testing methods applied are at the discretion of theSocietys surveyor Following tests on the test plant lubricating and hydraulic oil filters shall be checked forimpurity
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DNV GL AS
13242 Tests and examinations to be carried out
132421 General test and examination
mdash checking of documentationmdash examination in respect of workmanship compliance with the approved documents and for completenessmdash checking of safety clearances and passive protection measuresmdash examination of accesses ladders rails and platformsmdash examination of the cabin or the control stand and the control equipmentmdash examination of the manufacturers plate on which at a minimum shall be permanently indicated
mdash manufacturers namemdash year of constructionmdash serial numbermdash where applicable type designationmdash nominal load(s) and load radius (radii)
mdash examination of marking see [1325]
mdash additional tests andor examinations as required
132422 Test run1324221 Newly designed lifting appliances shall be test-run in the presence of the Societys surveyoraccording to a programme approved by the Society If possible this shall take place at the manufacturersbut with the Societys consent it may also take place elsewhere or at the place of operation1324222 Shipboard lifting appliances subject to special operating conditions shall undergo test runsunder these conditions At least one of every different type of lifting appliance shall be tested in this wayThis for instance means that the test run shall be performed with the ship also at the stipulated inclination1324223 A test run may cover the following insofar as applicable
mdash checking the interaction of all movable parts and functionsmdash function test under available loadmdash brake test with dynamic test load according to Table 13-2 by releasing the operators control 3
mdash emergency brake test with dynamic test load according to Table 13-2 (see also [133324]) 3
mdash checking the emergency load release devicemdash endurance tests on all power units under nominal load with heating measurementmdash noise measurement (also in the cabin)mdash measurement of power consumption and contractually agreed speeds under nominal loadmdash additional measurements including electrical ones if necessarymdash checking and adjustment of all valves and control equipmentmdash pressure testsmdash testing and adjustment of all safety devices and limit stopsmdash testing of lighting ventilation intercom etcmdash testing of fire protection systemmdash further tests as required
1324224 Easing of testing requirements shall be agreed with the Society
132423 Proof of stability against overturningFor the proof of stability against overturning for wheeled lifting appliances the requirements given in[4522] and [6512] apply
3 Brake tests with test load shall be restricted to the required number Emergency tests shall as far aspossible be performed only once
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DNV GL AS
1325 Marking of the lifting appliance13251 Lifting appliance number
132511 The sequential numbering of shipboard lifting appliances shall agree with the details in thecertificates and rigging plans
132512 The following rule for numbering shall be applied
mdash first all lifting appliances for cargo handling starting from the fore and arranged in pairs progressing fromport to starboard starting on deck then below deck
mdash next all lifting appliances needed for operating the ship but none of the gear exclusively for launching life-saving equipment Here also starting on deck then below deck
132513 The number of the lifting appliance shall be preceded by Nr or also No
13252 Nominal load(s)
132521 The nominal load(s) of lifting appliances for cargo handling shall be indicated in metric tonnes ton other lifting appliances especially with lower nominal loads the indication may also be in kilograms kgThe nominal load(s) of lifting appliances shall be preceded by the letters SWL where applicable with thefollowing additions
mdash SWL (P) for pairs of lifting appliancesmdash SWL (G) for lifting appliances with grabsmdash SWL (M) for conveyance of persons
Table 13-1 Examples of markings
Item No onboard the ship Nominal load Load radius Lifting appliance type Meaning of the marking
Lifting appliance with boom
No 3 SWL 40 t 24 ndash 32 m In the indicated area of load radiusloads up to 40 t may be transported
No 2
SWL 250 t
SWL 120 t
SWL 60 t
35 ndash 12 m
35 ndash 255 m
35 ndash 34 m
Crane with 3 load steps Theload radius limits of the allocatednominal loads shall not be exceeded1)
No 4SWL (G) 264 t
SWL 30 t
28 ndash 28 m
28 ndash 28 m
revolving cranes
In the indicated area of loadradius loads up to 264 t can betransported during grab operationup to 30 t in general cargooperation 2)
Nos 2 + 3 SWL (P) 60 t 26 ndash 31 mIn the indicated area of load radiusloads up to 60 t may be transportedby 2 cranes slewing jointly
No 1 SWL 50 t minusgantry cranewith foldabletrolley girders
In the whole operating range of thegantry crane and the trolley loadsup to 50 t may be transported
No 2SWL 50 t
SWL 186 t
36 ndash 14 m
36 ndash 40 mrevolving crane Crane with variable load range 3)
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DNV GL AS
Item No onboard the ship Nominal load Load radius Lifting appliance type Meaning of the marking
SWL 5 t 44 ndash 42 m Marking for the auxiliary hoist
Loading gear without boom
No 10 SWL 16 t minus bridge cranelifting platform Nominal load of the lifting appliance
No 18 SWL 3 ndash 6 t minus rope hoist
Where the hoisting rope has a singlereeve loads up to 3 t may be liftedup to 6 t in the case of double reeve4)
1) In the crane drivers cabin a load radius diagram shall be visibly displayed2) The difference between SWL (G) and SWL results from the different hoist load coefficients see Table 5-2
The nominal load SWL (G) includes the dead load of the grab As an example a grab may be marked as follows
SWL 24 t underneath WT 24 t3) Information about the curve-type variation of the nominal loads can be taken from the load radius diagram
displayed in the crane driveracutes cabin see Figure 5-44) The types of reeve shall be marked properly on the lifting appliance In the case of more than double reeve an
operating instruction is required
13253 Load radius (radii)
132531 The load radius (radii) of lifting appliances is (are) to be indicated in metres ldquomldquo When variablethe minimum and the maximum value each
132532 Gantry and bridge cranes with trolleys are not given a load radius indication
13254 Details of execution
132541 The marking giving details of the nominal load shall be in writing at least 80 mm high and thatregarding lifting appliance number or boom inclination at least 50 mm high
132542 This marking shall be permanently applied eg by means of metal plates or by tracing thecontour with a centre-punch or by means of welding spotsGlued-on foils are permitted only for lifting appliances under deck
132543 The marking for the nominal load and if applicable the load radius shall be located clearly apartfrom the lifting appliance number
13255 Location
132551 The marking shall be applied at a clearly visible location with jib cranes at both sides with gantrycranes at the fore and aft side of the gantry relative to the longitudinal direction of the ship
132552 In the case of lifting appliances which can be combined in pairs additional marking shall beapplied at a suitable location for the combined loadOn slewing cranes with crane booms arranged on a common crane column this marking shall be applied atthe fore and aft parts of the column relative to the longitudinal direction of the ship
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DNV GL AS
13256 Examples of marking
132561 Marking is part of the safety measures for the operation of lifting appliances and therefore subjectto examination see [1341]Where variable equipment and reeve options exist operating instructions are required
132562 In Table 13-1 some typical marking examples are listed including explanationsSpecial marking requires agreement with the Society
1326 Stamping of lifting appliances
13261 Prior to the Societys issuance of the test certificate as per [13271] the lifting appliance shall bestamped as follows
mdash the certificate number with the distinguishing letters of the Societymdash the stamp with month and year of test
13262 An additional stamp covering the nominal load is not applied until after the load test has beencarried out
13263 Cranes shall be stamped at the bottom end of the left-hand jib spar next to the point where it joinsthe crane houseLifting appliance assembly groups and lifting appliances other than cranes shall be stamped in a prominentposition
1327 Certification of supervision of construction
13271 For all shipboard lifting appliances completed and tested a test certificate on Form 2092a is issuedby the Societys surveyorWhere lifting appliances assembly groups are manufactured by subcontractors each assembly group receivesits own test certificate of Form 2092aWhere interchangeable components and loose gear are already a part of the lifting appliance during thesupervision of construction test certificates and examination certificates of form CG3 shall be providedFor wire ropes which are already part of the lifting appliance at the supervision of construction testcertificates and examination certificates of form CG4shall be providedWhere winches are already a part of the lifting appliance during the supervision of construction testcertificates and examination certificates of form 2092a shall be providedWhere luffing and slewing cylinders are already a part of the lifting appliance during the supervision ofconstruction test certificates and examination certificates of form 2092a shall be providedThis paragraph does not apply to chain and rope hoists manufactured in series production
13272 Apart from explanatory notes concerning the acceptance procedures the test certificate as per[13271] may contain notes regarding other certificates (eg CG3 CG4 2092a) protocols etc such aseg the following details
mdash manufacturers namemdash type designation and production numbermdash nominal load(s) and if applicable load radius (radii)mdash date and the Societys reference number of the plan approvalmdash associated ship (yard no or DNV GL Ship ID No)mdash stamp
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DNV GL AS
133 Initial test and examination
1331 General notes
13311 Prior to commissioning an initial test and examination within the scope described in [1332] to[1332] at the place of operation is requiredThe sequence of steps for the test and examination is as deemed necessary by the Societys surveyor whoalso decides the scope of his examination
13312 During practical testing of lifting appliances dependent on an external power supply care shall betaken to ensure that the test is carried out using the type of power supply envisaged from the ships mainWhere ships are fitted for shoreside power supply shore and ship power shall be compatible
13313 The certificates and rigging plans stated in [133412] shall be presented as proof of supervisionof construction and as an integral part of the lifting appliance documentation
1332 Function test
13321 This test serves to provide proof of the good working order of all components installed systemsand safety devices The test procedure is at the Societys surveyors discretion
13322 In the case of permanently installed lifting appliances the function test amongst other thingsserves to verify whether parts of the ships structure or the ships equipment restrict the working range orimpede the working process
13323 The function test to be carried out for the Societys surveyor does not normally serve to checkwhether all possible operations wanted by the operator can be effected Proving this is the responsibility ofthe manufacturer or supplier
13324 With the exception of the test on the overload protection devices the function test may be carriedout with any given load see also [131311]
13325 A function test using a test load requires the manufacturerrsquos consent
1333 Load test13331 General requirements
133311 All shipboard lifting appliances shall undergo a load test with weights prior to being put intoservice The test shall be carried out at the place of operation in order that their respective foundations ordriveways be included in the test
133312 In the case of lifting appliances below deck which is difficult to access load tests may alternativelybe conducted using approved load measuring devices with a tolerance limit of le 25
133313 Lifting appliances shall be subjected to a dynamic load testThe size of the test load shall be taken from Table 13-2
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DNV GL AS
Table 13-2 Dynamic test loads for shipboard lifting appliances
Nominal loads (LNe) Test loads (LPdyn) 1
up to 20 t20 t to 50 t
over 50 t
SWL + 25SWL + 5 t
SWL + 101 If applicable to be multiplied with fd according to [7334]
13332 Load test performanceFor the dynamic load test to be performed for the Societys surveyor the test load shall be lifted slowly andif possible also slewed and luffed In detail the following applies
133321 For lifting appliances generally the test load shall be lowered rapidly and braked in variouspositions andor settings Braking shall be effected by releasing the control levers
133322 Cranes under test load shall run the full travelling distance or at maximum load radius slowlycover the full swinging or slewing range Additionally the minimum load radius shall be tested and in thecase of cranes with radius dependent nominal loads also an intermediate value
133323 Regarding crane columns and their integration into the ships hull as well as lifting appliancefoundations in general tests according to [133321] are required in longitudinal and transverse directionsof the ship ie to fore and aft and to port and starboard each
133324 For lifting appliances used for cargo handling one emergency brake test with the test load byoperating the emergency switch or button shall be carried out either at the manufacturers or at the place ofoperation
133325 When carrying out the load test care shall be taken to ensure that all movable parts are able tooperate freely in all the lifting appliance andor derrick booms positions all ropes are unobstructed by anyother parts and the ropes can wind satisfactorily onto the winch drums
133326 In the case of ramps the test load arrangement shall conform to the intended operating mode
13333 Requirements for hoisting winches
133331 If the pull of the hoisting-winch is insufficient to lift the test load a second winch or other liftingappliance may be brought in to assist with the hoist Braking and holding the test load however shall beaccomplished using solely the winch belonging to the lifting appliance
133332 Where hoisting-winches have not lifted the test load by themselves proof shall be obtained bytesting that with the maximum number of layers of rope on the winch drum the nominal load is hoistedsatisfactorily by the winches
133333 The ability of the winch to hold the test load with the drive to the winch switched off shall beproved In doing so no slip shall occur with the exception of hydraulic winches without standstill brakes see[136824]
133334 Hydraulic cranesIf hydraulic cranes are unable to lift a test load 25 greater than the nominal load because of the pressurelimit lifting the maximum possible load is sufficient This shall however exceed the nominal load by at least10
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DNV GL AS
1334 Examination13341 Documentation check
133411 Priority shall be given to checking if the examination of drawings for lifting appliances cranecolumns boom supports and lashing equipment foundations runways and all supporting structures has beenconcluded successfully and if all structural modifications or changes possibly resulting therefrom have beencarried out
133412 Supervision of construction shall be documented by test certificates The lifting appliancedocumentation remaining onboard shall include
mdash rigging plansmdash test certificates for interchangeable components and loose gearmdash test certificates for ropes
133413 Regarding the certificates stated in [133412] their correct correlation to the certified structuralparts or components shall be checked by comparing the stamping andor properties of these partsThe certificates shall be checked with respect to correctness in form and content
13342 General visual inspectionThe general visual inspection may eg refer to the following checks
mdash general condition completeness and correct riggingmdash assembly interfaces between components constructed on site and components suppliedmdash undisturbed power transmission through transversely arranged plates such as deck plates (Where
required this shall be checked by means of drilling holes which shall be welded up after the check)mdash inscription of number SWL and where required load radiusmdash warning and indication signboards as well as warning paintwork where requiredmdash accesses to lifting appliances and to control standsmdash accesses to driver cabins and working and control platforms inside and outside the lifting appliance and to
boom supportsmdash emergency descentsmdash condition and equipping of control stands and driver cabinsmdash working area of the lifting appliancemdash range(s) of sight for the operator from inside the driver cabin
13343 Examination after the load testAfter the load test the load-bearing components of lifting appliance shall undergo a visual examinationThis examination shall if possible exclude the formation of possibly permanent deformations or cracks atforce application points or at special design details
1335 Stamping
13351 If the initial tests and examinations have not given rise to any objections the lifting appliance shallbe stamped before the relevant certificates are issued
13352 Cranes with boom shall be stamped at the bottom end of the right-hand jib member and next tothe point where that member is connected to the crane house and in a prominent position on all other liftingappliances
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DNV GL AS
13353 The stamp shall contain the following information
mdash shipboard number of the lifting appliancemdash stamp with the month and year of testmdash nominal load of the lifting appliance in [t] or where required in [kg] and the permissible minimum and
maximum crane load radius in [m] Where the nominal load varies with the load radius the nominal loadand the corresponding load radius shall be stated for the maximum and minimum values
mdash certificate number and distinguishing letters of the Society
1336 Certification of the initial tests and examinations
13361 Following performance of the tests and examinations and stamping the Societys surveyor issuesthe certificate Form CG2 for load-tested lifting appliances handling cargo and OLA101 for load tested liftingappliances not handling cargo
13362 The tests and examinations of the lifting appliance are confirmed by the Societys surveyor in aregister book of Form CG1 to which the certificate and the survey report are added
13363 The certification and documentation system for shipboard lifting appliances is described in [137]
134 Periodic tests and examinations
1341 General notes
13411 Shipboard lifting appliances subject to periodic supervision by the Society shall be examined atregular intervals by the Societys surveyor and subjected to load tests in his presence
13412 The intervals between examinations and between the load tests described below are customaryinternationally Deviating national requirements shall be taken into account if applicable
13413 In cases where a lifting appliance dependent on an external power supply is tested therequirements given in [13312] apply
1342 Due dates13421 Examinations
134211 Lifting appliances and loose gear shall be examined annually by the Societys surveyor unlessother intervals are required by national regulationsThe operator is as a matter of principle obliged to give the Society due notice of the examination
134212 The following examinations vary depending on type and scope
mdash annual examinations see [1343]mdash five-yearly examinations see [1344]
13422 Load tests
134221 No later than five years after the load test a further load test is required for shipboard liftingappliances to be performed in the presence of the Societys surveyorThe operator is as a matter of principle obliged to give the Society due notice of the load testA regular recurrent load test of loose gear is not required internationally by ILO
Standard mdash DNVGL-ST-0377 Edition May 2016 Page 243Standard for shipboard lifting appliances
DNV GL AS
134222 For practical reasons load tests shall coincide if possible with the five-yearly examination
13423 Exceeding the due date
134231 In the case of shipboard lifting appliances subject to the regulations of ILO the intervals of oneand five years regarding examinations and load tests shall not be exceededThis applies on the analogy to recurrent thorough examinations of loose gear
134232 In the case of lifting appliances not subject to the ILO regulations the interval stated in[134231] may be exceeded by up to three months when admitted by the Flag State Administration Thisapplies also to related loose gearThis does not however postpone the due date of the next examination The same applies inversely to testsperformed before the due date
134233 Where the intervals stated in [134231] and [134232] are exceeded the validity of entrieson examinations performed and the validity of test certificates expires in the register bookIn the case of classified shipboard lifting appliances the respective class notation is suspended once the fiveyear interval has been exceeded by more than three months
1343 Annual examinationsThe purpose of annual examinations shall confirm technical safety of operation within the periods of five-yearly examinations
13431 Scope of examinations
134311 The scope of examinations depends on age condition and frequency of use of lifting appliancesNormally lifting appliances need not be unrigged and dis-mantled for the performance of yearlyexaminations
134312 Essentially the scope of examination comprises
mdash checking documentation and certificates for completeness and validity and with reference to maintenanceand inspection measures arranged or performed by the shiprsquos management
mdash checking for completeness and correct rigging or reeving respectively using the rigging plansmdash checking for damage wear deformation corrosion soiling oil leakage etcmdash checking for proper markingmdash function test using available loadmdash random examination of the interchangeable components and correlation to the relevant certificates based
on the stamps appliedmdash verification of newly-fitted partsmdash recording the examination carried out in the register book or where required in a corresponding
certificatemdash preparation of a survey report
134313 The list in [134312] is by way of an example The actual scope of tests and examinations isat the discretion of the Societys surveyor whereby negative findings may require further examinations ormeasures see [13442]
13432 Dealing with components
134321 Use of steels liable to age is not permitted as a matter of principle so that heat treatment ofcomponents at regular intervals is not required
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DNV GL AS
134322 Components which do not comply with these rules or which are worn to the permitted limits shallbe replaced by new ones with the prescribed dimensions
134323 Any parts renewed since the last examination shall be submitted to the Societys surveyortogether with the certificates required
1344 Five-yearly examinations13441 General notes
134411 The purpose of five-yearly tests and examinations shall confirm or generate a solid technical basisfor the upcoming annual examinations
134412 Five-yearly examinations and load tests shall be performed if possible at the time of ClassRenewal ie during the period in shipyard refit to have available sufficient technical equipment test weightsand interchangeable components if necessary
13442 Scope of examinationsIn accordance with these rules five-yearly examinations shall extend and complement the examinationsdescribed in [13431] and where required the measures described thereafter which may if necessary beextended
134421 Examination of structural and interchangeable components1344211 If deemed necessary by the Societys surveyor individual parts shall be dismantled andif necessary unrigged for the examination All parts found to be unsafe to operate shall be repaired orreplaced1344212 The Societys surveyor is entitled to demand a load test or a load test repeat for liftingappliances interchangeable components or loose gear if deemed necessary
134422 Examination of slew rings1344221 Slew rings shall be examined with respect to bearing clearance noise lubrication andcorrosionThe tight fit of the pins shall be checked by at least one random hammer testWhere increased internal wear is suspected extruded grease shall be checked by an appropriate method forabraded particles1344222 Slew rings of shipboard cargo cranes operating at sea which are not equipped with specialcontrol and measuring devices shall be checked regularly by special control measures agreed with themanufacturerWhere increased internal wear becomes apparent it may be required to remove the slew ring and todismantle it for examination1344223 The associated drives and brakes shall be checked with respect to wear function and generalcondition
134423 Examination of hydraulic cylindersApart from a thorough visual examination with respect to straightness oil leakage bearing clearance andabsence of cracks in the connecting structures a function test of pipe burst safety valves or similar safetycomponents with available load is required
134424 Examination of winchesWinches shall be examined with respect to
mdash condition fastening and functionmdash wear to brakes rope grooves and flanged discsmdash sufficient lubrication
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DNV GL AS
mdash function of safety equipmentmdash correct rope windingmdash observance of the required three safety turnsmdash tight fit and absence of corrosion of the rope-end attachment(s)
134425 Crack testsWhere a visual inspection gives reason for this the Societys surveyor may request crack tests using theprocedure appropriate to each caseThe following areas of design need particular attention
mdash flange connection of the slew ring at the crane column or the foundationmdash connections between longitudinal and transverse structural members of crane boomsmdash bend areas of all kinds especially on crane columnsmdash connections between crane columns and hatch coamingsmdash corner connections of crane gantriesmdash power transmission in the direction of thickness of platesmdash special (noticeable) details of construction
134426 Examination for corrosionThe following areas of design need particular attention
mdash supporting areas of crane booms at stowage devicesmdash loose ropes with downward hanging end attachments see [85313]mdash contact areas without watertight sealing eg in case of welded eye platesmdash special areas of design where water my accumulate
1345 Load tests
13451 For the performance of load tests the requirements given in [1333] apply however no emergencyshut-down test is required nor tests with several different nominal loads load radii and ship directions
13452 At the five-yearly load tests of shipboard lifting appliances normal testing of the maximum nominalload at the associated maximum load radius will suffice
13453 At the five-yearly load tests the tests are if possible to be performed using weights The weightsshall be calibrated and certified or verifiable
13454 The magnitude of test load shall correspond to Table 13-2 In exceptional cases a lower testload may be used with hydraulically driven lifting appliances where the working pressure cannot becorrespondingly increased see [133334]
13455 Five-yearly load tests of lifting appliances under deck may also be effected using a calibrated loadmeasuring instrument whose indication of measured values shall remain constant for five minutesThe instrument shall have an accuracy of plusmn 25If the nominal load LNe of any lifting appliance exceeds 15 t use of a load measuring instrument as far aspossible shall be avoided
1346 Confirmation of periodic tests and examinations
13461 Following performance of the tests and examinations the Societys surveyor will issue thecertificate Form CG2 for load-tested lifting appliances handling cargo and OLA101 for load tested liftingappliances not handling cargo
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DNV GL AS
13462 The tests and examinations of the lifting appliances used for cargo handling and associated loosegear will be certified by the Societys surveyor in the register book Form CG1 Part I II and the certificateplus survey report added to the register book
13463 The tests and examinations of the lifting appliances not used for cargo handling and associatedloosed gear will be certified by the Societys surveyor in the register book Form CG1 Part IV V
13464 The stamping required according to [1335] in advance of the issuing of certificates is in generalnot required for periodic load tests
13465 The system of certification and documentation for lifting appliances is described in [137]
135 Extraordinary tests and examinationsModifications damage renewals and special occasions may require extraordinary load tests andorexaminations as described in the following
1351 General notes
13511 The operator shall inform the Society if essential modifications are intended to be made to liftingappliances or loose gear when damage affecting safety has occurred or renewal of load-bearing structuralelements shall be carried out
13512 In the cases described above the Society decides on the respective measures examinations andload tests
13513 Any essential modification and any repair or renewal of load-bearing components with theexception of ropes and interchangeable components shall be carried out under the supervision of theSociety Where this is not possible in individual cases because of the circumstances a re-examination shallbe carried out on a suitable date
13514 Extraordinary load tests and examinations may be credited towards the periodic tests andexaminations if they comply with the prescribed conditions with respect to type and scope
13515 All load tests shall be performed using weights in the manner described in [1345]Regarding certification of tests and examinations the requirements given in [1346] apply
1352 Essential modifications
13521 Essential modifications are subject to the same tests and examinations as the initial manufacture
13522 Essential modifications include besides renewal of load-bearing components modifications of
mdash nominal loadmdash load radiusmdash hoisting andor luffing systemsmdash cable tackle system unless different types of reeve are provided in the designmdash load-bearing components
13523 Non-essential modifications include modifications which will in no way affect safety andor functionof lifting appliances or loose gear Such modifications shall be presented to the Society surveyor on his firstvisit to the ship after the modification has been carried out
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DNV GL AS
1353 Damage
13531 The requirements given in [136] shall be observed when an evaluation is made whether damageunduly affects the safety of lifting appliances or loose gear
13532 Damage affecting safety requires an examination of the damage and a repair plan with specificdetails which is subject to approval by the SocietyFollowing repair an examination within the necessary scope and a load test are required
13533 Depending on the evaluation of the damage lifting appliances or loose gear shall be put out ofoperation or where required be operated at reduced nominal load andor load radiusRegarding repairs and operation at reduced nominal load the requirements given in [1369] apply
13534 Damage which does not affect safety shall be presented to the Societys surveyor at the first visitto the ship after the occurrence of the damage
1354 Renewals
13541 Following each renewal of load-bearing components of lifting appliances and loose gear a load testand an associated examination of this gear is required
13542 The requirements ogiven in [13541] do not apply to ropes and interchangeable componentsbecause these are tested examined and certified independentlyRenewal of axes pins rope-sheaves etc do not in general require a new load testThe renewal of all parts mentioned shall be pointed out to the Societys surveyor on the occasion of thefollowing examination
13543 Following replacement or repair of winches a load test is required unless the winch has been load-tested on a test plant and certified accordingly
13544 Special occasionsThe Society reserves the right to ask for extraordinary load tests andor examinations in specially justifiedcases
136 Wear damage repair
1361 General notes
13611 The details which follow regarding deformation wear tolerances etc shall be considered asreference values to assess the remaining margin of safety of damaged corroded or worn componentsIn the case of major damage of shipboard lifting appliances or in cases of doubt the Society shall beconsulted
13612 Any damaged worn or corroded part which is not replaced shall once the tolerances have beenexceeded be restored to the original dimensions using equivalent materialsRegarding an alternative reduction of the nominal load see [13691]
13613 For worn or corroded parts which are close to reaching the tolerance limits the Societys surveyormay determine a time period for repair or replacement
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DNV GL AS
13614 Regarding loose gear interchangeable components and ropes reference is also made to [75] and[8533]
1362 Acceptable reduction of plate thickness
13621 For plates profiles and pipes the acceptable reduction of plate thickness is 10
13622 In cases of limited local corrosion or wear a reduction of plate thickness of up to 20 is acceptableprovided this does not result in a reduction of the load-bearing capacity of the cross-section
13623 In cases of isolated pitting a reduction of plate thickness of up to 30 is acceptable
13624 Due to the above reductions of plate thickness the characteristic values of a cross-section underconsideration may be weakened at the most by 5
1363 Acceptable cracks
13631 In category 1 components (see Table 13-1) no cracks can be tolerated
13632 In lateral wind bracing latticework crosspieces and similar stiffeners or knee plates whose purposeis to reduce the slenderness ratio or stiffen load-bearing structures cracks up to the following lengths areacceptable if there is evidence that they do not extend into the load-bearing structure
mdash 10 of the connection lengthmdash 3 times plate thickness
the lower of the two values applyingIn the case of pipes the connection length is the circumferenceIn the case of box girders or beams each chord web and flange width shall be considered separately as aconnection length
1364 Acceptable deformations13641 Deflections
136411 Compression bars1364111 Under the maximum permissible loading compression bars may not display uniform deflectiongreater than the equivalent of the bar length divided by 2501364112 Unstressed compression bars or those stressed only by their own weight which are category 1components may not display uniform deflection greater than the equivalent of the bar length divided by 5001364113 Unstressed compression bars or those stressed only by their own weight which are category2 components such as lateral wind bracing or latticework crosspieces may not display uniform deflectiongreater than the equivalent of the bar length divided by 350
136412 Tension barsTension bars shall not when unstressed display uniform deflection greater than the equivalent of the barlength divided by 50
136413 Boomsjibs1364131 For booms subject to compressive stress under permissible load the requirements given in[1364111] apply The uniform deflection due to the dead weight alone shall not be greater than theequivalent of the crane boom length divided by 350
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DNV GL AS
1364132 The lowering of the top of the boom under load andor dead weight is not limited when thepermissible load is observed
13642 Deformation of chords and flanges
136421 I-BeamsEach half-flange may individually or together be deformed by up to 15 of its breadth measured from webto outer edge
136422 Angle profilesFlanges of angle profiles may individually or together be deformed by up to 15 of their breadth measuredfrom flange to outer edge
1365 Acceptable indentationsThe following requirements presuppose smooth transition pieces and apply provided that no bends foldscracks or thinning have developed
13651 Compression bars
136511 Cylindrical pipes1365111 Pipes forming category 1 components
The following conditions shall be observed
ℓ le d
b le 025 d
f le 05 t
where
ℓ = length of indentation measured in the longitudinal direction of the pipeb = breadth of indentationf = depth of indentation (depth gauge)d = outer diametert = wall thickness
1365112 Pipes forming category 2 components
The following conditions shall be observed
a) central range (13 ℓ) b) outer range
ℓ le d ℓ le 15 middot d
b le 05 middot d b le 07 middot d
f le t f le 2 middot t
136512 Rectangular tubes and box girders1365121 In the case of rectangular tubes and box girders indentations at the corners may have a depthcorresponding to 8 of the smallest side dimension1365122 For acceptable indentations of plates the requirements for cylindrical pipes similarly applyInstead of the diameter the side dimension of the plate under consideration shall be taken
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DNV GL AS
136513 I-BeamsThe webs of I-beams may not have any indentations
136514 Angle profilesAngle profiles may not have any indentations at the corners
13652 Tension barsIn the case of tension bars the indentation depth may be up to one third of the indentation length The outerdimensions of hollow profiles however shall not be reduced by more than 25 in the indentation areaIf necessary the requirements given in Sec2 [352] shall be observed
13653 Girders subject to bending
136531 Indentations at bearing or load introduction points are not acceptable
136532 In areas other than mentioned in [136531] the rule is that indentations up to the dimensionsin [136511] and [136512] are acceptable on the tension side on the compression side onlydimensions of half that size
1366 Acceptable wear on rope-sheaves
13661 The side wall thickness of rope sheaves made from normal-strength materials shall meet thefollowing condition at the bottom of the groove
t = side wall thickness [mm]FS = static rope pull according to [8232] [kN]
13662 The details at [13661] apply to disc or spoked DIN rope-sheaves meeting the Dd ratiostipulated in Table 8-3Rope-sheaves of grey cast iron are not permitted
13663 The wall thickness according to [13661] may reduce in an upward direction to 13 at theoutermost edge
13664 Rope imprints located at the bottom of the rope groove require a change to the pairing of rope andrope-sheave
1367 Acceptable wear on pinsincrease of bearing clearances13671 PinsFrom the point of view of load-bearing capacity a reduction in diameter of 10 is acceptable
13672 Bearing clearance
136721 Foot bearingsThe tolerable increase of bearing clearance is two times the initial clearance