rvs.T. T. V^c ,e

I DISTRIBUTION SHEET

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of 1 D is t r ibu t ion

From Equipment Stress Analysis/8D430

Date December 12, 1994

Project Title/Work Order Des- gn for Tank 241SY101 Pump Removal

EDTNo. 608386 Miscellaneous Component N2B2K

Des- gn for Tank 241SY101 Pump Removal ECN No. NA

Name MSIN Text

With All Attach.

Text Only Attach./ Appendix

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R. M. Boger J . S. Burgess C. E. Hanson F. H. Huang R. L. Jorissen J. W. Lentsch M. L. McElroy G. E. McPherson T. C. Mackey M. J . Ostrom R. B. Pan Central Files (2 Copies) rvs.T. T. V^c r ,e.o

L4-90 X G2-03 X H5-09 . X H5-67 X H5-53 X S7-15 X Sl-51 X S2-41 X S2-03 X H5-68 X H5-53 X L8-04 X L-S-O") K

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5. Proj./Prog./Dept./Div.: 6. Cog. Engr.: 7. Purchase Order No.: NA

8 . Or ig inator Remarks:

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1. WHC-SD-WM-DA-168 NA Miscellaneous Component Design for Tank 241SY101 Pump Removal

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1, 2, 3, or 4 (see MRP 5.43)

1. Approval 4. Review 2. Release 5. Post-Review 3. Information 6. Dist. (Receipt Acknow. Required)

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(J) Name

R. L. Jorissen

(K) Signature (L) Date (Ml MSIN Reason

Disp.

^ V ^ / V VH5-53

ESA Mngr. R.B. Pan J ^ / l J^—^/fH™-5*

N. L. H c E l r o y ^ , z f p ^ < g ^ j / a / ? g S 1 - 5 7 QA

Safety G. E. McPherson/g. f ffce^ J4»4e-

WL SZ-<*( I-Q1-9H

T. C. Mackey *2- "V? S2-03

Indep. Review J . S. Burges _s^ 7/MI5-53

18.

F. H. Huang

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Portions of this document may be illegible in electronic image products, images are produced from the best available original document.

RELEASE AUTHORIZATION

Document Number: WHC-SD-WM-DA-168, REV 0

Document Title: Miscellaneous Component Design for Tank 241SY101 Pump Removal

Release Date: 2/28/95

This document was reviewed following the procedures described in WHC-CM-3-4 and is:

APPROVED FOR PUBLIC RELEASE

WHC Information Release Administration Specialist:

February 28, 1995

TRADEMARK DISCLAIMER. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof or its contractors or subcontractors.

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DISCLAIMER

A-6001-400.2 (09/94) WEF256

This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof.

SUPPORTING DOCUMENT 1. Total Pages, 'O ! ~-j

T i t l e

Miscellaneous Component Design for Tank 241SY101 Pump Removal

3 . Number

WHC-SD-WM-DA-168 Rev Mo.

5. Key Words

Analysis, Bending, Mock-up pump Test weight, Support saddle, Spreader beam, Safety fac tor weld strength, l i f t i n g lug

• ""PROVED FOR

Author

Name: F. H. Huang

Signature iZvP-X ^

\ s

7 s j j , 0 O Organization/Charge Code

8D430/Mgg4A^/V2 t>2 £-

The disposal equipment is designed for use in removing the hydrogen mixer pump from tank 241SY101. The design of the structural elements of the equipment is based on the design criteria established for this task as shown in Reference WHC-SD-WM-DA-165. AEC designed and analyzed the lifting beam, support saddles, test weight, and modified mock-up pump. WHC conducted additional analyses on the test weight, mock-up pump, removable support, and saddle modification for air pallets. The calculations meet the strength requirements and verify the equipment with the load chart for the equipment removal system (ERS) for tank 241SY101.

Abstract

J&n£ VgÂ" 8. PURPOSE AND USE OF DOCUMENT - This document was prepared for use

wHbin the U.S. Department of Energy and its contractors.^^ is to be oêd only to perform, direct, or integrate i^rk under U.S. Department of Energy contracts. This document isôt approved for publ^êlease until reviewed, PATENT STATUS^t This document copy, since i l ^ s transmitted in advance of patent^ lea ranee, is made available^n confidence solely for use in per^rmance of work undent contracts with the U.S. Department of Enocgy. This documentJ^ not to be published nor its contents otherwise aiyseminated or used for purposes other than specified above before pa^nt approvalfor such release or use has been secured, upon request, rtom theâtent Counsel, U.S. Department of Energy Field Office, Richlanl^JA.

DISCLAIMER - This report J(ffs prqaared as an account of work sponsored by an agency of tire United S^^tes Government. Neither the United States Governmenjîor any agency^hereof, nor any of their employees, nor any o^^heir contractors^Nûbcontractors or their employees, makes an^warranty, express or lmWied, or assumes any legal liability orêsponsibility for the accurate completeness, or any third party^ruse or the results of such use o^qny information, apparatus, profluct, or process disclosed, or represenSt that its use would not infringe privately owned rights. Reference fratein to any specificômmercial product, process, or service by tiSde name, trademajK, manufacturer, or otherwise, does not neceSârily cons^*ute or imply its endorsement, recommendation, or favorirWby th^rUnited States Government or any agency thereof or rcs Sntractors or subcontractors. The views and opinions of authors

expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof.

9. Impact Level SQ

10. RELEASE STAMP

•J .Si ' 2

<3w*«r : 1995

hr-.-rk J*?"'

A-6400-073 (11/91) CEF} UEF124

%;< C -X

MISCELLANEOUS COMPONENT DESIGN FOR TANK 241SY101 PUMP REMOVAL

December 1994

PREPARED BY: A ' / A <Jtw.s F. H. Huang Materials Engineer^

£2&3£ Date / ^ / ? / ^

REVIEWED BY: S. Burgess

Equipment Stress Analysis Date j^/9/94.

APPROVED BY; n ,A B. Pan, Manager

Equipment Stress Analysis

Date p-M* j

Westinghouse Hanford Company Hanford Operations and Engineering Contractor

for the U. S. Department of Energy #S

I DISTRIBUTION'OF THIS DOCUMENT IS UNLIMITED

WHC-SD-WM-DA-168 * Rev. 0

DESIGN VERIFICATION METHOD

The need for design verification has been reviewed with the method selected as indicated below:

Independent Review

Alternate Calculations

Qualification Testing

Formal Design Review

R. B. P a n X V ^ ' ' ^ CognizanC/Project/Design Manager

SD #WHC-SD-WM-DA-168

ECN # N A

ii

WHC-SD-WM-DA-168 Rev. 0

TYPICAL CHECKLIST FOR INDEPENDENT REVIEW

Document Reviewed WHC-SD-WM-DA-168

Author F. H. Huano

Yes No N/A

Problem completely defined.

Necessary assumptions explicitly stated and supported.

Computer codes and data files documented.

Data used in calculations explicitly stated in document. Data checked for consistency with original source information as applicable.

Mathematical derivations checked including dimensional consistency of results.

Models appropriate and used within range of validity or use outside range of established validity justified.

Hand calculations checked for errors.

Code run streams correct and consistent with analysis documentation.

Code output consistent with input and with results reported in analysis documentation.

Acceptability limits on analytical results applicable and supported. Limits checked against sources.

Safety margins consistent with good engineering practices.

Conclusions consistent with analytical results and applicable limits.

Results and conclusions address all points required in the problem statement.

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MANDATORY Software QA Log Number N/A

J. S. Burgess Reviewer

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iii

* WHC-SD-WM-DA-168

Rev. 0

CONTENTS

1.0 INTRODUCTION 1 2.0 SUMMARY 1 3.0 DISCUSSION 2

3.1 Spreader Beam 2 3.2 Support Saddle . . . . . . . . . . 2 3.3 Test Weight 2 3.4 Mock-up Pump Modification . . . . . 3 3.5 Removable Support for the Transport Assembly . . . . . . . . . 3 3.6 Saddle Modification for Air Pallets . . . . . . . . . . . . . . 4

4.0 REFERENCES . 5

Appendix A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A-l Temporary Pump 2 Structural Engineering Support of Hydrogen Mitigation in Tank SY-101, Advanced Engineering Consultants

Appendix B B-l Additional Analysis of Container Test Weight for Tank 241SY101

Appendix C C-l Additional Analysis of Mock-up Pump Modification for Tank 241SY101

Appendix D . . . . . . . . . . . . . . . . . . . . . . . D-l Analysis of Removable Support for the Transport Assembly

Appendix E E-l Analaysis of Saddle Modification for Air Pallets

FIGURE

1. Load Chart of the Equipment Removal System for Tank 241SY101 7

iv


MISCELLANEOUS COMPONENT DESIGN FOR TANK 241SY101 PUMP REMOVAL 1.0 INTRODUCTION

A mixer pump has been used to mitigate the hydrogen build-up in tank 241SY101 (SY101), located in the 200 West Area of the Hanford Site. New equipment is being prepared for the removal, transport, storage, and disposal of the test pump. The disposal equipment for the test pump now in tank SY101 includes a shipping container, a strongback, a lifting beam, a test weight, container support stands, a modified mock-up pump, a flexible receiver blast shield, a lifting yoke, and a yoke brace. The structural evaluations of container and strongback are detailed in another supporting document (WHC 1994a), the engineering analyses of flexible receiver blast shield/lifting yoke and yoke brace are given in other supporting documents (WHC 1994b, WHC 1994c), respectively. Engineering tasks that were contracted to Advanced Engineering Consultants (AEC) include the design and analysis of the following.

• Two spreader-beam lifting devices. • Container test weight. • Container support saddles. • Mock-up pump modification. This report documents the work description, design basis, assumptions,

and design calculations provided by AEC for the above components. All AEC documents appear in Appendix A. Additional work conducted by Westinghouse Hanford Company (WHC) on the modified container test weight, modification to the mock-up pump, the removable support for the transport assembly, and saddle modification for air pallets also are included in this document.

This supporting document reports on the structural analysis of the equipment based on requirements for safety class 3 (DOE-RL 1993a), the Manual of Steel Construction (AISC 1989), and the Hanford Hoisting and Rigging Manual (DOE-RL 1993b).

2.0 SUMMARY The disposal equipment is designed for use in removing the hydrogen

mixer pump from tank SY101. The design of the structural elements of the equipment is based on the design criteria established for this task as shown in WHC 1994a. AEC designed and analyzed the lifting beam, support saddles, test weight, and modified mock-up pump. WHC conducted additional analyses on the test weight, mock-up pump, removable support, and saddle modification. The calculations meet the strength requirements and verify the equipment with the load chart for the equipment removal system (ERS) for the tank, as shown in Figure 1, which illustrates the design wind, live, and dead loads for the trailer and strongback.

1

WHC-SD-WM-DA-168 *" Rev. 0

3.0 DISCUSSION

The design criteria are listed in WHC 1994a and in Appendix A. The following allowable stresses are used for the structural calculations of steel members and connections in those critical components of tank SYlOl that are of A-36 steel or other mild steels: 12,000 lbf/in2 for bending, tension, axial compression, and bearing stresses; 7,200 lbf/in2 for shear stress; 7,200 lbf/in on the effective area for welds; and one-half the allowable stresses given in AISC 1989 for bolts. Basically, the allowable stresses are one-third the yield strength.

3.1 Spreader Beam

The major part of the 7.5-ft-long spreader beam is made of W18X106. A 3-in-thick lug with a 2 13/16-in diameter hole is full-penetration welded to the top of the W beam. Underneath the lug plate are two ^-in. stiffener plates welded to each side of the beam to ensure that stress is transferred from the flange to the web. The calculations consider the stresses of the spreader beam for a design load of 125 kips and a rated load of 100 kips per DOE-RL-92-36 (DOE-RL 1993b).

3.2 Support Saddle

The container support saddles are designed to withstand a linear uniform load of 2,455 lb/ft, concentrated loads of 5,000 and 7,000 lb, and a wind load of 11.43 Ibf/ft2. The 2,455 lb/ft uniform load is not shown in the Figure 1 load chart because the weight of the radiation shielding material is not included in Figure 1. Also, the 11.43 Ibf/ft2 wind load differs from the Figure 1 load chart value of 10 lbf/ft because the container is subjected to different design wind velocities in the vertical position versus the horizontal storage position. Each saddle, measuring 4 by 8 by 1.5 ft in height, is designed to ensure that the Central Waste Complex floor slab is not damaged. Two lugs are welded at the tops of the saddle ends to hold the container with a chain. The calculations check the bending and the tear-out stresses on the lugs. The sliding force and overturning moment from wind meet the required safety factor of 1.5.

3.3 Test Weight

The test weight assembly, used for testing the hydraulic system on the trailer, is designed to simulate the pump weight. During testing, the test weights are attached at the top of the container. The total weight of the test weight assembly (16,324 lb) was determined by evaluating the load chart in Figure 1. Placing the test weight assembly at the top of the container simulates the load on the hydraulic system as if the pump was actually in the container. This weight is equivalent to 125% of the actual weight of the pump lifted by the hydraulic system. The weight assembly consists of a bulkhead

2


plate, removable filler plates, and support legs. Six 5-ft by 5-ft by 2-in. filler plates are required to make a test weight assembly of 16,324 lb. The center of gravity (C.G.) for the assembly is calculated to determine the location of hole of each filler plate through which a 3-in.-diameter rod is used for horizontal lift. The AEC calculations check the tear-out resistance of the vertical and horizontal lugs. The calculations also check the weld strengths and bending stresses of the support legs (W8X28 beams) and the lug plates. After AEC completed the design, a live load of 3,000 lb was added at the top of the container near the test weight, so the weight of the test weight had to be recalculated. With a hydraulic force of 203,600 lb and an • updated container uniform load of 928 lb/ft compared to 1,000 lb/ft shown in Figure 1, the weight of the new test weight is calculated to be 20,657 lb. A slight modification on the AEC design was made by adding two 2-in.-thick filler plates. This change necessitated a reanalysis of the weld strengths and bending stresses of the support legs and the lug plates to ensure that the AISC requirements were still met (see Appendix B).

3.4 Mock-up Pump Modification

A mock-up pump is used to simulate installation and removal of the actual pump. To verify the lifting capacity of the cradle and for testing the hydraulic trailer, the mock-up pump is made with its dimensions, weight, and C.G. equivalent to those of the actual pump. AEC made some modifications to the existing mock-up pump to simulate the weight and C.G. of the actual pump and designed removable disks that can be attached to the mock-up pump. To simplify lifting the mock-up pump, a two-point lifting was designed. Both lifting points are at the locations 14 ft from the two ends of the mock-up pump.

The dimensions of the pump sections and the locations of the disks are shown in drawing H-2-83749. The maximum bending stress with an impact factor of 125% during horizontal lifting is 9,200 lbf/in2, less than the allowable stress of 12,000 lbf/in2 (Appendix C).

3.5 Removable Support for the Transport Assembly

The temporary container support will be attached to the lateral support cradle for the container after the container is raised hydraulically to the vertical position to accept the experimental pump. Once the pump is inserted into the container, both pump and container are rotated and lowered to rest on the removable support, which is inclined 7° with respect to the ground. The container support is inclined to prevent fluid from draining from the contaminated pump while it rests on the support to allow the following tasks: removing the external container funnel from the container inner flange, cutting off the 16-in. pump column, and installing the inner and outer container caps. To minimize contamination during work, an 11- by 11-ft shielding plate is.attached vertically to the trailer support. After these

3


tasks are completed, the container is raised and the removable support for the transport assembly is removed. The container then is lowered to the horizontal position and transported to the shot loading area designated to receive it.

The total weight of the container and pump with an impact factor of 125% is 83,000 lb. The bearing stress of the W30xl91 beams, which support the container, the pump, and the shielding plate, is checked to be within the allowable stress. The web crippling of the beams also is found to be below the load limit. Standing above the beams is the shielding plate, which has a face 11 by 11 ft receiving significant wind load. The wind pressure acting on the 11- by 11-ft shielding plate is 19.35 lbf/ft2, or a total force of 2,340 lb against the plate, estimated on the basis of SDC 4.1 (DOE-RL 1993a) for safety class 3 structures. Analysis that shows bending of the 1-in. shielding plate as a result of wind load meets the strength requirements of the AISC (1989).

The vertical shielding plate is supported by two braces that consist of L4x3 and L3x3. The strength of each brace is found to satisfy the design criterion. Analysis also shows that the strength of eight 1-in. bolts used to fasten the shielding plate to the existing trailer support is adequate to support the weights of the plate (4,940 lb) and the vertical load of the inclined container (41,347 lb). A significant moment acting on the shielding plate as a result of the eccentric container reactions indicates a need to add stiffeners to reinforce the plate. Calculations determine that three stiffeners %-in. thick and 5-in. wide with a spacing of 5 % in. meet the strength requirements of the AISC for the combined axial and bending stresses of the reinforced shielding plate (see Appendix D for calculation details). All welds in the removable support are found to have adequate strength.

3.6 Saddle Modification for Air Pallets Because air pallets will be used to move the container and pump into the

2403WD storage building, the container support saddles are modified to accept two air pallets for each support. The size of the air pallets is determined from the reaction force at a location 68 in. from the top cap of the container. On the basis of the linear uniform load of 2,455 lb/ft and concentrated loads of 5,000 and 7,000 lb, the reaction force is found to be 73,053 lb. With the allowable soil bearing pressure of 2,600 lb/ft2, calculations determine that two 5- by 5-ft air pallets are needed to withstand a load of 80,000 lb, which is slightly higher than the half-weight of the container assembly.

The container and pump will be chained to the supports, which rest on the concrete pad. The support is designed to have two air pallets installed underneath and to be capable of resting on the concrete pad without damaging the facility floor. Calculations show that the support need a contact area with the floor of 20 by 120 in. on each side before the air pallets are activated. Thus, the support requires dimensions of 102 by 120 in. with center base area of 62 by 120 in. above the floor to accommodate the two

4


pallets. To satisfy the AISC strength requirement for bending of the support with a span of 62 in., five W12xl9 beams are needed to support the container and pump before the air pallets are inflated. The bending and shear stresses on the 1-in. support plate placed above the beams are calculated to be smaller than the allowable stresses (see Appendix E).

Two fork lifts will guide the assembled container, pump, and saddle support into the facility building after the air pallets are activated and the assembly clears the floor by approximately 1 in. A tow bar is designed to attach to the W12xl9 beams on the container support; the end of the tow bar has an eye for connection to the fork lift with a trailer hitch pin. The tow bar eye is located at the intersection of two square tubes (5 by 5 by 1/4 in.) that weld to vertical 1 %-in.-thick plates. With pins inserted through the vertical plates and held by the support structure, the tow bar eye is capable of rotating so that it can reach the connector of the fork lift, which is 6 to 12 in. higher than the container support. Because the square tube is much stiffer than the plate, the structural evaluations for the tow bar consider the combined bending and compression of the vertical plate subjected to a maximum load of 18,000 lb and restrained by the square tube. Analysis of an elastic straight beam with one end guided and the other end simply supported (Young 1989) determines that the combined maximum bending and compression stresses of the plate satisfy the strength requirements of the AISC for structural members subjected to combined stresses. Details of the calculations appear in Appendix E.

4.0 REFERENCES AISC, 1989, Manual for Steel Construction, Ninth Edition, American Institute

of Steel Construction, Chicago, Illinois. ASNI, 1986, Special Lifting Devices for Shipping Containers Weighing 10,000

Pounds (4500 kg) or More, American National Standard Institute, New York, New York.

DOE-RL, 1993a, Standard Arch-Civil Design Criteria, Design Loads for Facilities, Hanford Plant Standard SDC-4.1, Rev. 12, U.S. Department of Energy-Richland Field Office, Richland, Washington.

DOE-RL, 1993b, Hanford Site Hoisting and Rigging Manual, D0E-RL-92-36, U.S. Department of Energy, Richland Field Office, Richland, Washington.

WHC, 1994a, Analysis of Container and Strongback for Pump Removal from Tank 241SY101, WHC-SD-WM-DA-165, Westinghouse Hanford Company, Richland, Washington.

WHC, 1994b, Analysis of the Flexible Receiver Lifting Yoke and Blast Shield Assembly (Tank 241SY101), WHC-SD-WM-DA-160, Westinghouse Hanford Company, Richland, Washington.

5


WHC, 1994c, Structural Analysis: Flexible Receiver Yoke Brace for the 241SY101 Mixer Pump, WHC-SD-WM-DA-157, Westinghouse Hanford Company, Richland, Washington.

Young, 1989, Roark's Formulas for Stress and Strain, McGraw-Hill, Inc., New York, New York.

6

WIND LOAD 10 LB/FT' EfTHER DIRECTION

/•CENTERLINE OF C.G 1 EL 7 ' -9 * C.G T EL 7 ' - 0 5/16"

CENTERUNE OF PIN

O'-ff V—OUTRIGGER. EXTENDED

LOCATION TO BE DETERMINED BY TRAILER MFG.

LOAD CHART, 101SY


Appendix A Temporary Pump 2 Structural Engineering Support of

Hydrogen Mitigation in Tank SY-101 Advanced Engineering Consultants

San Francisco, California

A-l

WHC-SD-WM-DA-168 Advanced REV. 0 Engineering _ Consultants P A G E A " z

180 Montgomery Street, Suite 850 San Francisco, CA 94104 Telephone: (415)291-9600 Fax: (415)291-9696

J u l y 1 5 / 1994

Mr. Randy Jorissen Westinghouse Hanford Company P.O. Box 1970, H5-56 Richland, WA 99352 Subject: Calculations for Temporary Pump 2 Structural

Engineering Support of Hydrogen Mitigation in Tank SY101, Task 2 of BOA 322666

Dear Mr. Jorissen: Enclosed is the final set of the subject calculations. This completes our work scope for this Task Order. This has been a challenging and interesting project. Mike Chiao and I have enjoyed working with you and Mr. Tom Mackey on this project, and hope to be able to work with you on future projects. Please call me if you have any questions. Very truly yours.

Lincoln E. Malik President

LEM:rm Enclosure

A-2

Form 3.3-3 Advanced Engineering Consultants sw&ta i

Calculation Cover Sheet WHC-SD-WM-DA-168 REV. 0

PAGE A -3

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Subject TfcM-PtoP-^w-T f^-M-P 2 , ~

Sheet No. • • • I t l

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Subject

Advanced WHC-SD-WM-DA-168 REV. 0

Engineering , Consultants ™ b t rt b

TfeM- fo iUv f i - y pix*A_P X —

T^VyX-h Ce>^ TtrfrJTS

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WHC-SD-WM-DA-168 REV. 0 .


PAGE A - 1 7


PAGE^A- [ £


PAGE A- \°\


PAGE A - 2 0


PAGE A- 2 |


PAGE A - 2 1


PAGE A - 2 3


PAGE A - 2 4

Subject

Advanced Engineering Consultants


PAGE A - 2 - f

L \ P i i A ^ T*>fc<>.»A. < V ^ S f c r * ^ - n > U t v

Sheet No. 1-13

Job/Calc. No. <L£ 1 4 .0-1 , 1 - » 1 - /

Rev. No. 0

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A-25

WHC-SD-WM-DA-168 REV. 0 PAGE A- 10*1

The dummy pump is to be used by WHC to simulate installation and removal of the actual pump. This requires that general dimensions, weight and C.G. of the dummy pump simulate those of the actual pump.

AEC started with a dummy pump designed by others, and was asked in this project to make the changes necessary such that the modified dummy pump will simulate the actual pump weight and C.G.

To accomplish this, AEC needed data on the actual pump, as well as the dummy pump design that is to be modified. The information received from WHC, both documented data and data passed to AEC verbally from WHC engineering staff, is documented on pages 5-33 through 5-35.

Based on the data received, AEC calculated the weight of the dummy pump design based on a materials take off from the design calcs/Dwgs. Actual as-built weights were not available. AEC designed and located eight disks to be added to the dummy pump (as shown in Sheet 6-13) to simulate the weight and C.G. of the actual pump, per data given to AEC.

AEC assumes:

1. The thickness of the end plate of Section 6 (sheet 5-2) will be increased from 3/4 in. to 2 in. such that the weight will be increased by 780 lb., and this change will be shown on Dwg. H-2-821397.

Sheet 5-34 <3-Job/Calc No. CA4001-02-1

Rev. 0 LEM . 6 / 2 7 / 9 4 Ucvo Ufa (<K 4

A-107


PAGE A-\0% Sheet 5-34b

Job/Calc No. CA4001-02-1 Rev. 0

LEM 6/27/94

WHC will assess impact of any changes made to AEG designed dummy pump weights (disks) and/or their locations that might, be required.

The dummy pump will be lifted at two points when the pump is in horizontal position.

3 6 in. and 16 in. pipe diameter joints will be strengthened by WHC and modifications shown on Dwg. H-2-821397.

A-108

/ ^ 5 5 Advanced ^ . ^ M Engineering MEMORANDUM

Consultants [eS ca IUU <> pcfj-o tw ex- <, DATE: Mav o . 1Q94 L ~ i 4


TO: Randy J o r i s s e n (WHC) P A G E A ~ < Z i f

FROM: Lincoln E. Malik

SUBJECT: Tank 241 SY101 Mixer Pump Removal and Installation Project BOA MJB-SMV-322666-002R, AEC Job No. 4001-02

Dear Randy: This memo summarizes the data and clarifications AEC needs to proceed with the subject project: Task 1 - Lifting Beam: 1. The design loads for each of the two lifting beams is not .A clear for us. The scope ,of work calls for a canister plus >Y** pump design weight of 150 Kips. However the load chart we

Q received from you adds up to approximately 70 Kips, which is \ supposed to include an impact factor of 1..2S.

The loads are not uniformly distributed in the canister (the pump head is more heavy than the shaft) . Design of the lifting beams requires that we have the maximum load on either lift beam. We can do this by having a load distribution of the canister and internals, as is given in the load chart, or a maximum lift load per lift beam defined by WHC. In this regard, AEC also has a concern as to whether the design of the lift beams will be consistent with the design of

. X the lifting lugs on the sides of the canister. The plates and , A« V welds now shown on the drawings may not be sufficient for the "P.vjS1 design load'of the pin that will go in them. Also, will WHC J AX ' or AEC. take the responsibility for checking bearing and other

associated loads on the canister lug plates. It does not make good sense to size a large pin for the design loads and factor of safety of 3, if the lug plates are designed for lower loads.

^

tf 0 2. Should lift beam design loads include strongback, or will the strongback be left on the trailer?

3. AEC needs the size of hook used with the lift beams to size the hole in the beam lug plate. Alternatively, we can design

DtSraBUTlON: AEC/4QQI-02. LEMfgTVl A ' * 2 4

a pin to accommodate the hook. This might be a better overall detail both from a design and operations point of view.

4". Lift beam will be designed per AISC working stress design with -allowable' stresses per design criteria for C-106.

Task 2 - Saddles: Our design to-date assumes the following. Please advise if this is -to be different.

Saddles will be designed for load distribution shown on the load chart. Design will be based on AISC working stress design approach for gravity loads only. Seismic aad stLaA. loads have been eliminated from consideration by WHC (per phone conversation of 5 / 6 / 9 4 ) . ^ ^ ^ *V/U/. Saddles will be placed on grout (for leveling) and the coefficient of friction used will be 0.2 (steel to concrete). Fricrion must still be used to resist initial lateral loads from laying the caniscer on the* saddles at (15/ with

• horizontal. L./#° }/i. The saddles will be designed to be placed on the 8" slab-on-

grade with soil bearing pressure of 2600 psf (ref. Dwg. STRL FDN PLAN & DETS).

Y^. Height at low point of saddle is assumed to be 4-3/4" (from A^-t.o. base plate to b.o. radius plate).

<fjb. AEC assumes that the container is designed to span the length between the two lifting lugs. Once the saddles are placed, WHC will check the container to span between the saddles, if necessary. >'

/ , *6/ /J^—~] ^^ [<n


PAGE A- 12-r

p\uk^ 57/% 373- r^-2- f^K

A-125

k-A\»

R<7M ENG [HEERIHG <5f lT M 3 3 . 3 5 .

1 3 9 ! NO,

IS-V\

WHC Response to, AEC FAX (dated Sf"n" 241SY101 Mixer Pump Project

I Lincoln MalikJ

PflQE 2

Respondent

• This correspondence is a follow-up |o our conversation on May 10, 1994, regarding the answers saddles designs

to your quest ons on the

Response to Task 1 Questions/Cdmrnen

Randy Oorissen WHC-SD-WM-DA-168 REV. 0 PAGE A - u b

:s - Lifting

ifting beam and support

Beam 1. ! t I !i

The 101SY load part shows approximately 70 kip total load because it does not include the weight o| the lead shot used for shielding,: which will add an addjtional 66 kip|. The lead'shot must be included in the lifting beam design. As a design load, use 100 kips for each' lifting beam (this 'includes an impactjfactd'r of l:2i5). AEC and WHC musj jointly determine the size of the pin at the container/lifting beam interface. It is WHC's responsibility! to determine structural adequacy=of the container's lug plates; nowever, AEC feel's that the container tugs or welds are inadequate, AEC must discuss their concerns with VJHC until alljparties are satisfied that workable solution has been reached.'(

i r i it Do not include sjtrongback in "lifting beam, will be -left on the trailer. '

if

design loads: the s

AEC will; determine Provide WHC with th« lifting interface. Correct.

rohgback

pin (or clevis) size for the lift beam lug;plate e clevis/lug geometry and WHC will provide*requii provi< required

Response to Task 2 Questions/Comments - Saddles I I ' : " I 'I 1. Do not design saddles for loadj distribution on load chart, as

do not ipclude tjhe lead shot used for shielding. WHC will FA* updated ]oad chart to AEC on 5/11/94 for use in saddle design design for seismic, loads; howe'ver, the saddles must be design (with the weight! of the container, 'Wind loads should have min on saddle design). Use AISC working stress approach and AISC stresses'for saddles.

2.

ithe loads an Do not

d for wine mai effect al1owable

Per our conversation, your plan is to use 2 saddles, one located at each end of the container under the ribs]that attach to the lifting lugs. I WHC will|check the container for the interface loads on the assumption { that the( saddles! support the container over a 1/4 circle. This design ' will preclude the necessity of" leveling multiple saddles. However, if

\ :•

A-l|6

,h, i , > [U~n \

the container cannot withstand theti interface loads with 2 saddles, you [ must gV.to-.a multi-saddle design. !!A steel/concrete friction [coefficient of 0.2 is acceptable. ;I;understand your concern that a 15 degree tilt | angle f ora] horizontal will put higri loads- in one saddle when [the 1 container first* contacts'the saddle - per( our conversation, VJHCVill j limit tKe horizontal tilt angle to '.10 degrees. When the container first contacts a single saddle, thej soil [capacijty allowable of 260d psf may be exceeded .-this'is acceptable; because it is a transient load jand bearing capacity], allowables ara generally b'ased oin settlement. Provide' conceptual design to WHCASAP Correct Correct .(this is the same as £-106) Correct

for checking interface loads.

WHC-SD-WM-DA-168 REV. 0 PAGE A- ill

•• i

l

A-127.

* I

I 'ANALYTICAL CALCULATIC

WHC-SD-WM-DA-168 REV. 0 PAGE A- | ^

Subject lot-sj1: re>MT»/Mgg /^u / fp /LgAf t stioT L.OA& aiST^iduriosi Originator , CALCf, Checker -^SS

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WHC-SD-WM-DA-168 REV. 0 PAGE A- t^«f

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TO HORIS-0NT/M. PC5irjQ>4

A-129


(p.S."b

RECORD OF MEETING • TELECON CO

nATP. 6/2/94

L-i-O

AEC PARTICIPANTS: Mike C.S. Chiao R«.

OTHER PARTICIPANTS:

PROJECT/SUBJECT: —

Randy Jorissen , (WHC)

WHC-SD-WM-DA-168 REV. 0 PAGE A- ISO

WHC Temporary Pump 2/Dummy Pump & Saddles

P.O. MJB-SWV-322666, Task 322666-002, AEC Job 4001-02

DISCUSSION NOTES:

Dummv Pump:

After Randy meets with Tom to discuss the subject matter tomorrow, he will then respond to AEC's previous request whether the dummy pump shown on Dwg. SK-2-24086, Rev. "0" reflects the as-built condition. AEC is instructed to use the total length and limit a maximum cross sectional dimension of 36" as shown on Dwg. SK-2-24086 for designing and modifying the dummy pump. Existing dummy pump weighs 19,43 5 lbs. per WHC calcs. on 11/28/92 by D.E. Ryman; new dummy pump after modifying wj.ll weigh 25,095 lbs. and the center of gravity to match that shown on 101SY load chart. Randy did not object to AEC's proposal of increasing the new pump weights by filling the pipe sections with water.

Saddles: WHC is still checking the canister rings for structural adequacy; however, he instructed AEC to go ahead to finalize the design AEC submitted earlier.

A-130

DISTRIBUTION: AEC/aOOl-02. LEM, SB, MCC. R. J o r i s s e n (WHO

http://wj.ll

RECOF MEETING TELECON


PAGE A - i $ )

r>ATF- 6 /3 /94

AEC PARTICIPANTS: Lincoln Malik, Mike C.S. Chiao UH< Randy Jorissen (WHC) OTHER PARTICIPANTS:—

PROJECT/SUBJECT" WHC Temporary Pump 2/Dummy Pump

DISCUSSION NOTES:

Dummv Pump:

1. Randy will provide AEC a dimension - distance between the pump end and pivot point as shown on 101SY load chart.

2. AEC will locate center of gravity from the left end of the dummy pump that will match the end location of the actual pump on the cradle when tested; see SK-2-24086, Rev. 0 for dummy pump orientation.

3. Randy will provide actual weight of the concrete-filled pipe segments of the dummy pump to AEC.

,• 4. AEC will check structural integrity of the dummy pump that

will be supported by series of 41" O.D. disks when the pump lays inside the canister; AEC will detail the disks.

5. WHC decided using concrete instead of water to fill in the pipes for adding weights to the pump.

A-131

DISTRIBUTION- AEC/4001-02, LEM, SB, HCC, R. J o r i s s e n (WHC)


RECO MEETIN^ TELECON


PAGE A - [ 32

5 D A T E : — 5 / 2 6 / 9 4 .

AEC PARTICIPANTS:

OTHER PARTICIPANTS:

PROJECT/SUBJECT:—

Mike C.S. Chiao to-fcyt^

Randy Jorissen (WHC)

WHC Temporary Pump 2/Lifting Beams, Saddles P.O. MJB-SWV-322666, Task 322666-002, AEC Job 4001-02

DISCUSSION NOTES:

Lifting Beams: Randy received lifting beam sketches AEC faxed to him yesterday; agreed to single-plate (1-3/4" thick) extension to the underside of top flange of the beam; approved 12" clearance between the bottom of the beam and top of canister rings; AEC requested WHC to verify this dimension on the sketch. Saddles: Randy asked how much of the container being supported in the AEC design; responded that the support is over a 1/4 circle. Test Weights: Test weights include the weight of the holder; design two lifting lugs on the holder - one vertical, other horizontal; the center of the vertical lug is lined up with center of gravity of the holder itself, the horizontal lug is lined up with center of gravity of the holder plus all the weights. However, the vertical lug is still designed for full weights. Dummy Pump: Randy will verify if the dummy pump shown on WHC sketch reflects as-built condition; WHC calcs. showed a conflicting dimension; use dimensions & load shown on 101SY load chart to check and modify the dummy pump.

A-132

DISTRIBUTION: AEC/4001-02, LEM, SB, MCC, R. J o r i s s e n (WHC)


Advanced Engineering PAGE A-133. Consultants 180 Montgomery Street. Suite 850 San Francisco. CA 94104 Telephone: (415)291-9600 Fax: (415)291-9696

August 17 , 1994 wmm Ms. Theresa Peterson Westinghouse Hanford Company P.O. Box 1970, H5-53 Richland, WA 99352 Subject: Hydrogen Mitigation in Tank SY101 - Dummy Pump Weights Dear Ms. Peterson; This letter is to confirm our telephone conversation earlier this afternoon. We understand that WHC wishes to replace the %in 16 UNC2A x %in, A354 Grade BD Hex Cap Screws for the MPA Dummy Pump Removable Discs, shown in drawing H-2-834749, Sh. 1, with Same screws made of A307 Grade material. AEC finds this replacement to be acceptable for this case.

Please call me if you have any questions.

Very truly yours,

Tjincoln E. Malik President LEM:rm

A-133


Appendix B Additional Analysis of Container Test Weight for Tank 241SY101

DESIGN CALCULATION

(1) Drawing ^ 2 - ^ - ? < y ? / r ^ / 7 (2) Doc. No. (4) Building (5) Rev. (7) Subject 77^- oJotfLrfis)t>/WA~.J*..


PAGE B-2 OF B-6

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Date -U- )~ f r t j , Date " ? - / > - 9fr

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PAGE B-3 OF B-6

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ANALYTICAL CALCULATIONS


PAGE B-4 OF B-6

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DESIGN CALCULATION

(1) Drawing /•/ -Z ~S}7^- 3 >*<W (2) Doc. No. (4) Building (5) Rev. (7) Subject Tact <*i4H)Ur $rx (*/ W C^^;**^

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PAGE B-5 OF B-6

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DESIGN CALCULATION

(1) Drawing (+'1, - ? 5 7 ^ / ? ^ , ^ (2) Doc. No.

(4) Building (5) Rev.

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PAGE B-6 OF B-6

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B-6


Appendix C

Additional Analysis of Mock-up Pump Modification for Tank 241SY101

C-l

DESIGN CALCULATION

(1) Drawing H~l-W*%A+*-<> ( 2 ) Doc. No. (4) Building **-2-wnf./**" { 5 ) R e v .

< 7) (8) Originator F"/J UfAr,. •< (9) Checker J. / . •(*£,&*

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PAGE C-2 OF C-12

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DESIGN CALCULATION WHC-SD-WM-DA-168 REV. 0

(1) Drawing / / V - , f » 7 ? J t M Q ) Doc. No. : p A G E ^ ^ c _ i 2

(4) Building (5) Rev. . . (7) Subject ?y LQ\ M.t/kup put*,a 4»^>-». / / , , (8) Originator FV /4.itr...\ ' Date 7 - / 9 - 9 » (9) Checker J . V/. ^ „ Date 7/2.z/?<{

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(4) Building (5) Rev. ( t ,

(7) Subject fy/ol Mot}<. up l?u*»uJ A i r f t W A , ^

PAGE C-4 OF C-12

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BD-6100 060 1 (12/87)

(D Drawing U - j - A S 7 V f, Kew. v (2) Doc. No. p A G £ C 6 Q F Q _ 1 2

(4) Building (5) Rev. ' ( 6 , . . . (7) Subject Sy In \ Made vu /;//*..- y A*~*»*S ^-i -. (8) Originator 7^/4 /Ju*«* Date *7-,q^Cji4

(9) Checker Q , n ? . 7 > , < y A \ Date 7 / ^ / . ] <f

(10)

4 9-ty<f,2 ( < A ? r ) V ^ ~ ^cro.jr f / y ; Va . -f 7 / r ^ « '*./*? 7 1 ) ^ 1 / ^ 2 + / V . / ^ V 1 -

• -+ vy z f 2 -* 7, r -/ / -.jj-f "?/*.£ C //. £7 r ) -t 7 ^ . 3 x </2.-* 3-<s2,r(<*z.v7r-+<'7. ?7 r+ *>•)

-+ 2-yyr.t-t ./W77 •+ S~*r>.l-

? n ? o + 4/*7.r -*- "?*2'2/

T * 4 * ^ OJJ^U p,/- M*tJ<iy> f 5 ^ /

-4 mi* 3 + ?/0.S -+ 74*/.? .4 *V*r <~*3

C-6

BD-6A00-060 I (12/87)

(1) Drawing / / - 2 - ^ * 7 ^ 1 /0?,y. P (2) Doc. No. (4) Building (5) Rev. (6) Job (7) Subject 5V tol Mock vp Y>i+>~*b4***~,lb

PAGE C-7 OF C-12

(8) Originator p/•/ fJttft*tj^ • Date 7 - ^ Z - f ^ (9) Checker / ' );(

(10)

th<f'»^. • Date 7-2/ -<? V-

l^ffX-i' Date n/ijTAZ-

7?4- {e/tOn ir&

- tu3c r> c r - A - h) ~c -]/z - ^ (i-^-b-oYz

•Vx

•M**,s /*tr6(i7M-6' n <>-< 0.4z-f V/z

f7.ifi) + (<fi2,f7r-M*l+f7.W+{Wl-G%y-**fl'.

c-7

BD-6400-060 1 (U/87)

(1) Drawing / / - 1 -f2. 7</- J. &*,.& (2) Doc. No. p A Q E Q Q Q ? Q _ u

(4) Building (5) Rev. , (7) Subject gy/o/ M,*J? Up tu*»»A«»t*k\y (8) Originator j>H UISA»A. Date __-___££_ (9) Checker .\MA'J<TA. Date fa/ftf

(10)

x^xB: r - n<f-sj - iHn.2 -/rbi>47

% = _____2__i___3_ 7 *< 3

- 7 3-37 /"*''

C£ - "3 7^2 X / 2 : •

0. /<.

C-8

BD-6400-060 1 (12/87)

DESIGN CALCULATION

(1) Drawing /J--?-JP ? 7 V fl F> iMTj Doc. No. (4) Building \ (5) Rev. (7) Subject Z..- / / / / . < • LUA -&<* Hoc-k i/pi7u,~&

(6.


PAGE C-9 OF C-12

^ (8) Originator p/i {J,rr.„< (9) Checker

(10)

T Date 9-2,t~$<J Date lf_Z.\fao

J J

Ll r-k«t l-«6 Fey- M2&M UP pu~%.h U i^w

£_*&.6f C4,J*e. /•

— h in r c j » TO'hJ O-J-C'^Uf ASl G*.£>*»~f J i - ^ kilos. /\jtA4/fhcyi

Ul,*.>nt k*id -ft*, b-p/t*^- / « £ , &JL 2-~d era**.

£;X£ Jfa pU-ryxp <&4*>^h -T^U? JsOt*j*r &«jp • 1%<-

XLcw* \ U

\

" \

C-9

BD-6400-060 1 (12/37)

DESIGN CALCULATION

(1) Drawing / l - l - <f ^ 1 ¥ ? , & « , . .7(2) Ooc. No.

(4) Building (5) Rev.


PAGE C-10 OF C-12

(7) Subject U £{-;*,'•, Z ^ * X»^ M<>r.b>ju Du^P

(8) Originator / = # /4uAn* f i# (Man*.

1 J (10) L?a.*l £**««. I :

t<hr>~fr*~l*J Ufo .

Date 7-2./—$ i

Date "7/2./ £?</

y 1

71—G-p*-

- 2 ; ^ > < r ;*»*-

cn = 22.

ylVr<

o.<

C-10

BD-6400-060.1 (12/87)

DESIGN CALCULATION

(1) Drawing ji^j.-^J 'JU £ / p - v o ^ ) Doc. No. (4) Buiiding ' (5) Rev. (7) Subject > - V v v ^ Lue- -A-v Mo<J* up j?«>*p

(6


PAGE C - l l OF C-12

If (8) Originator Pi J- lkta„* (9) Checker .'. V. A-fc-r -yl

(10)

Date ~?-x/~ 4J<.

°lit*»

C - l l

8D-6400-060 1 (12/87)

DESIGN CALCULATION

(1) Drawing IT- ; ~f J7 </<?, &~.Q(2) Doc. No. (4) Building (5) Rev.

WHC-SD-WM-DA-168 REV. 0 •

PAGE C-12 OF C-12

(7) Subject L-lJ-iltA U*e -£-^r\*d? <s/i Au*~(> (8) Originator F/l iiiu e,.<i (9) Checker J M. &£c*-

HO)

Date- J^u rig. Date V l . ' f&

Lead -faZc 2 :

P-/A rx j.^r ~i <r fops

Send'** $-h-&

a . i rK«

# 7 = ^ s ~ * . < • <

Grmbre ? i . ^ / e ^ " - a a a , <5v? Co**&rt£± /nstzie. f>'pe

- 4. r^v*

— 2-* f / *3 —

C-12

£'*«*

0

- ^ *F-2 4 "

BD-6400-060 1 (12/37)

WHC-SD-MM-DA-168 Rev. 0

Appendix D Analysis of Removable Support for the Transport Assembly

D-l

(1) Drawing K ' 2 - £ 3 > ~ 7 5 < (2) Doc. No. (4) Building. (5) Rev. (6 PAGE D-2 (7) Subject TT/-V.J</Vier / - ^ . ' " w W y Pm.n\Jt- +>&.us. SuuVtrAT (8) Originator J, '•/. £ 4 & /3L ' Date "' 'Ao/jJ

(9) Checker { ^ ^ / ^ T ^ ^ Date ^ f l / S . ? ^

(10) O iJ jCCTTv/c"

pump- coHimtitJinL 15 &QIJ<\ tziGVfrr&j]

SflUii -p&tArt tlwTV iT&f/sti. (/rise

D-2 3D-6400-060.1 (12.87)

(1) Drawing / 7 - 2 - , f ? 7 5 5 (4) Building

DESIGN CALCULATION

(2) Doc. No.. (5) Rev.

WHC-SD-WM-DA-16S REV. 0

PAGE D-3

(7) Subject ~reAuJ<fiY7T f4-4.f&u RLS figJMOwAM-s: <?,AA0SS

(8) Originator /, (/ f^^t-^f (9) Checker [tf0?<&/?-Jtf

(10)

Date 4/zs/-?*/ . Date g'frzc. 9<H

5-0

il.tf"'

\WL

4 Cc^TVr.Ocrtl

^ loo i-i_

+ o,OGo53 " 0,1(1'

D-3

BD-6400-060.1 (12/87)

DESIGN CALCULATION - WHC-SD-WM-DA-168 REV. 0

(D Drawing / / - 7 ~ , ? . ? 7 5 Y (2) Doc. No. p A Q E ^ (4) Building ; (5) Rev. (i (7) Subject -TtfsAKJCPrMT feCPfatof'./ f^M^'AXf-£ grtfPMr (8) Originator ,/ , (/- f^^^ D a t e ^AJ/^. (9) Checker x/dfflfV J*"??*^* Date £ £&£. ? ^

(10)

^oTkriMA 6-f 4_ Of CaiorWl'ioC-vC (a) C.t>L,: UAJE 2<J

V*T--Wc<aA crHsfcT 'f 4 of. CwuTM-uoat

u -UZSM. ±M>i(*l^) ~ 2G. - 51.15 H. .

3.3oi°

VG/tnufc r 24,5*V3k -b.$7A$ - 3.5.75"*

D-4

9D--6400-060.1 (12/87)

DESIGN CALCULATION

(1) Drawing / / - 2 - 5 3 7 jf. T (2) Doc. No. (4) Building (5) Rev. (6) J.


PAGE .D-5

'(7) Subject -f(Z/hjJ<Z(e//_r /h£< rz», if <_J fi-Gst* aysPxr ^ ^ / ^ W r (8) Originator , J. {/• C^fy£# (9) Checker ifyptdf/? " 7 ^ ^ -

Date Date

(10)

it

v .

38) - 5 3 o * o ( i i 5 ^ i - j , ^

$ • 3 ;

425.815 V 5

ft

4l 7 i

^ = - M 6^^.?13

^f/3n^-- 25/6

D-5

BD-6400-060 1 (12/87)


(1) Drawing / / - 2 - g 3 7 5 " f (2) Doc. No. p A Q E Q _ 6

(4) Building (5) Rev. (6 (7) Subject 7 7 ^ : A / - / ^ ^ Y - X ^ r v r •-;*>,-:••.//*-.£,y3 S'jfrfs.r (8) Originator . J , \ / . PA/^/** Date °>/fa'IC* , (9) Checker {/dm& A L7Zf^*- Date .C /)fle. ?"^

(10) ifj\v# L*i+s • (j**/S'(//Kc& 7-Bs)

'- 12.5 7 ^

AA - ii rr id * ji rr

^ - A 2.

D-6

BD-6400-060 1 (12/87)

DESIGN CALCULATION

(1) Drawing tf~2-2J~75<> (2) Doc. No. (4) Building (5) Rev. ___ (6.


PAGE D-7

^/v)r (7) Subject TtAust p'rt 7 / f< < ,~A« mr y /n %&v, g/it-KL^ frM/atf (8) Originator , J. (/. t^Ctfi. (9) Checker l/^fa^^7pLa^

Date ^ / I s r /g j / Date i"^ ^ ^

(10) / ^ Y # ZCMt!iO(\ MSA cW 3ff}£LQ{*^ fLAT£

P . F »

<?/JV7 •*- z?/£

« I ^

! 1 - * & )

g ^ ^ U i -- 2! Z,£S%r

D-7

BD-6400-060 1 (12/87)

DESIGN CALCULATION WMC-SD-WM-DA-168 REV. 0

(1) Drawing /t-L-BV-^fS (2) Doc. No. (4) Building (5) Rev. (7) Subject -TVAAA ProLT fc^^KQJ ft1 rSt^iAfw-^, tC So-jfcrAr

(t PAGE D-8

(8) Originator- I l/- l?lC ?A (9) Checker \/j~77t^£S

! Zoffc

Date V z g / ? * / . Date - ^ ~ / b ^ . 94-.

(10)

6 < f e ^ - 144

F ^ "• /r 3G -S" r "WrL" " / * i j c

CLC - /2L<

?~- 1.1[C/f^

tbtSC £.1.)

CMC ^ ?~ no) (4(?c pa S-ilZ

£ - 72^3 " ~ ^ ^ 7 %/^ < 7 2 ^ %>- CK

&oLT gtl's frb-qui*&l>

L4X3

h ' h - 2 ^ 7 ^ + 2 57$'* So%i.

D-8 BD-6400-060.1 (12.87)

DESIGN CALCULATION

(1) Drawing j-f-Z'SS 755 (2) Doc. No.. .(4) Building (5) Rev. (6


PAGE D-9

(7) Subject Tff^^faAr j4sfc/5««tt(>./ f.&MrAfPA-A(jT &>'Jf>A. r (8) Originator (9) Checker {,

J. V- &,£,£* f Date ^flSfa/J f

Date 5 - 2 t e g . ? ^

(10)

/> r \f lii^-i. si (//-ay

CH-ecc %.&JIOHU£, j~m&*s: //o L 4-*$ *% ?

fTTU J U U

4-0/2-

c vP UJ" 2 5"7k

z'-7/"

IXXO

- V * * ^ - ~ — • • • , . , ^ ^ -

I'-oK"

#-; - 1 3 4 . 2 / = r

. n ' - * " T

'i •a.

<u\ , 7_ '

D-9

BO-6400-060 1 (12.87)

(1) Drawing ^-Z-Sjl^lS (4) Building

DESIGN CALCULATION

(2) Doc. No.

(5) Rev. (6


PAGE D-10

(7) Subject -f£rt-fi(< p,MJT_ fe/W/H/ dfiHM/&faL£ ^MfMLT (8) Originator J • \f kef fcl ; Date V ^ / f ^ ,

(9) Checker ~\^^Sf J-TZk^Z- Date <Z~S)J2O. 9 4 -

(10) U) *y

z. s

/,

3

v v \

- Z&.?S7°

*/

1^= r ^ + r ^ - i ^ - 3Wr i-M -6.375"--4.IL, ^

r ...o.J3.4 it) .

- t. XI5/to

~ O.L^^iaJ:

D-IO

BD-6400-060 l (12.87)

http://--4.il

(1) Drawing l4-Z~8>$1 $5 (2) Doc. No. /« » •„• ,« D I P A G E D- l l (4) Building (5) Rev. ( (7) Subject TtfA*)$ f&tr Az<tSU*.itlU K<r#CNatohU? ZtKOffftfC (8) Originator , J - 1/ (Ef^Q&A ; • Date Qjyq/cjlj (9) Checker {/dtM^/f-TZZ^l— Date £ ~ Z)<g». ^ 7 * -

[10) HA^ - 2 2 W £ ^ <*.

AA^ =. 22i5</ *V*><(

Tbfc 4,l(* 6. SIS'

(,5te*/f*f-

Snt&$ frT 6

i •2.OO20 (#-7^J_ ^lUZoO'Zls) r Li

fc& 4,i<> ^,57r - ^

z ^ 1 -

.- -into*//**

Ot L&S rrsiu ) % (~j - /.oo<§)

DMI " "

BD-6400-060 1 (12.87)

DESIGN CALCULATION

(1) Drawing //'2-BS7S5 _ (2) Doc. No.. (4) Building (5) Rev.


PAGE D-12

(7) Subject -TfLtMrttffKT fcCfZuKU/ tCfacNSfaie ZitpQwr f. (8) Originator (9) Checker \J/$JPl& s#~7Zi<sz£-

Date Qh.Cifa.4 . Date j$"T 2>gg. 94—

(10)

«»

$-- 6, 69(4 tti1

ft (0(0 STlfflStAS <?H &*, %Qe^ 6f fiatr-

/

L4<lt% 'lb

*//' STir?*!&*/

£*%& JO>. )fTW)

aA--°'7;r

^

Fb -. o,15 Fl

-- zLi<f£> /to*

1 D-12

BD-6400-060 1 (1.2.87)

(1) Drawing 14~Z"%3 7 < 5 (2) Doc. No. (4) Building (5) Rev.

PAGE D-13

(7) Subject TfftrfiiSPcrJL-T A^<C?AA tiC<J tf T?S« ir./&fr%>L-£ $ i ^ f a f (8) Originator , J • V - & & £ &rn (9) Checker l/tUW&f/? % l ^ -

Date ,&/r2>/£tf Date £ 2>ec. /??4-

(10)

= / d # l #

A«, - * luJ

2-0 7

- 3 25-5" ^

<o

*/• I

Zltl / /AJ

^>z "7T^

u,$c? fa ' FrLutr us-eLe

/ &

D-13 "

8D-6400-060 ! (U 87^

(D Drawing tf'2-6 3 7*5 (2) Doc. No. • p A Q E

(4) Building 1 _ (5) Rev. . . . "(7) Subject TelMJS QaaT (KZC^Kcy &ws<nJ£!AQL£ KtippsnLT (8) Originator . .{, ^-&A 0 ' Pate ^ A ? (9) Checker \J0m?/f7J&&---= Date / £ £»&. /??4~

(10) Clf&CK #mop(*J dMl'V^i- o£.

i*JcnqtfT OP i" PL^n;

Li FT)(a IT) (.& Fr) fa° % 3 ) "' -IMA *

S'fftWL f&l '"&OLT

D-14

BD-6400-060 ! (U.87)

DESIGN CALCULATION WHC-SD-WM-DA-168 REV. 0 .

(1) Drawing l--2~£-l 1^5 (2) Doc. No. ,(4) Building (5) Rev. (6

PAGE D-15

(7) Subject f l ' f t u ^ ^ T t f cs f?»t* KLV {^JTM^M^fj^ Krrttsr$T (8) Originator , . / Cl {LrpX Date W*\/a'J ,

l/g/m/f^^^- — Date '6 U*. ?+L_

WlllOtUA^AA* 0CAJT <SffcVifHi (A-IS^ JS.-S) - i. ?P . d

(9) Checker

(10)

t 7

K,

, ^ 4- a, 573 "

r

L z i.s 4 = i'SC%)~- Liz?" (fifst J3*

2 C^?2)

t,4~- _£H±-c <r.7$LkU

J.o fk- hfi(ss) = 5 ^ / ^ u crfZ

D-15 BO-6400-060.1 (12/87)

(1) Drawing / A ~ ? ~ £ ^ 7 5 T (2) Doc. No. PAGE D-16 i(4) Building (5) Rev. (7) Subject -Tlt/*MJ< OrMT (krtrJuMy f / c ^ b M y f - g C*MsfA.r (8) Originator \ {/ (<CCfal ' Date ^HtofaZ (9) Checker [IfiMMtfTIw^ Date b Dec, /fft

(10) CiHrziC B^Ybeuoc-i tfi-f t*J3axi£((

£ c.ULf^t (ft-isc Kf.sJ

(I- ^151*

•L«j = 6.116 HJ

A / - I'm

£--1% .m

1 j.>

• (' fi-KC KJ.V

+to ' 0' 7'0 it)

£ > * I.IBi M

A/ - / i la \''^7

•(o.1l) \^l + r /<

ie - Lfl.^fa.V) 1 + 3 (3^63 / W

' 6 . 7 ] " ' ^

K jl- 215.U 7 4^.z*7 ft

D-16

BD-6400-060 1 (12/87)

(1) Drawing H - 2 - £ 5 7 ?"5" (4) Building

DESIGN CALCULATION

(2) Doc. No. (5) Rev. «-

WHC-SD-WM-OA-168 REV, 0

PAGE D-17

(7) Subject Ttf/h.AjCPfMT /Uc£>t~t2f.y tferzum/eitxr C ^fMPfiMLT (8) Originator J ,\j. CTCC, frv( (9) Checker \ktH0/rf-/JL*6.

Date iqfrZftjq -A-Date ^ bee. ?4~

(10)

- a

WJ

D-17

BD-6400-060 1 (12/87)

DESIGN CALCULATION

(1) Drawing / ^ " - ' 2 - & 75"5" (2) Doc. No. (4) Building (5) Rev. ^ (6


PAGE D-18

'(7) Subject To+ujieeMT A-SS&*, ALU rf^syi Q\sem ge rviPPwL C (8) Originator V' £<j6fti. (9) Checker {AUPiS//£ ^ ^ A

Date lo/fsfaM _ Date 6 £>eC./??4-

[10)

* af

£>'-]" IS TOO USlOd 72> ASSOUAN (?£/&a*A0L£ I 7 "

% Vv s ~

. » / ' '

£ * 3 t f ^ M + 3(fc)&

±A

- hi23 '*>

( a

i«V^l 4- 3(^fe)(u%-.^J3T l i -

D-18~

8D-6400-060 1 (12/87)

(1) Drawing ^ ~ 7 " 3 ^ ^ (2) Doc. No. p A G E D _ l g

M) Building (5) Rev. (7) Subiect T9*>.<,.f.P0*T A<c.f?MAL\J /s iM.rn* Jut ej£ <;(»ff'MT (8) Originator J. </ f/C^^if Date ' /^//B/a.^ (9) Checker y/tftt>0f/? " T W < £ — Date 6 Pet*. /??#-

do) _ X* 3$A^

Ctu

SiSuioiKj crr&cfss no pLM-nr

% - U X - r . ^-tfc TJ CiT gr,'t ) 1

in/ <s?7<r. V o T c *• ^ * / 7 • • • •

^ - 6,(»P^ £|$£ sez.V0*> ft-2-

- 2 7 P O + \ / ? - -

- 34,!7

*7.n5

D-19~

BD-6400-060 1 (12,37)

(1) Drawing ft-l-$$lrf (2) Doc. No. PAGE D-20 , (4) Building (5) Rev.

(7) Subject T*frv$pir,tJ / k ^ ^ L l / tf &**v\/t&h*,Le ^b\a,fs>»r (8) Originator J_\(. £y*jL Date iV/&/*</ (9) Checker V/Ut&//?'7&<&4- Date £ 7>ef. /???—

(10)

j r _ _ _ ^ ' ! - 4 , 2 ^ 7

ii_ - \> u "

4R r •

^ \ J

v * * » (/HS2F^

D-20

BD-6400-060 I (12 8 7!

(D Drawing ff~l-4 3 7 ^ T (2) Doc. No. p A G E Q _ 2 1

IA) Building ; (5) Rev. ; . . (7) Su bi ect 7V / w C PO*T /U<> d , Al. y f K'MWU* ¥.<.€. Sv\ffeN.T (8) Originator J.V- iZ^CKA Date fp/ftf^ (9) Checker T/diW?//?'7*^ Date £ 2>ed . /994~~

(10)

Chirac UJ£ID zrzt-ss (tfonczc^m. sH^At srxess)

r = 8 4,^2.2.

/\LLcJL^>m6L£ 6O£U0 STRESS,

a, 3 ^ T - F T * 70 %,T-

^"TXtSS ¥><?£ W <^F % " R C L t T

- tf. I 0 f J *J >

z-6>_

D-21

8D 6400-060 : •;•: 37)


Appendix E Analysis of Saddle Modification for Air Pallets

E-l

(1) Drawing A ~ 2 - g 3 7 6 J (4) Building

DESIGN CALCULATION

(2) Doc. No.

(5) Rev. (6;

WHC-SD-WI* REV. 0

PAGE E-2

-DA-168

(7) Subject <'Profit* MnoK/eAr/a** fort Alt ?M-A (8) Originator . / , V. £•££/?#_

(9) Checker _ ^ ^

Date f'/7.°/** Date, £ %e<L. /??f—

(10)

f ZLO&%rK • (/*-*5'&'%t>i-)

g&tcri'*i>s- A-r CM r&u>G*. z'w'p'cnc r Manors

Tirfi cM j r CoornmetL

i SM.

Z&.W*-' ^ . 7 5 - "

S<£€ li-I-31734 YcnL UM-/0S <ZG£ LOW CtfnAr io\S</

e f r + 'k% = f<fz/747

£lAk~- -^oi>c (zq.is) +• 7a<?o^23*0.2r)

+ .( l l%^ Us4ns)(Mlrt*/i.- wis)

+ ( , z 4 * / ^ ( n w ) ^« - } j r -.?T,?S)

E-2

8D-6400-060 1 (U/87)

DESIGN CALCULATION WHOSD-WM-DA-168 REV. 0

(1) Drawing / / ~ 2 - & ? 7 k ? (2) Doc. No. ,^ . • PAGE E-3

(4) Building (5) Rev. (6) J "(7) Subject £fr-f)K>(-€ M\&A(F-< CJ-ICU) fzM AiP pALtj=13 (8) Originator J , l/- iEc^ &/L Date_jVWfj/_ (9) Checker

(10)

+ M, &S,eo O -t- a j 7o 7, ovo ~ lZ& (52.5)

**^ -s& = *«/#?

fAW(fti\/l*i /f££A. OF /hue p/f-LLl^T

75, 051*-?- &€>ob^

/pfi-LUET WO- -_ lZ4* M*-/- &* *•

^l/h^l/ir^^fl - Of AeXs-^O fay Z33-£,*#{ t

Site (*o*<co" x i%" d=r- _ J

use 2, ST-V5"' fad /0*LL<m ^.UKioe*.

V /«^

'r-^(£<^--a£/_iV "'•* E-3

80-6400-060 1 i " : 87)

(1) Drawing /f~ 2 - %?>1 Ll (2) Doc. No. PAGEE-4 (4) Building (5) Rev. (6] ''(7) Subject £A-t)0L& M.ff*f'c)'cfrflcLJ per* At/? fatJ_t-T5 (8) Originator -/rJ/- /F^G&S Date / / A ? / ? ?

[/t0m&/?~77J€^-— Date 6 dec /??4-(9) Checker

(10) QeTEyZMUt* W"<&«JT FOR $0K L0*B

*r Ci^JT^rt Of kz" Sf/PsJ.

t A „ Bo 6 , - L ) . ' / • _ , , , )

fA- — - - — - UYd K-iU.

b

jm-* /OS,** 72 y 5 u>tx<\q s^ ii'itaJ1

5~(zt>i): /oC ,f/to2- ate.

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(1) Drawing / A 2 - £ 3 7 6 3 (2) Doc. No. (4) Building ; (5) Rev. (6!


PAGE E-6

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PAGE E-7

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PAGE E-8

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BD-6400-060 1 (12/87)


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PAGE E - l l

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(1) Drawing ff " 2 - ? ^ l ( o l (2) Doc. No..

(4) Building (5) Rev. d.


PAGE E-14

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8D-6400-060.1 (12/87)

(1) Drawing H"'2~'^3*7'ID 3 (4) Buildinc

DESIGN CALCULATION

(2) Doc. No. (5) Rev.


PAGE E-16

''(7) Subject. S/H?/jt.e- jA,y',Pictrr/jp &M Me P*-LL£T (8) Originator J r V, K ^ F^ _ _ Date U/l.G fa*} (9) Checker

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Date £&»,_ /?74-

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WHC-SD-WM-OA-168 REV. 0

PAGE E-17

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E-17

80-6400-060 1 (12/87)

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(1) Drawing If- 2~ S3 Ik 1 (2) Doc. No. (4) Building (5) Rev. (6) J


PAGE E-18

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8D-6400-060.1 (12.87)

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(1) Dro/ving / - A - 2 - & 3 7 (oZ (2) Doc. No.. (4) Building (5) Rev. (6) J


PAGE E-19

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BO-6400-060 1 (12.87)

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DESIGN CALCULATION WHC-SD-WM-DA-168

(1) Drawing _J£zllllILl (2) Doc. No. p A G £ £ _ 2 1

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(1) Drawing /•/ - 2 ~£ .? 7 £, 3 (2) Doc. No. (4) Building (5) Rev. (6


PAGE E-22

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Date ///i?/W - Date '(, 72^r.. /??<?-

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E-22 BD-6400-060.1 (12/87)

DESIGN CALCULATION WHC-SD-WM-DA-168 KtV. 0

(1) Drawing tf " 2 - ^ 3 7 ^ 3 (2) Doc. No. p A f i E ^ ^

(4) Building (5) Rev. (-, . _ _ _

••(7) Subject <> Ana a US A/IW^t'cJrrtm fay frt( PfiiJL&T*

(8) Oviginator J. t/< tTc^CtA. Date t(/l<jfef

(9) Checker ^ $Jf*u9//?'rf'''J' Date 6 $011^ /??f-~

(10)

Roark's Formulas for Stress and Strain. Sixth Edition

Table 3

— - R W = load

Notation:

W:= 18000-cos( 4 5 . R 180' R

W := o *•

M 0 :=0

9 o : = 0

A o : = 0

T"1 = 0

T 2 = 0

R a :=0

R b := 0

M a := 0

M b := 0

V : = 0

E : = 29000000

| : = 10-1.3753

12

1 = 0

l : - _ 12.75 + 5.25 - .25

X := I + .25 - 6

a := 0

w = load per unit length

M 0 = applied couple

q 0 = angular displacement

A0 = lateral displacement

T-j = temperature on top suface

T2 = temperature on bottom surface

R a = left vertical reaction

Rb = right vertical reaction

M a = left end moment

M D = right end moment

V = shear

E = modulus of elasticity

I = moment of interia

1 - temperature coefficient of expansion

25 - 3.875 I = length of beam

x = lenght from left end of beam

a = x distance from left end

<x-a>n = <D(x-a)(x-a)n

E-23

(1) Drawing / / • " 2 ~ 6 3 7 £ 3 (2) Doc. No. a - j w PAGE E-24

(4) Building (5) Rev. ,

(7) Subject <T/^/)OL(=- /l/l^}^/U^n'oK> F-lg At/ P&LLkTJ

(8) Originator J ' if- ££&&/} Date ///z^/W

(9) Checker ^//$4/&W2*/?~77i#6. Date 6> $?£,. / ^ ^ — (10)

W 4 := 18000-cosj — •%) a ! := 0 1 \180 / . 1

1.f Left end guided, right end simply supported

R a 1 : = 0 M a 1 ( x ) : = W 1 - ( l - a 1 ) 8 a 1 : = 0

'*'" ' \ 6-E-l V —"i • ° i ;

R M W : : W I M b 1 := 0

W 1 fi 2\ ° Vb1 : = 0

1. Concentrated load

Transverse Shear

V 1 ( x ) : = R a 1 - W 1 - * ( x - a 1 ) V ^ x ) =-1.273-10'

Bending Moment

M-,(x) := M g 1 ( x ) + R a 1 - x - W r ( D ( x - a ^ - f x - a-,) M ^ x ) = 7.319-104

Slope

,4

M a 1 ( x ) - x R a 1 - x 2 W r < t > ( x - a 1 ) - ( x - a 1 ) 2

9 i ( x ) = e a 1 + — - - — + — - - -E l 2-E-l 2-E-l

9.,(x) = 0.016 £ r

Deflection

M y i 0 0 : = y a l ( x ) + 9 a 1 - x + — - r — + — - r i

al (*)-><2 R a 1 - x 3 W 1 - Q ( x - a 1 ) - ( x - a 1 ) 3

2-EI 6-E-l 6-E-l y ^ x ) =-0.106

E-24

(1) Drawing M'2'53 7L3 (2) Doc. No. .__ p A Q E £ _ 2 5

(4) Building (5) Rev. (

(7) Subject <Ay>ri(.e- Movn'/^c^ryvo &>*> At fi PhU.eTl (8) Originator J* (/ £&&&?. .Date ll/lln*

(9) Checker [/#&*#? /£~77l&6- Date 6 Astf. /??<?-(10)

W 2 = -28050 a 2 = I + .25 - 6

1.f Left end guided, right end simply supported

R a 2 . = 0 M a 2 ( W 2 ) : = W z ( l - a 2 )

y a 2 (w 2);= — ^ i / r ^ n 2 - ' + 2- a 2-' - a 2)

R b 2 ( W 2 ) : = W 2 M b 2 : = 0

a 2 : = 0

W

2-E-l 1. Concentrated load

b 2 ( W 2 ) : = ^ 2 r ( i 2 - a 2 2 ) y b 2 ; = 0

Transverse Shear

V 2 . ( x . W 2 ) : = R a 2 - W 2 . * ( x - a 2 ) V 2 ( x , W 2 ) = 2.805-104

Bending Moment

M 2 ( x . W 2 ) : = M a 2 ( W 2 ) + R a 2 . x - W 2 - < D ( x - a 2 ) . ( x - a 2 )

M 2 ( x , W 2 ) = -1.6I3-103

Slope

M a 2 ( W 2 ) - x R a 2 x 2 W 2 . 0 ( x - a 2 ) - ( x - a 2 ) 2

9 2 ( x , W 2 ) = 8 a 2 + . E-l 2E-I 2-E-l ~

9 2 ( x , W 2 ) = -0.021

Deflection

x3 f uu \ / « i N « M a 2 ( W 2 > x 2 R a 2 - x 3 W 2-Q(x - a 2 ) - ( x - a 2 ) 3

y 7 ( x , W ? ) := y a -> (W 2 ) + e a 2 - x + > i — + - <-^ '— 2 ^ V a ^ *' a/L 2-EI 6-E-l 6-E-l

y 2 ( x , W 2 ) =0.148

E-25

DESIGN CALCULATIO W H C-SD-WM-DA-168 REV. 0

(1) Drawing H'7~61>1L3 (2) Doc. No. PAGE E-26

(4) Building (5) Rev. v . ,

(7) Subject SAO/)L£ A/1 crtf^'l r/-T!4Q Ft>K Aid PfirLL-CK

(8) Originator J/ I/- &1&C&L " » • - / f

(9) Checker i;fem<&/# 77ic^L. Date **(%<*.(44

Date ^ HOT.. /??<?-

(10)

X := I + .25 - 6 W 2 = -30000 ,-29000 ..20000

0.2

y i(x) o

y2(x.w2)

y i(x)+y2( x 'w2) -o.i

-0.2

-0.3

L20000

-- ---

1 I I

22::::::=^ _0. "*""•--- --

i 1 1 1 - 3 ' 1 0 4 - 2 ' 1 0 4

x : = 0 , . l . . l W 2 : = - 2 0 0 0 0

- 1 M 0 4

W 2

I ' lO 4 2'10 4

0.2

0.1

y'i<*)

y 2(x.W 2) 0

y i (x )+y 2 (x .w 2 )

- 0 . 1 -

-0.2

E-26

(1) Drawing P ^ ' 8 3 1 L.I

(4) Building

DESIGN CALCULATIO

.(2) Doc. No.

, (5) Rev.


PAGE E-27

(J) Subject £prJ)f)L£ M-OV) \&> CAr/pfJ Ft># /hi/ f/-<-L£TZ

JM. £<$r-,e/L (8) Originator

(9) Checker

Date ff/t^/^

Date ££&<. /?&£—

(10)

V ^ U . 2 5 - 6 ) + V 2 ( l + -25 - 6 , W 2 ) '7.272-103 V ^ O ) + V 2 ( 0 , W 2 ) = -1.273-104

M 1 (! 4- .25 - 6) + M 2 ( I + -25 - 6,W 2 ) = -4.18M0 4 M ^ 0 ) + M 2 ( 0 , W 2 ) = 6.16-104

vvf

5M(T -

V l < x ) + V 2 ( x , W 2 )

M , ( x ) + M 2 ( x , W 2 )

—5-104

I I I I I I

\ ....._ I _ .o.

I

I I I I I I 10 12

E-27

(D Drawing H ' l ' ^ l L l (2) Doc. No. p A Q E E _ 2 8

.(4) Building (5) Rev. . . (7) Subject S/h/)»0(.A AAaniCirArirA) &* Alfi SAUETS

(8) Originator J / V, E&&EH Date Ifflfjh^ (9) Checker " ^ ^ ^ 7 ^ ^ Date & $&<L /99&—

(10)

I:

Fb-z o.l5 Fy (ftisc pl.t)

F = 6.15&(.)'- 21 </t*u'i~

P -T.O, U C - 6,04-5

f-\W --V-&T- '•*»

- 0.&7 7 <. ho 0<

E-28

BD-6400-060 1 ; - J87)

rvs.T. T. V^c ,e

Documents

Transcript of rvs.T. T. V^c ,e