Design Calculation Column C1023

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Table of Contents

Cover Sheet ............................................................................................................................................................. 3

Title Page ................................................................................................................................................................ 5

Warnings and Errors : ..................................................................................................................................... 6

Input Echo : ........................................................................................................................................................... 7

XY Coordinate Calculations : .................................................................................................................. 42

Flg Calc [Int P] : New Flange ......................................................................................................... 44

Flg Calc [Int P] : BF-2 ....................................................................................................................... 53



Flg Calc [Int P] : BF-5 ....................................................................................................................... 80

Flg Calc [Int P] : BF-6 ....................................................................................................................... 89

Internal Pressure Calculations : ......................................................................................................... 98

External Pressure Calculations : ....................................................................................................... 121

Element and Detail Weights : ................................................................................................................ 138

Nozzle Flange MAWP : .................................................................................................................................... 147

Natural Frequency Calculation : ......................................................................................................... 148

Wind Load Calculation : ............................................................................................................................ 149

Earthquake Load Calculation : .............................................................................................................. 155

Wind/Earthquake Shear, Bending : ....................................................................................................... 157

Wind Deflection : ........................................................................................................................................... 159

Longitudinal Stress Constants : ......................................................................................................... 162

Longitudinal Allowable Stresses : ..................................................................................................... 164

Longitudinal Stresses Due to . . . : ............................................................................................. 166

Stress due to Combined Loads : ............................................................................................................ 173

Center of Gravity Calculation : ......................................................................................................... 189

Sup. Lug Calcs: Ope : ................................................................................................................................. 190

Nozzle Calcs. : N03 ...................................................................................................................................... 208

Nozzle Calcs. : N04 ...................................................................................................................................... 226



Nozzle Calcs. : LI1 ...................................................................................................................................... 234

Nozzle Calcs. : N02 ...................................................................................................................................... 239

Nozzle Calcs. : LI-2 .................................................................................................................................... 263

Nozzle Calcs. : LG2 ...................................................................................................................................... 269

Nozzle Calcs. : SG2 ...................................................................................................................................... 284

Nozzle Calcs. : N01 ...................................................................................................................................... 299

Nozzle Calcs. : N5 ........................................................................................................................................ 305

Nozzle Schedule : ........................................................................................................................................... 324

Nozzle Summary : ............................................................................................................................................. 327

Vessel Design Summary : ............................................................................................................................ 329



Cover Page

C-1023

OT Distillation Column

DESIGN CALCULATION

In Accordance with ASME Section VIII Division 1

ASME Code Version : 2010 Edition, 2011a Addenda



Cover Page

Job File : C:\DOCUMENTS AND SETTINGS\SAS\MY DOCUMENTS\SK\SA

Date of Analysis : Dec 18,2015

PV Elite 2012, January 2012



Title Page

Note: PV Elite performs all calculations internally in Imperial Units

to remain compliant with the ASME Code and any built in assumptions

in the ASME Code formulas. The customary Imperial database is

used for consistency. The finalized results are reflected to show

the users set of selected units.



C-1023OT Distillation ColumnFileName : C-1023--------------------------------------------

Warnings and Errors : Step: 0 3:23p Dec 18,2015

Class From To : Basic Element Checks.

==========================================================================

Class From To: Check of Additional Element Data

==========================================================================

There were no geometry errors or warnings.

PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2012



C-1023OT Distillation ColumnFileName : C-1023--------------------------------------------Input Echo : Step: 1 3:23p Dec 18,2015

PV Elite Vessel Analysis Program: Input Data

C-1023

OT Distillation Column

Design Internal Pressure (for Hydrotest) 3.0000 bars

Design Internal Temperature 220 C

Type of Hydrotest UG99-b Note [34]

Hydrotest Position Horizontal

Projection of Nozzle from Vessel Top 0.0000 mm.

Projection of Nozzle from Vessel Bottom 0.0000 mm.

Minimum Design Metal Temperature -5 C

Type of Construction Welded

Special Service None

Degree of Radiography RT-2

Miscellaneous Weight Percent 0.0

Use Higher Longitudinal Stresses (Flag) Y

Select t for Internal Pressure (Flag) N

Select t for External Pressure (Flag) N

Select t for Axial Stress (Flag) N

Select Location for Stiff. Rings (Flag) N

Consider Vortex Shedding N

Perform a Corroded Hydrotest N

Is this a Heat Exchanger No

User Defined Hydro. Press. (Used if > 0) 0.0000 bars

User defined MAWP 5.1600 bars

User defined MAPnc 0.0000 bars

Load Case 1 NP+EW+WI+FW+BW




Load Case 2 NP+EW+EE+FS+BS

Load Case 3 NP+OW+WI+FW+BW

Load Case 4 NP+OW+EQ+FS+BS

Load Case 5 NP+HW+HI

Load Case 6 NP+HW+HE

Load Case 7 IP+OW+WI+FW+BW

Load Case 8 IP+OW+EQ+FS+BS

Load Case 9 EP+OW+WI+FW+BW

Load Case 10 EP+OW+EQ+FS+BS

Load Case 11 HP+HW+HI

Load Case 12 HP+HW+HE

Load Case 13 IP+WE+EW

Load Case 14 IP+WF+CW

Load Case 15 IP+VO+OW

Load Case 16 IP+VE+EW

Load Case 17 NP+VO+OW

Load Case 18 FS+BS+IP+OW

Load Case 19 FS+BS+EP+OW

Wind Design Code IS-875

Basic Wind Speed for IS-875 170.00 Km/hr

Wind Zone Number 4

Base Elevation 300.00 mm.

Percent Wind for Hydrotest 33.0

Risk Factor 1.0

Terrain Category 3

Equipment Class 1

Topography Factor 1.0

Damping Factor (Beta) for Wind (Ope) 0.0100

Damping Factor (Beta) for Wind (Empty) 0.0000




Damping Factor (Beta) for Wind (Filled) 0.0000

Seismic Design Code IS-1893-SCM

Importance Factor for IS-1893 1.000

Soil Factor 1.300

Zone Number 3.000

Percent Seismic for Hydrotest 10.000

Design Nozzle for Des. Press. + St. Head Y

Consider MAP New and Cold in Noz. Design N

Consider External Loads for Nozzle Des. Y

Use ASME VIII-1 Appendix 1-9 N

Material Database Year Current w/Addenda or Code Year

Configuration Directives:

Do not use Nozzle MDMT Interpretation VIII-1 01-37 No

Use Table G instead of exact equation for "A" Yes

Shell Head Joints are Tapered Yes

Compute "K" in corroded condition Yes

Use Code Case 2286 No

Use the MAWP to compute the MDMT Yes

Using Metric Material Databases, ASME II D No

Complete Listing of Vessel Elements and Details:

Element From Node 10

Element To Node 20

Element Type Elliptical




Description Bottom Dish

Distance "FROM" to "TO" 50.000 mm.

Inside Diameter 1000.0 mm.

Element Thickness 10.000 mm.

Internal Corrosion Allowance 0.0000 mm.

Nominal Thickness 12.000 mm.

External Corrosion Allowance 0.0000 mm.

Design Internal Pressure 3.0000 bars

Design Temperature Internal Pressure 220 C

Design External Pressure 1.0346 bars

Design Temperature External Pressure 220 C

Effective Diameter Multiplier 1.2

Material Name SA-240 316L

Allowable Stress, Ambient 115.10 N./mm²

Allowable Stress, Operating 106.50 N./mm²

Allowable Stress, Hydrotest 149.70 N./mm²

Material Density 0.008027 kg./cm³

P Number Thickness 0.0000 mm.

Yield Stress, Operating 118.50 N./mm²

External Pressure Chart Name HA-4

UNS Number S31603

Product Form Plate

Efficiency, Longitudinal Seam 1.0

Efficiency, Circumferential Seam 1.0

Elliptical Head Factor 2.0


Detail Type Insulation

Detail ID Ins: 80

Dist. from "FROM" Node / Offset dist -250.00 mm.




Height/Length of Insulation 300.00 mm.

Thickness of Insulation 160.00 mm.

Density 0.0001100 kg./cm³


Detail Type Nozzle

Detail ID N03

Dist. from "FROM" Node / Offset dist 1.0000 mm.

Nozzle Diameter 200.0 mm

Nozzle Schedule 10S

Nozzle Class 150

Layout Angle 0.0

Blind Flange (Y/N) N

Weight of Nozzle ( Used if > 0 ) 0.0000 Kgf

Grade of Attached Flange GR 2.2

Nozzle Matl SA-312 TP316


Detail Type Nozzle

Detail ID N04



Nozzle Schedule 10S

Nozzle Class 150

Layout Angle 0.0








--------------------------------------------------------------------


Element To Node 30

Element Type Cylinder

Description Shell-1

















Detail ID Ins: 80









Detail Type Nozzle

Detail ID LI1



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 180.0





--------------------------------------------------------------------


Element To Node 40


Description Shell-2



















Detail Type Packing

Detail ID Pack:[1 of 1]


Height of Packed Section 0.0000 mm.


Percent Volume Holdup 0.0

Specific Gravity of Packing Liquid 0.0



Detail ID Ins: 80






Detail Type Nozzle

Detail ID N02



Nozzle Schedule STD

Nozzle Class 150

Layout Angle 0.0









Detail Type Nozzle

Detail ID LI-2



Nozzle Schedule 80S

Nozzle Class 150

Layout Angle 180.0





--------------------------------------------------------------------


Element To Node 50

Element Type Flange

Description BF-1


Flange Inside Diameter 1000.0 mm.













Material Name SA-182 F316L








UNS Number S31603

Class / Thickness / Grade :: > 5

Product Form Forgings

Perform Flange Stress Calculation (Y/N) Y

Weight of ANSI B16.5/B16.47 Flange 0.0000 Kgf

Class of ANSI B16.5/B16.47 Flange

Grade of ANSI B16.5/B16.47 Flange



Detail ID Ins: 80





--------------------------------------------------------------------





Element To Node 60

Element Type Flange

Description BF-2












Material Name SA-182 F316L







Detail ID Ins: 80





--------------------------------------------------------------------





Element To Node 70


Description Shell-3




















UNS Number S31603

Product Form Plate




Detail Type Packing










Detail Type Packing

Detail ID Mellapack-2








Detail ID Ins: 80






Detail Type Lug

Detail ID SUPPORT LUG


Number of Lugs 4

Dist. from OD to Lug Cntrline(dlug) 300.00 mm.

Height of Gusset Plates (hgp) 252.00 mm.




Force Bearing Width (wfb) 125.00 mm.

Weight of Lug 35.000 Kgf

Lug Start Angle (degrees) 0.0

--------------------------------------------------------------------


Element To Node 90


Description Shell-5
















Detail Type Packing












Detail ID Ins: 80





--------------------------------------------------------------------


Element To Node 100


Description Shell-6



























Detail Type Packing









Detail ID Ins: 80






Detail Type Nozzle




Detail ID LG2



Nozzle Schedule 10S

Nozzle Class 150

Layout Angle 0.0






Detail Type Nozzle

Detail ID SG2



Nozzle Schedule 10S

Nozzle Class 150

Layout Angle 135.0





--------------------------------------------------------------------


Element To Node 120


Description Shell-8




















Detail ID Ins: 80





--------------------------------------------------------------------


Element To Node 130

Element Type Flange

Description BF-3






















Detail ID Ins: 80





--------------------------------------------------------------------


Element To Node 140

Element Type Flange

Description BF-4






















Detail ID Ins: 80





--------------------------------------------------------------------


Element To Node 150





Description Shell-9
















Detail Type Packing









Detail ID Ins: 80








--------------------------------------------------------------------


Element To Node 160


Description Shell-10
















Detail Type Packing












Detail ID Ins: 80





--------------------------------------------------------------------


Element To Node 170





















Detail Type Packing









Detail ID Ins: 80





--------------------------------------------------------------------


Element To Node 180





















Detail Type Packing









Detail ID Ins: 80





--------------------------------------------------------------------





Element To Node 190


















Detail Type Packing









Detail ID Ins: 80








--------------------------------------------------------------------


Element To Node 200



















Detail ID Ins: 80









Detail Type Nozzle

Detail ID N01



Nozzle Schedule 40S

Nozzle Class 150

Layout Angle 0.0





--------------------------------------------------------------------


Element To Node 210

Element Type Flange

Description BF-5






















Detail ID Ins: 80





--------------------------------------------------------------------


Element To Node 220

Element Type Flange

Description BF-6






















Detail ID Ins: 80





--------------------------------------------------------------------


Element To Node 230






















Detail ID Ins: 80





--------------------------------------------------------------------


Element To Node 240

Element Type Elliptical

Description Top Dish


















Elliptical Head Factor 2.0



Detail ID Ins: 80






Detail Type Nozzle

Detail ID N5



Nozzle Schedule 10S

Nozzle Class 150

Layout Angle 0.0







C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------XY Coordinate Calculations : Step: 2 3:23p Dec 18,2015

XY Coordinate Calculations

| | | | | |

From| To | X (Horiz.)| Y (Vert.) |DX (Horiz.)| DY (Vert.) |

| | mm. | mm. | mm. | mm. |

--------------------------------------------------------------

Bottom Dis| ... | 50.0000 | ... | 50.0000 |

Shell-1| ... | 1550.00 | ... | 1500.00 |

Shell-2| ... | 2825.00 | ... | 1275.00 |

BF-1| ... | 2970.00 | ... | 145.000 |

BF-2| ... | 3115.00 | ... | 145.000 |

Shell-3| ... | 4470.00 | ... | 1355.00 |

Shell-4| ... | 5970.00 | ... | 1500.00 |

Shell-5| ... | 7470.00 | ... | 1500.00 |

Shell-6| ... | 8970.00 | ... | 1500.00 |

Shell-7| ... | 10220.0 | ... | 1250.00 |

Shell-8| ... | 10720.0 | ... | 500.000 |

BF-3| ... | 10865.0 | ... | 145.000 |

BF-4| ... | 11010.0 | ... | 145.000 |

Shell-9| ... | 12510.0 | ... | 1500.00 |

Shell-10| ... | 14010.0 | ... | 1500.00 |

Shell-11| ... | 15510.0 | ... | 1500.00 |

Shell-12| ... | 17010.0 | ... | 1500.00 |

Shell-13| ... | 18510.0 | ... | 1500.00 |

Shell-14| ... | 19220.0 | ... | 710.000 |

BF-5| ... | 19365.0 | ... | 145.000 |

BF-6| ... | 19510.0 | ... | 145.000 |

Shell-15| ... | 19810.0 | ... | 300.000 |

Top Dish| ... | 19860.0 | ... | 50.0000 |



C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------XY Coordinate Calculations : Step: 2 3:23p Dec 18,2015




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Flg Calc [Int P] : New Flange Flng: 7 3:23p Dec 18,2015

Flange Input Data Values Description: New Flange :

BF-1

Description of Flange Geometry (Type) Integral Weld Neck

Design Pressure P 3.00 bars

Design Temperature 220 C

Internal Corrosion Allowance ci 0.0000 mm.

External Corrosion Allowance ce 0.0000 mm.

Use Corrosion Allowance in Thickness Calcs. No

Flange Inside Diameter B 1000.000 mm.

Flange Outside Diameter A 1200.000 mm.

Flange Thickness t 70.0000 mm.

Thickness of Hub at Small End go 10.0000 mm.

Thickness of Hub at Large End g1 30.0000 mm.

Length of Hub h 75.0000 mm.

Flange Material SA-182 F316L

Flange Material UNS number S31603

Flange Allowable Stress At Temperature Sfo 106.50 N./mm²

Flange Allowable Stress At Ambient Sfa 115.10 N./mm²

Bolt Material SA-193 B7

Bolt Allowable Stress At Temperature Sb 172.38 N./mm²

Bolt Allowable Stress At Ambient Sa 172.38 N./mm²

Diameter of Bolt Circle C 1140.000 mm.

Nominal Bolt Diameter dB 24.0000 mm.

Type of Threads TEMA Metric




Number of Bolts 44

Flange Face Outside Diameter Fod 1065.000 mm.

Flange Face Inside Diameter Fid 1000.000 mm.

Flange Facing Sketch 1, Code Sketch 1a

Gasket Outside Diameter Go 1065.000 mm.

Gasket Inside Diameter Gi 1000.000 mm.

Gasket Factor m 3.0000

Gasket Design Seating Stress y 68.95 N./mm²

Column for Gasket Seating 2, Code Column II

Gasket Thickness tg 3.0000 mm.

ASME Code, Section VIII, Division 1, 2010, 2011a

Hub Small End Required Thickness due to Internal Pressure:

= (P*(D/2+Ca))/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*(1000.0000/2+0.0000))/(106.50*1.00-0.6*3.00)+Ca

= 1.4109 mm.

Hub Small End Hub MAWP:

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50 * 1.00 * 10.0000 )/(500.0000 + 0.6 * 10.0000 )

= 21.046 bars

Corroded Flange ID, Bcor = B+2*Fcor 1000.000 mm.

Corroded Large Hub, g1Cor = g1-ci 30.000 mm.

Corroded Small Hub, g0Cor = go-ci 10.000 mm.

Code R Dimension, R = (C-B)/2 - g1 40.000 mm.




Gasket Contact Width, N = (Go - Gi) / 2 32.500 mm.

Basic Gasket Width, bo = N / 2 16.250 mm.

Effective Gasket Width, b = Cb sqrt(bo) 10.158 mm.

Gasket Reaction Diameter, G = Go - 2 * b 1044.684 mm.

Basic Flange and Bolt Loads:

Hydrostatic End Load due to Pressure [H]:

= 0.785 * G² * Peq

= 0.785 * 1044.6837² * 3.000

= 26222.697 Kgf

Contact Load on Gasket Surfaces [Hp]:

= 2 * b * Pi * G * m * P

= 2 * 10.1581 * 3.1416 * 1044.6837 * 3.0000 * 3.00

= 6119.520 Kgf

Hydrostatic End Load at Flange ID [Hd]:

= Pi * Bcor² * P / 4

= 3.1416 * 1000.0000² *3.0000/4

= 24027.451 Kgf

Pressure Force on Flange Face [Ht]:

= H - Hd

= 26222 - 24027

= 2195.245 Kgf

Operating Bolt Load [Wm1]:

= max( H + Hp + H'p, 0 )

= max( 26222 + 6119 + 0 , 0 )

= 32342.219 Kgf

Gasket Seating Bolt Load [Wm2]:

= y * b * Pi * G + yPart * bPart * lp




= 68.95*10.1581*3.141*1044.684+0.00*0.0000*0.00

= 234389.141 Kgf

Required Bolt Area [Am]:

= Maximum of Wm1/Sb, Wm2/Sa

= Maximum of 32342/172 , 234389/172

= 133.350 cm²

ASME Maximum Circumferential Spacing between Bolts per App. 2 eq. (3) [Bsmax]:

= 2a + 6t/(m + 0.5)

= 2 * 24.000 + 6 * 70.000/(3.00 + 0.5)

= 168.000 mm.

Actual Circumferential Bolt Spacing [Bs]:

= C * sin( pi / n ) )

= 1140.000 * sin( 3.142/44 )

= 81.327 mm.

ASME Moment Multiplier for Bolt Spacing per App. 2 eq. (7) [Bsc]:

= max( sqrt( Bs/( 2a + t )), 1 )

= max( sqrt( 81.327/( 2 * 24.000 + 70.000 )), 1 )

= 1.0000

Bolting Information for TEMA Metric Thread Series (Non Mandatory):

-----------------------------------------------------------------------------

Minimum Actual Maximum

-----------------------------------------------------------------------------

Bolt Area, cm² 133.350 137.609

Radial distance bet. hub and bolts 36.510 40.000

Radial distance bet. bolts and the edge 28.580 30.000

Circumferential spacing between bolts 58.740 81.327 168.000




-----------------------------------------------------------------------------

Min. Gasket Contact Width (Brownell Young) [Not an ASME Calc] [Nmin]:

= Ab * Sa/( y * Pi * (Go + Gi) )

= 137.609 * 172.38/(68.95 * 3.14 * (1065.000 + 1000.00 ) )

= 5.303 mm.

Note: Recommended Min. Width for Sheet and Composite Gaskets per table 2-4 :

= 32.000 mm.

Flange Design Bolt Load, Gasket Seating [W]:

= Sa * Ab

= 172.38 * 137.6091

= 241876.05 Kgf

Gasket Load for the Operating Condition [HG]:

= Wm1 - H

= 32342 - 26222

= 6119.52 Kgf

Moment Arm Calculations:

Distance to Gasket Load Reaction [hg]:

= (C - G ) / 2

= ( 1140.0000 - 1044.6837 )/2

= 47.6581 mm.

Distance to Face Pressure Reaction [ht]:

= ( R + g1 + hg ) / 2

= ( 40.0000 + 30.0000 + 47.6581 )/2

= 58.8291 mm.

Distance to End Pressure Reaction [hd]:

= R + ( g1 / 2 )




= 40.0000 + ( 30.0000/2.0 )

= 55.0000 mm.

Summary of Moments for Internal Pressure:

Loading Force Distance Bolt Corr Moment

End Pressure, Md 24027. 55.0000 1.0000 1322. Kg-m.

Face Pressure, Mt 2195. 58.8291 1.0000 129. Kg-m.

Gasket Load, Mg 6120. 47.6581 1.0000 292. Kg-m.

Gasket Seating, Matm 241876. 47.6581 1.0000 11528. Kg-m.

Total Moment for Operation, Mop 1742. Kg-m.

Total Moment for Gasket seating, Matm 11528. Kg-m.

Effective Hub Length, ho = sqrt(Bcor*goCor) 100.000 mm.

Hub Ratio, h/h0 = HL / H0 0.750

Thickness Ratio, g1/g0 = (g1Cor/goCor) 3.000

Flange Factors for Integral Flange:

Factor F per 2-7.2 0.745

Factor V per 2-7.3 0.108

Factor f per 2-7.6 1.505

Factors from Figure 2-7.1 K = 1.200

T = 1.839 U = 11.813

Y = 10.750 Z = 5.545

d = .10972E+07 mm.³ e = 0.0074 mm.^-1

Stress Factors ALPHA = 1.521

BETA = 1.695 GAMMA = 0.827

DELTA = 0.313 Lamda = 1.140

Longitudinal Hub Stress, Operating [SHo]:




= ( f * Mop / Bcor ) / ( L * g1² )

= (1.5049*1742/1000.0000)/(1.1400*30.0000²)

= 25.06 N./mm²

Longitudinal Hub Stress, Seating [SHa]:

= ( f * Matm / Bcor ) / ( L * g1² )

= (1.5049*11527/1000.0000)/(1.1400*30.0000²)

= 165.81 N./mm²

Radial Flange Stress, Operating [SRo]:

= ( Beta * Mop / Bcor ) / ( L * t² )

= (1.6953*1742/1000.0000)/(1.1400*70.0000²)

= 5.19 N./mm²

Radial Flange Stress, Seating [SRa]:

= ( Beta * Matm/Bcor ) / ( L * t² )

= (1.6953*11527/1000.0000)/(1.1400*70.0000²)

= 34.31 N./mm²

Tangential Flange Stress, Operating [STo]:

= ( Y * Mo / (t² * Bcor) ) - Z * SRo

= (10.7496*1742/(70.0000²*1000.0000))-5.5455*5

= 8.73 N./mm²

Tangential Flange Stress, Seating [STa]:

= ( y * Matm / (t² * Bcor) ) - Z * SRa

= (10.7496*11527/(70.0000²*1000.0000))-5.5455*34

= 57.74 N./mm²

Average Flange Stress, Operating [SAo]:

= ( SHo + max( SRo, STo ) ) / 2

= (25+max(5,8))/2

= 16.89 N./mm²




Average Flange Stress, Seating [SAa]:

= ( SHa + max( SRa, STa ) ) / 2

= (165+max(34,57))/2

= 111.78 N./mm²

Bolt Stress, Operating [BSo]:

= ( Wm1 / Ab )

= (32342/137.6091)

= 23.05 N./mm²

Bolt Stress, Seating [BSa]:

= ( Wm2 / Ab )

= (234389/137.6091)

= 167.04 N./mm²

Stress Computation Results: Operating Gasket Seating

Actual Allowed Actual Allowed

Longitudinal Hub 25. 160. 166. 173. N./mm²

Radial Flange 5. 106. 34. 115. N./mm²

Tangential Flange 9. 106. 58. 115. N./mm²

Maximum Average 17. 106. 112. 115. N./mm²

Bolting 23. 172. 167. 172. N./mm²

Minimum Required Flange Thickness 67.361 mm.

Estimated M.A.W.P. ( Operating ) 18.9 bars

Estimated Finished Weight of Flange at given Thk. 232.8 kg.

Estimated Unfinished Weight of Forging at given Thk 402.2 kg.

Flange Rigidity Based on Required Thickness [ASME]:

Flange Rigidity Index, Seating (rotation check) per APP. 2 [Js]:



C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Flg Calc [Int P] : BF-2 Flng: 8 3:23p Dec 18,2015

Flange Input Data Values Description: BF-2 :

BF-2













Flange Material SA-182 F316L













Number of Bolts 44












= (P*(D/2+Ca))/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*(1000.0000/2+0.0000))/(106.50*1.00-0.6*3.00)+Ca

= 1.4109 mm.


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50 * 1.00 * 10.0000 )/(500.0000 + 0.6 * 10.0000 )

= 21.046 bars














= 0.785 * G² * Peq

= 0.785 * 1050.4807² * 3.000

= 26514.527 Kgf


= 2 * b * Pi * G * m * P

= 2 * 9.7596 * 3.1416 * 1050.4807 * 3.0000 * 3.00

= 5912.070 Kgf


= Pi * Bcor² * P / 4

= 3.1416 * 1000.0000² *3.0000/4

= 24027.451 Kgf


= H - Hd

= 26514 - 24027

= 2487.076 Kgf


= max( H + Hp + H'p, 0 )

= max( 26514 + 5912 + 0 , 0 )

= 32426.598 Kgf






= 68.95*9.7596*3.141*1050.481+0.00*0.0000*0.00

= 226443.453 Kgf



= Maximum of 32426/172 , 226443/172

= 128.829 cm²


= 2a + 6t/(m + 0.5)

= 2 * 24.000 + 6 * 70.000/(3.00 + 0.5)

= 168.000 mm.


= C * sin( pi / n ) )

= 1140.000 * sin( 3.142/44 )

= 81.327 mm.


= max( sqrt( Bs/( 2a + t )), 1 )

= max( sqrt( 81.327/( 2 * 24.000 + 70.000 )), 1 )

= 1.0000


-----------------------------------------------------------------------------


-----------------------------------------------------------------------------

Bolt Area, cm² 128.829 137.609







-----------------------------------------------------------------------------


= Ab * Sa/( y * Pi * (Go + Gi) )

= 137.609 * 172.38/(68.95 * 3.14 * (1070.000 + 1010.00 ) )

= 5.265 mm.


= 32.000 mm.[Note: Exceeds actual gasket width, 30.000 ]


= Sa * Ab

= 172.38 * 137.6091

= 241876.05 Kgf


= Wm1 - H

= 32426 - 26514

= 5912.07 Kgf



= (C - G ) / 2

= ( 1140.0000 - 1050.4807 )/2

= 44.7596 mm.


= ( R + g1 + hg ) / 2

= ( 40.0000 + 30.0000 + 44.7596 )/2

= 57.3798 mm.


= R + ( g1 / 2 )




= 40.0000 + ( 30.0000/2.0 )

= 55.0000 mm.

















T = 1.839 U = 11.813

Y = 10.750 Z = 5.545

d = .10972E+07 mm.³ e = 0.0074 mm.^-1


BETA = 1.695 GAMMA = 0.827

DELTA = 0.313 Lamda = 1.140





= ( f * Mop / Bcor ) / ( L * g1² )

= (1.5049*1728/1000.0000)/(1.1400*30.0000²)

= 24.87 N./mm²


= ( f * Matm / Bcor ) / ( L * g1² )

= (1.5049*10826/1000.0000)/(1.1400*30.0000²)

= 155.73 N./mm²


= ( Beta * Mop / Bcor ) / ( L * t² )

= (1.6953*1728/1000.0000)/(1.1400*70.0000²)

= 5.15 N./mm²



= (1.6953*10826/1000.0000)/(1.1400*70.0000²)

= 32.22 N./mm²


= ( Y * Mo / (t² * Bcor) ) - Z * SRo

= (10.7496*1728/(70.0000²*1000.0000))-5.5455*5

= 8.66 N./mm²


= ( y * Matm / (t² * Bcor) ) - Z * SRa

= (10.7496*10826/(70.0000²*1000.0000))-5.5455*32

= 54.23 N./mm²


= ( SHo + max( SRo, STo ) ) / 2

= (24+max(5,8))/2

= 16.76 N./mm²





= ( SHa + max( SRa, STa ) ) / 2

= (155+max(32,54))/2

= 104.98 N./mm²


= ( Wm1 / Ab )

= (32426/137.6091)

= 23.11 N./mm²


= ( Wm2 / Ab )

= (226443/137.6091)

= 161.38 N./mm²







Bolting 23. 172. 161. 172. N./mm²











BF-3













Flange Material SA-240 316L













Number of Bolts 44












= (P*(D/2+Ca))/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*(1000.0000/2+0.0000))/(106.50*1.00-0.6*3.00)+Ca

= 1.4109 mm.


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50 * 1.00 * 10.0000 )/(500.0000 + 0.6 * 10.0000 )

= 21.046 bars








= 68.95*9.7596*3.141*1050.481+0.00*0.0000*0.00

= 226443.453 Kgf



= Maximum of 32426/172 , 226443/172

= 128.829 cm²


= 2a + 6t/(m + 0.5)

= 2 * 24.000 + 6 * 70.000/(3.00 + 0.5)

= 168.000 mm.


= C * sin( pi / n ) )

= 1140.000 * sin( 3.142/44 )

= 81.327 mm.


= max( sqrt( Bs/( 2a + t )), 1 )

= max( sqrt( 81.327/( 2 * 24.000 + 70.000 )), 1 )

= 1.0000


-----------------------------------------------------------------------------


-----------------------------------------------------------------------------

Bolt Area, cm² 128.829 137.609







-----------------------------------------------------------------------------


= Ab * Sa/( y * Pi * (Go + Gi) )

= 137.609 * 172.38/(68.95 * 3.14 * (1070.000 + 1010.00 ) )

= 5.265 mm.




= Sa * Ab

= 172.38 * 137.6091

= 241876.05 Kgf


= Wm1 - H

= 32426 - 26514

= 5912.07 Kgf



= (C - G ) / 2

= ( 1140.0000 - 1050.4807 )/2

= 44.7596 mm.


= ( R + g1 + hg ) / 2

= ( 40.0000 + 30.0000 + 44.7596 )/2

= 57.3798 mm.


= R + ( g1 / 2 )




= 40.0000 + ( 30.0000/2.0 )

= 55.0000 mm.

















T = 1.839 U = 11.813

Y = 10.750 Z = 5.545

d = .10972E+07 mm.³ e = 0.0074 mm.^-1


BETA = 1.695 GAMMA = 0.827

DELTA = 0.313 Lamda = 1.140





= ( f * Mop / Bcor ) / ( L * g1² )

= (1.5049*1728/1000.0000)/(1.1400*30.0000²)

= 24.87 N./mm²


= ( f * Matm / Bcor ) / ( L * g1² )

= (1.5049*10826/1000.0000)/(1.1400*30.0000²)

= 155.73 N./mm²


= ( Beta * Mop / Bcor ) / ( L * t² )

= (1.6953*1728/1000.0000)/(1.1400*70.0000²)

= 5.15 N./mm²



= (1.6953*10826/1000.0000)/(1.1400*70.0000²)

= 32.22 N./mm²


= ( Y * Mo / (t² * Bcor) ) - Z * SRo

= (10.7496*1728/(70.0000²*1000.0000))-5.5455*5

= 8.66 N./mm²


= ( y * Matm / (t² * Bcor) ) - Z * SRa

= (10.7496*10826/(70.0000²*1000.0000))-5.5455*32

= 54.23 N./mm²


= ( SHo + max( SRo, STo ) ) / 2

= (24+max(5,8))/2

= 16.76 N./mm²




= 52.14 * Ma / Bsc * Cnv_fac * V / ( Lambda * Eamb * go 2 * ho * Ki )

= 52.14 * 10826.5/1.0000 * 9806.636 * 0.108/( 1.028 * 195128 *

10.000 2 * 100.000 * 0.300 )

= 0.990 (should be <= 1)

Flange Rigidity Index Operating (rotation check) per APP. 2 [J]:

= 52.14 * Mo / Bsc * Cnv_fac * V / ( Lambda * Eop * goc 2 * ho * Ki )

= 52.14 * 1728.9/1.0000 * 9806.636 * 0.108/( 1.028 * 181063

* 10.000 2 * 100.000 * 0.300 )

= 0.170 (should be <= 1)

Flange Rigidity Based on Given Thickness [ASME]:



= 52.14 * 10826.5/1.0000 * 9806.636 * 0.108/( 1.140 * 195128 *

10.000 2 * 100.000 * 0.300 )

= 0.893 (should be <= 1)



= 52.14 * 1728.9/1.0000 * 9806.636 * 0.108/( 1.140 * 181063

* 10.000 2 * 100.000 * 0.300 )

= 0.154 (should be <= 1)






BF-4


























Number of Bolts 44












= (P*(D/2+Ca))/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*(1000.0000/2+0.0000))/(106.50*1.00-0.6*3.00)+Ca

= 1.4109 mm.


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50 * 1.00 * 10.0000 )/(500.0000 + 0.6 * 10.0000 )

= 21.046 bars














= 0.785 * G² * Peq

= 0.785 * 1050.4807² * 3.000

= 26514.527 Kgf


= 2 * b * Pi * G * m * P

= 2 * 9.7596 * 3.1416 * 1050.4807 * 3.0000 * 3.00

= 5912.070 Kgf


= Pi * Bcor² * P / 4

= 3.1416 * 1000.0000² *3.0000/4

= 24027.451 Kgf


= H - Hd

= 26514 - 24027

= 2487.076 Kgf


= max( H + Hp + H'p, 0 )

= max( 26514 + 5912 + 0 , 0 )

= 32426.598 Kgf






= 68.95*9.7596*3.141*1050.481+0.00*0.0000*0.00

= 226443.453 Kgf



= Maximum of 32426/172 , 226443/172

= 128.829 cm²


= 2a + 6t/(m + 0.5)

= 2 * 24.000 + 6 * 70.000/(3.00 + 0.5)

= 168.000 mm.


= C * sin( pi / n ) )

= 1140.000 * sin( 3.142/44 )

= 81.327 mm.


= max( sqrt( Bs/( 2a + t )), 1 )

= max( sqrt( 81.327/( 2 * 24.000 + 70.000 )), 1 )

= 1.0000


-----------------------------------------------------------------------------


-----------------------------------------------------------------------------

Bolt Area, cm² 128.829 137.609







-----------------------------------------------------------------------------


= Ab * Sa/( y * Pi * (Go + Gi) )

= 137.609 * 172.38/(68.95 * 3.14 * (1070.000 + 1010.00 ) )

= 5.265 mm.




= Sa * Ab

= 172.38 * 137.6091

= 241876.05 Kgf


= Wm1 - H

= 32426 - 26514

= 5912.07 Kgf



= (C - G ) / 2

= ( 1140.0000 - 1050.4807 )/2

= 44.7596 mm.


= ( R + g1 + hg ) / 2

= ( 40.0000 + 30.0000 + 44.7596 )/2

= 57.3798 mm.


= R + ( g1 / 2 )




= 40.0000 + ( 30.0000/2.0 )

= 55.0000 mm.

















T = 1.839 U = 11.813

Y = 10.750 Z = 5.545

d = .10972E+07 mm.³ e = 0.0074 mm.^-1


BETA = 1.695 GAMMA = 0.827

DELTA = 0.313 Lamda = 1.140





= ( f * Mop / Bcor ) / ( L * g1² )

= (1.5049*1728/1000.0000)/(1.1400*30.0000²)

= 24.87 N./mm²


= ( f * Matm / Bcor ) / ( L * g1² )

= (1.5049*10826/1000.0000)/(1.1400*30.0000²)

= 155.73 N./mm²


= ( Beta * Mop / Bcor ) / ( L * t² )

= (1.6953*1728/1000.0000)/(1.1400*70.0000²)

= 5.15 N./mm²



= (1.6953*10826/1000.0000)/(1.1400*70.0000²)

= 32.22 N./mm²


= ( Y * Mo / (t² * Bcor) ) - Z * SRo

= (10.7496*1728/(70.0000²*1000.0000))-5.5455*5

= 8.66 N./mm²


= ( y * Matm / (t² * Bcor) ) - Z * SRa

= (10.7496*10826/(70.0000²*1000.0000))-5.5455*32

= 54.23 N./mm²


= ( SHo + max( SRo, STo ) ) / 2

= (24+max(5,8))/2

= 16.76 N./mm²





= ( SHa + max( SRa, STa ) ) / 2

= (155+max(32,54))/2

= 104.98 N./mm²


= ( Wm1 / Ab )

= (32426/137.6091)

= 23.11 N./mm²


= ( Wm2 / Ab )

= (226443/137.6091)

= 161.38 N./mm²







Bolting 23. 172. 161. 172. N./mm²











= 52.14 * 10826.5/1.0000 * 9806.636 * 0.108/( 1.028 * 195128 *

10.000 2 * 100.000 * 0.300 )

= 0.990 (should be <= 1)



= 52.14 * 1728.9/1.0000 * 9806.636 * 0.108/( 1.028 * 181063

* 10.000 2 * 100.000 * 0.300 )

= 0.170 (should be <= 1)




= 52.14 * 10826.5/1.0000 * 9806.636 * 0.108/( 1.140 * 195128 *

10.000 2 * 100.000 * 0.300 )

= 0.893 (should be <= 1)



= 52.14 * 1728.9/1.0000 * 9806.636 * 0.108/( 1.140 * 181063

* 10.000 2 * 100.000 * 0.300 )

= 0.154 (should be <= 1)






BF-5


























Number of Bolts 44












= (P*(D/2+Ca))/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*(1000.0000/2+0.0000))/(106.52*1.00-0.6*3.00)+Ca

= 1.4107 mm.


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.52 * 1.00 * 10.0000 )/(500.0000 + 0.6 * 10.0000 )

= 21.049 bars








= 68.95*10.1581*3.141*1044.684+0.00*0.0000*0.00

= 234389.141 Kgf



= Maximum of 32342/172 , 234389/172

= 133.350 cm²


= 2a + 6t/(m + 0.5)

= 2 * 24.000 + 6 * 70.000/(3.00 + 0.5)

= 168.000 mm.


= C * sin( pi / n ) )

= 1140.000 * sin( 3.142/44 )

= 81.327 mm.


= max( sqrt( Bs/( 2a + t )), 1 )

= max( sqrt( 81.327/( 2 * 24.000 + 70.000 )), 1 )

= 1.0000


-----------------------------------------------------------------------------


-----------------------------------------------------------------------------

Bolt Area, cm² 133.350 137.609







-----------------------------------------------------------------------------


= Ab * Sa/( y * Pi * (Go + Gi) )

= 137.609 * 172.38/(68.95 * 3.14 * (1065.000 + 1000.00 ) )

= 5.303 mm.


= 32.000 mm.


= Sa * ( Am + Ab ) / 2

= 172.38 * ( 133.3497 + 137.6091 )/2

= 238132.59 Kgf


= Wm1 - H

= 32342 - 26222

= 6119.52 Kgf



= (C - G ) / 2

= ( 1140.0000 - 1044.6837 )/2

= 47.6581 mm.


= ( R + g1 + hg ) / 2

= ( 40.0000 + 30.0000 + 47.6581 )/2

= 58.8291 mm.


= R + ( g1 / 2 )




= 40.0000 + ( 30.0000/2.0 )

= 55.0000 mm.

















T = 1.839 U = 11.813

Y = 10.750 Z = 5.545

d = .10972E+07 mm.³ e = 0.0074 mm.^-1


BETA = 1.695 GAMMA = 0.827

DELTA = 0.313 Lamda = 1.140





= ( f * Mop / Bcor ) / ( L * g1² )

= (1.5049*1742/1000.0000)/(1.1400*30.0000²)

= 25.06 N./mm²


= ( f * Matm / Bcor ) / ( L * g1² )

= (1.5049*11349/1000.0000)/(1.1400*30.0000²)

= 163.25 N./mm²


= ( Beta * Mop / Bcor ) / ( L * t² )

= (1.6953*1742/1000.0000)/(1.1400*70.0000²)

= 5.19 N./mm²



= (1.6953*11349/1000.0000)/(1.1400*70.0000²)

= 33.78 N./mm²


= ( Y * Mo / (t² * Bcor) ) - Z * SRo

= (10.7496*1742/(70.0000²*1000.0000))-5.5455*5

= 8.73 N./mm²


= ( y * Matm / (t² * Bcor) ) - Z * SRa

= (10.7496*11349/(70.0000²*1000.0000))-5.5455*33

= 56.85 N./mm²


= ( SHo + max( SRo, STo ) ) / 2

= (25+max(5,8))/2

= 16.89 N./mm²





= 52.14 * 11349.2/1.0000 * 9806.636 * 0.108/( 1.078 * 195128 *

10.000 2 * 100.000 * 0.300 )

= 0.990 (should be <= 1)



= 52.14 * 1742.3/1.0000 * 9806.636 * 0.108/( 1.078 * 181063

* 10.000 2 * 100.000 * 0.300 )

= 0.164 (should be <= 1)




= 52.14 * 11349.2/1.0000 * 9806.636 * 0.108/( 1.140 * 195128 *

10.000 2 * 100.000 * 0.300 )

= 0.936 (should be <= 1)



= 52.14 * 1742.3/1.0000 * 9806.636 * 0.108/( 1.140 * 181063

* 10.000 2 * 100.000 * 0.300 )

= 0.155 (should be <= 1)






BF-6


























Number of Bolts 44












= (P*(D/2+Ca))/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*(1000.0000/2+0.0000))/(106.52*1.00-0.6*3.00)+Ca

= 1.4107 mm.


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.52 * 1.00 * 10.0000 )/(500.0000 + 0.6 * 10.0000 )

= 21.049 bars














= 0.785 * G² * Peq

= 0.785 * 1044.6837² * 3.000

= 26222.697 Kgf


= 2 * b * Pi * G * m * P

= 2 * 10.1581 * 3.1416 * 1044.6837 * 3.0000 * 3.00

= 6119.520 Kgf


= Pi * Bcor² * P / 4

= 3.1416 * 1000.0000² *3.0000/4

= 24027.451 Kgf


= H - Hd

= 26222 - 24027

= 2195.245 Kgf


= max( H + Hp + H'p, 0 )

= max( 26222 + 6119 + 0 , 0 )

= 32342.219 Kgf






= 68.95*10.1581*3.141*1044.684+0.00*0.0000*0.00

= 234389.141 Kgf



= Maximum of 32342/172 , 234389/172

= 133.350 cm²


= 2a + 6t/(m + 0.5)

= 2 * 24.000 + 6 * 70.000/(3.00 + 0.5)

= 168.000 mm.


= C * sin( pi / n ) )

= 1140.000 * sin( 3.142/44 )

= 81.327 mm.


= max( sqrt( Bs/( 2a + t )), 1 )

= max( sqrt( 81.327/( 2 * 24.000 + 70.000 )), 1 )

= 1.0000


-----------------------------------------------------------------------------


-----------------------------------------------------------------------------

Bolt Area, cm² 133.350 137.609







-----------------------------------------------------------------------------


= Ab * Sa/( y * Pi * (Go + Gi) )

= 137.609 * 172.38/(68.95 * 3.14 * (1065.000 + 1000.00 ) )

= 5.303 mm.


= 32.000 mm.


= Sa * Ab

= 172.38 * 137.6091

= 241876.05 Kgf


= Wm1 - H

= 32342 - 26222

= 6119.52 Kgf



= (C - G ) / 2

= ( 1140.0000 - 1044.6837 )/2

= 47.6581 mm.


= ( R + g1 + hg ) / 2

= ( 40.0000 + 30.0000 + 47.6581 )/2

= 58.8291 mm.


= R + ( g1 / 2 )




= 40.0000 + ( 30.0000/2.0 )

= 55.0000 mm.

















T = 1.839 U = 11.813

Y = 10.750 Z = 5.545

d = .10972E+07 mm.³ e = 0.0074 mm.^-1


BETA = 1.695 GAMMA = 0.827

DELTA = 0.313 Lamda = 1.140





= ( f * Mop / Bcor ) / ( L * g1² )

= (1.5049*1742/1000.0000)/(1.1400*30.0000²)

= 25.06 N./mm²


= ( f * Matm / Bcor ) / ( L * g1² )

= (1.5049*11527/1000.0000)/(1.1400*30.0000²)

= 165.81 N./mm²


= ( Beta * Mop / Bcor ) / ( L * t² )

= (1.6953*1742/1000.0000)/(1.1400*70.0000²)

= 5.19 N./mm²



= (1.6953*11527/1000.0000)/(1.1400*70.0000²)

= 34.31 N./mm²


= ( Y * Mo / (t² * Bcor) ) - Z * SRo

= (10.7496*1742/(70.0000²*1000.0000))-5.5455*5

= 8.73 N./mm²


= ( y * Matm / (t² * Bcor) ) - Z * SRa

= (10.7496*11527/(70.0000²*1000.0000))-5.5455*34

= 57.74 N./mm²


= ( SHo + max( SRo, STo ) ) / 2

= (25+max(5,8))/2

= 16.89 N./mm²





= ( SHa + max( SRa, STa ) ) / 2

= (165+max(34,57))/2

= 111.78 N./mm²


= ( Wm1 / Ab )

= (32342/137.6091)

= 23.05 N./mm²


= ( Wm2 / Ab )

= (234389/137.6091)

= 167.04 N./mm²







Bolting 23. 172. 167. 172. N./mm²









C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Internal Pressure Calculations : Step: 9 3:23p Dec 18,2015

Element Thickness, Pressure, Diameter and Allowable Stress :

| | Int. Press | Nominal | Total Corr| Element | Allowable |

From| To | + Liq. Hd | Thickness | Allowance | Diameter | Stress(SE)|

| | bars | mm. | mm. | mm. | N./mm² |

---------------------------------------------------------------------------

Bottom Dis| 3.0000 | 12.000 | ... | 1000.0 | 106.50 |

Shell-1| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-2| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

BF-1| 3.0000 | 65.000 | ... | 1000.0 | 106.50 |

BF-2| 3.0000 | 65.000 | ... | 1000.0 | 106.50 |

Shell-3| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-4| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-5| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-6| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-7| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-8| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

BF-3| 3.0000 | 6.0000 | ... | 1000.0 | 106.50 |

BF-4| 3.0000 | 6.0000 | ... | 1000.0 | 106.50 |

Shell-9| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-10| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-11| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-12| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-13| 3.0000 | 10.000 | ... | 1000.0 | 106.50 |

Shell-14| 3.0000 | 10.000 | ... | 1000.0 | 106.52 |

BF-5| 3.0000 | 6.0000 | ... | 1000.0 | 106.52 |

BF-6| 3.0000 | 6.0000 | ... | 1000.0 | 106.52 |

Shell-15| 3.0000 | 10.000 | ... | 1000.0 | 106.52 |

Top Dish| 3.0000 | 12.000 | ... | 1000.0 | 106.52 |




Element Required Thickness and MAWP :

| | Design | M.A.W.P. | M.A.P. | Minimum | Required |

From| To | Pressure | Corroded | New & Cold | Thickness | Thickness |

| | bars | bars | bars | mm. | mm. |

----------------------------------------------------------------------------

Bottom Dis| 3.00000 | 21.2563 | 22.9727 | 10.0000 | 1.50000 |

Shell-1| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-2| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

BF-1| 3.00000 | 18.9112 | 20.4384 | 70.0000 | 67.3608 |

BF-2| 3.00000 | 19.0581 | 20.5976 | 70.0000 | 63.1190 |

Shell-3| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-4| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-5| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-6| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-7| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-8| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

BF-3| 3.00000 | 19.0581 | 20.5976 | 70.0000 | 63.1190 |

BF-4| 3.00000 | 19.0581 | 20.5976 | 70.0000 | 63.1190 |

Shell-9| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-10| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-11| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-12| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-13| 3.00000 | 21.0462 | 22.7457 | 10.0000 | 1.50000 |

Shell-14| 3.00000 | 21.0494 | 22.7549 | 10.0000 | 1.50000 |

BF-5| 3.00000 | 18.9140 | 20.4466 | 70.0000 | 66.2940 |

BF-6| 3.00000 | 18.9140 | 20.4466 | 70.0000 | 67.3354 |

Shell-15| 3.00000 | 21.0494 | 22.7549 | 10.0000 | 1.50000 |

Top Dish| 3.00000 | 21.2595 | 22.9820 | 10.0000 | 1.50000 |




1

= (2*S*E*t)/(K*D+0.2*t) per Appendix 1-4 (c)

= (2*115.10*1.00*10.0000)/(1.000*1000.0000+0.2*10.0000)

= 22.973 bars

Actual stress at given pressure and thickness, corroded [Sact]:

= (P*(Kcor*D+0.2*t))/(2*E*t)

= (3.000*(1.000*1000.0000+0.2*10.0000))/(2*1.00*10.0000)

= 15.031 N./mm²

Straight Flange Required Thickness:

= (P*R)/(S*E-0.6*P) + c per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)+0.000

= 1.411 mm.

Straight Flange Maximum Allowable Working Pressure:

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50 * 1.00 * 12.0000 )/(500.0000 + 0.6 * 12.0000 )

= 25.196 bars

Percent Elongation per UHA-44 (75*tnom/Rf)*(1-Rf/Ro) 5.114 %

Note: Please Check Requirements of Table UHA-44 for Elongation limits.

Cylindrical Shell From 20 To 30 SA-240 316L at 220 C

Shell-1

Material UNS Number: S31603

Required Thickness due to Internal Pressure [tr]:

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)




1


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.

Note: The thickness required was less than the Code Minimum, therefore

the Code Minimum value of 1.5000 mm. per UG-16 will be used.

Max. Allowable Working Pressure at given Thickness, corroded [MAWP]:

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars

Maximum Allowable Pressure, New and Cold [MAPNC]:

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.746 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²




Shell-3




1



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.746 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²







1

Shell-4



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.746 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²






1


Shell-5



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.746 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²





1



Shell-6



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.746 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²




1




Shell-7



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.746 bars


= (P*(R+0.6*t))/(E*t)




1

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²




Shell-8



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.746 bars




1


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²




Shell-9



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)




1

= 22.746 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²




Shell-10



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars





1

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.746 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²




Shell-11



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars




1

= (106.50*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.046 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.10*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.746 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²




Shell-13



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.50*1.00-0.6*3.000)

= 1.4109 + 0.0000 = 1.4109 mm.






1



= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.52*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.049 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.15*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.755 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²




Shell-15



= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.000*500.0000)/(106.52*1.00-0.6*3.000)

= 1.4107 + 0.0000 = 1.4107 mm.




1




= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.52*1.00*10.0000)/(500.0000+0.6*10.0000)

= 21.049 bars


= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (115.15*1.00*10.0000)/(500.0000+0.6*10.0000)

= 22.755 bars


= (P*(R+0.6*t))/(E*t)

= (3.000*(500.0000+0.6*10.0000))/(1.00*10.0000)

= 15.181 N./mm²



Elliptical Head From 230 To 240 SA-240 316L at 220 C

Top Dish



= (P*D*Kcor)/(2*S*E-0.2*P) Appendix 1-4(c)




1

= (3.000*1000.0000*1.000)/(2*106.52*1.00-0.2*3.000)

= 1.4087 + 0.0000 = 1.4087 mm.




= (2*S*E*t)/(Kcor*D+0.2*t) per Appendix 1-4 (c)

= (2*106.52*1.00*10.0000)/(1.000*1000.0000+0.2*10.0000)

= 21.259 bars


= (2*S*E*t)/(K*D+0.2*t) per Appendix 1-4 (c)

= (2*115.15*1.00*10.0000)/(1.000*1000.0000+0.2*10.0000)

= 22.982 bars


= (P*(Kcor*D+0.2*t))/(2*E*t)

= (3.000*(1.000*1000.0000+0.2*10.0000))/(2*1.00*10.0000)

= 15.031 N./mm²

Straight Flange Required Thickness:

= (P*R)/(S*E-0.6*P) + c per UG-27 (c)(1)

= (3.000*500.0000)/(106.52*1.00-0.6*3.000)+0.000

= 1.411 mm.

Straight Flange Maximum Allowable Working Pressure:

= (S*E*t)/(R+0.6*t) per UG-27 (c)(1)

= (106.52 * 1.00 * 12.0000 )/(500.0000 + 0.6 * 12.0000 )

= 25.200 bars




1



Hydrostatic Test Pressure Results:

Pressure per UG99b = 1.3 * M.A.W.P. * Sa/S 7.086 bars

Pressure per UG99b[34] = 1.3 * Design Pres * Sa/S 4.120 bars

Pressure per UG99c = 1.3 * M.A.P. - Head(Hyd) 24.700 bars

Pressure per UG100 = 1.1 * M.A.W.P. * Sa/S 5.996 bars

Pressure per PED = 1.43 * MAWP 7.379 bars

UG-99(b) Note 34, Test Pressure Calculation:

= Test Factor * Design Pressure * Stress Ratio

= 1.3 * 3.000 * 1.056

= 4.120 bars

Horizontal Test performed per: UG-99b (Note 34)

Please note that Nozzle, Shell, Head, Flange, etc MAWPs are all considered

when determining the hydrotest pressure for those test types that are based

on the MAWP of the vessel.

Stresses on Elements due to Hydrostatic Test Pressure:

From To Stress Allowable Ratio Pressure

Bottom Dish 21.1 149.7 0.141 4.22

Shell-1 21.3 149.7 0.143 4.22

Shell-2 21.3 149.7 0.143 4.22

Shell-3 21.3 149.7 0.143 4.22




1

Shell-4 21.3 149.7 0.143 4.22

Shell-5 21.3 149.7 0.143 4.22

Shell-6 21.3 149.7 0.143 4.22

Shell-7 21.3 149.7 0.143 4.22

Shell-8 21.3 149.7 0.143 4.22

Shell-9 21.3 149.7 0.143 4.22

Shell-10 21.3 149.7 0.143 4.22

Shell-11 21.3 149.7 0.143 4.22

Shell-12 21.3 149.7 0.143 4.22

Shell-13 21.3 149.7 0.143 4.22

Shell-14 21.3 149.7 0.143 4.22

Shell-15 21.3 149.7 0.143 4.22

Top Dish 21.1 149.7 0.141 4.22

Elements Suitable for Internal Pressure.




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------External Pressure Calculations : Step: 10 3:23p Dec 18,2015

1

External Pressure Calculation Results :


Elliptical Head From 10 to 20 Ext. Chart: HA-4 at 220 C

Bottom Dish

Elastic Modulus from Chart: HA-4 at 220 C : 0.180E+09 KPa.

Results for Maximum Allowable External Pressure (MAEP):

Tca OD D/t Factor A B

10.000 1020.00 102.00 0.0013617 46.36

EMAP = B/(K0*D/t) = 46.3585/(0.9000 *102.0000 ) = 5.0496 bars

Results for Required Thickness (Tca):


2.783 1020.00 366.57 0.0003789 34.14

EMAP = B/(K0*D/t) = 34.1369/(0.9000 *366.5715 ) = 1.0347 bars

Check the requirements of UG-33(a)(1) using P = 1.67 * External Design

pressure for this head.




= (1.728*1000.0000*1.000)/(2*106.50*1.00-0.2*1.728)

= 0.8113 + 0.0000 = 0.8113 mm.




1


= ((2*S*E*t)/(Kcor*D+0.2*t))/1.67 per Appendix 1-4 (c)

= ((2*106.50*1.00*10.0000)/(1.000*1000.0000+0.2*10.0000))/1.67

= 12.728 bars

Maximum Allowable External Pressure [MAEP]:

= min( MAEP, MAWP )

= min( 5.05 , 12.7283 )

= 5.050 bars

Thickness requirements per UG-33(a)(1) do not govern the required

thickness of this head.

Cylindrical Shell From 20 to 30 Ext. Chart: HA-4 at 220 C

Shell-1



Tca OD SLEN D/t L/D Factor A B

10.000 1020.00 2908.33 102.00 2.8513 0.0004271 35.91

EMAP = (4*B)/(3*(D/t)) = (4*35.9119 )/(3*102.0000 ) = 4.6941 bars



5.278 1020.00 2908.33 193.24 2.8513 0.0001664 15.00

EMAP = (4*B)/(3*(D/t)) = (4*14.9953 )/(3*193.2384 ) = 1.0346 bars




1

Results for Maximum Stiffened Length (Slen):


10.000 1020.00 63890.88 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-2




10.000 1020.00 2908.33 102.00 2.8513 0.0004271 35.91

EMAP = (4*B)/(3*(D/t)) = (4*35.9119 )/(3*102.0000 ) = 4.6941 bars



5.278 1020.00 2908.33 193.24 2.8513 0.0001664 15.00

EMAP = (4*B)/(3*(D/t)) = (4*14.9953 )/(3*193.2384 ) = 1.0346 bars



10.000 1020.00 63890.88 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-3




1




10.000 1020.00 7605.00 102.00 7.4559 0.0001496 13.48

EMAP = (4*B)/(3*(D/t)) = (4*13.4792 )/(3*102.0000 ) = 1.7619 bars



8.050 1020.00 7605.00 126.71 7.4559 0.0001091 9.83

EMAP = (4*B)/(3*(D/t)) = (4*9.8327 )/(3*126.7071 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-4




10.000 1020.00 7605.00 102.00 7.4559 0.0001496 13.48

EMAP = (4*B)/(3*(D/t)) = (4*13.4792 )/(3*102.0000 ) = 1.7619 bars






1

8.050 1020.00 7605.00 126.71 7.4559 0.0001091 9.83

EMAP = (4*B)/(3*(D/t)) = (4*9.8327 )/(3*126.7071 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-5




10.000 1020.00 7605.00 102.00 7.4559 0.0001496 13.48

EMAP = (4*B)/(3*(D/t)) = (4*13.4792 )/(3*102.0000 ) = 1.7619 bars



8.050 1020.00 7605.00 126.71 7.4559 0.0001091 9.83

EMAP = (4*B)/(3*(D/t)) = (4*9.8327 )/(3*126.7071 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars





1

Shell-6




10.000 1020.00 7605.00 102.00 7.4559 0.0001496 13.48

EMAP = (4*B)/(3*(D/t)) = (4*13.4792 )/(3*102.0000 ) = 1.7619 bars



8.050 1020.00 7605.00 126.71 7.4559 0.0001091 9.83

EMAP = (4*B)/(3*(D/t)) = (4*9.8327 )/(3*126.7071 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-7




10.000 1020.00 7605.00 102.00 7.4559 0.0001496 13.48

EMAP = (4*B)/(3*(D/t)) = (4*13.4792 )/(3*102.0000 ) = 1.7619 bars




1



8.050 1020.00 7605.00 126.71 7.4559 0.0001091 9.83

EMAP = (4*B)/(3*(D/t)) = (4*9.8327 )/(3*126.7071 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-8




10.000 1020.00 7605.00 102.00 7.4559 0.0001496 13.48

EMAP = (4*B)/(3*(D/t)) = (4*13.4792 )/(3*102.0000 ) = 1.7619 bars



8.050 1020.00 7605.00 126.71 7.4559 0.0001091 9.83

EMAP = (4*B)/(3*(D/t)) = (4*9.8327 )/(3*126.7071 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58




1

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-9




10.000 1020.00 8210.00 102.00 8.0490 0.0001379 12.42

EMAP = (4*B)/(3*(D/t)) = (4*12.4235 )/(3*102.0000 ) = 1.6239 bars



8.322 1020.00 8210.00 122.57 8.0490 0.0001056 9.51

EMAP = (4*B)/(3*(D/t)) = (4*9.5115 )/(3*122.5698 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-10






1


10.000 1020.00 8210.00 102.00 8.0490 0.0001379 12.42

EMAP = (4*B)/(3*(D/t)) = (4*12.4235 )/(3*102.0000 ) = 1.6239 bars



8.322 1020.00 8210.00 122.57 8.0490 0.0001056 9.51

EMAP = (4*B)/(3*(D/t)) = (4*9.5115 )/(3*122.5698 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-11




10.000 1020.00 8210.00 102.00 8.0490 0.0001379 12.42

EMAP = (4*B)/(3*(D/t)) = (4*12.4235 )/(3*102.0000 ) = 1.6239 bars



8.322 1020.00 8210.00 122.57 8.0490 0.0001056 9.51

EMAP = (4*B)/(3*(D/t)) = (4*9.5115 )/(3*122.5698 ) = 1.0346 bars




1



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-12




10.000 1020.00 8210.00 102.00 8.0490 0.0001379 12.42

EMAP = (4*B)/(3*(D/t)) = (4*12.4235 )/(3*102.0000 ) = 1.6239 bars



8.322 1020.00 8210.00 122.57 8.0490 0.0001056 9.51

EMAP = (4*B)/(3*(D/t)) = (4*9.5115 )/(3*122.5698 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-13




1




10.000 1020.00 8210.00 102.00 8.0490 0.0001379 12.42

EMAP = (4*B)/(3*(D/t)) = (4*12.4235 )/(3*102.0000 ) = 1.6239 bars



8.322 1020.00 8210.00 122.57 8.0490 0.0001056 9.51

EMAP = (4*B)/(3*(D/t)) = (4*9.5115 )/(3*122.5698 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-14




10.000 1020.00 8210.00 102.00 8.0490 0.0001379 12.42

EMAP = (4*B)/(3*(D/t)) = (4*12.4235 )/(3*102.0000 ) = 1.6239 bars






1

8.322 1020.00 8210.00 122.57 8.0490 0.0001056 9.51

EMAP = (4*B)/(3*(D/t)) = (4*9.5115 )/(3*122.5698 ) = 1.0346 bars



10.000 1020.00 ******** 102.00 50.0000 0.0001063 9.58

EMAP = (4*B)/(3*(D/t)) = (4*9.5757 )/(3*102.0000 ) = 1.2516 bars


Shell-15




10.000 1020.00 433.33 102.00 0.4248 0.0033097 53.73

EMAP = (4*B)/(3*(D/t)) = (4*53.7252 )/(3*102.0000 ) = 7.0225 bars



2.389 1020.00 433.33 427.01 0.4248 0.0003678 33.14

EMAP = (4*B)/(3*(D/t)) = (4*33.1369 )/(3*427.0106 ) = 1.0346 bars



10.000 1020.00 8787.03 102.00 8.6147 0.0001320 11.89

EMAP = (4*B)/(3*(D/t)) = (4*11.8923 )/(3*102.0000 ) = 1.5545 bars

Elliptical Head From 230 to 240 Ext. Chart: HA-4 at 220 C




1

Top Dish




10.000 1020.00 102.00 0.0013617 46.36

EMAP = B/(K0*D/t) = 46.3585/(0.9000 *102.0000 ) = 5.0496 bars



2.783 1020.00 366.57 0.0003789 34.14

EMAP = B/(K0*D/t) = 34.1369/(0.9000 *366.5715 ) = 1.0347 bars

Check the requirements of UG-33(a)(1) using P = 1.67 * External Design

pressure for this head.




= (1.728*1000.0000*1.000)/(2*106.52*1.00-0.2*1.728)

= 0.8112 + 0.0000 = 0.8112 mm.


= ((2*S*E*t)/(Kcor*D+0.2*t))/1.67 per Appendix 1-4 (c)

= ((2*106.52*1.00*10.0000)/(1.000*1000.0000+0.2*10.0000))/1.67

= 12.730 bars




1

Maximum Allowable External Pressure [MAEP]:

= min( MAEP, MAWP )

= min( 5.05 , 12.7302 )

= 5.050 bars

Thickness requirements per UG-33(a)(1) do not govern the required

thickness of this head.

External Pressure Calculations

| | Section | Outside | Corroded | Factor | Factor |

From| To | Length | Diameter | Thickness | A | B |

| | mm. | mm. | mm. | | N./mm² |

---------------------------------------------------------------------------

10| 20| No Calc | 1020.00 | 10.0000 | 0.0013617 | 46.3585 |

20| 30| 2908.33 | 1020.00 | 10.0000 | 0.00042710 | 35.9119 |

30| 40| 2908.33 | 1020.00 | 10.0000 | 0.00042710 | 35.9119 |

40| 50| No Calc | ... | 70.0000 | No Calc | No Calc |


60| 70| 7605.00 | 1020.00 | 10.0000 | 0.00014961 | 13.4792 |

70| 80| 7605.00 | 1020.00 | 10.0000 | 0.00014961 | 13.4792 |

80| 90| 7605.00 | 1020.00 | 10.0000 | 0.00014961 | 13.4792 |

90| 100| 7605.00 | 1020.00 | 10.0000 | 0.00014961 | 13.4792 |

100| 110| 7605.00 | 1020.00 | 10.0000 | 0.00014961 | 13.4792 |

110| 120| 7605.00 | 1020.00 | 10.0000 | 0.00014961 | 13.4792 |



140| 150| 8210.00 | 1020.00 | 10.0000 | 0.00013789 | 12.4235 |

150| 160| 8210.00 | 1020.00 | 10.0000 | 0.00013789 | 12.4235 |

160| 170| 8210.00 | 1020.00 | 10.0000 | 0.00013789 | 12.4235 |




1

170| 180| 8210.00 | 1020.00 | 10.0000 | 0.00013789 | 12.4235 |

180| 190| 8210.00 | 1020.00 | 10.0000 | 0.00013789 | 12.4235 |

190| 200| 8210.00 | 1020.00 | 10.0000 | 0.00013789 | 12.4235 |



220| 230| 433.333 | 1020.00 | 10.0000 | 0.0033097 | 53.7252 |

230| 240| No Calc | 1020.00 | 10.0000 | 0.0013617 | 46.3585 |


| | External | External | External | External |

From| To | Actual T. | Required T.|Des. Press. | M.A.W.P. |

| | mm. | mm. | bars | bars |

----------------------------------------------------------------

10| 20| 10.0000 | 2.78254 | 1.03458 | 5.04965 |

20| 30| 10.0000 | 5.27845 | 1.03458 | 4.69409 |

30| 40| 10.0000 | 5.27845 | 1.03458 | 4.69409 |

40| 50| 70.0000 | 67.3608 | 1.03458 | No Calc |

50| 60| 70.0000 | 63.1190 | 1.03458 | No Calc |

60| 70| 10.0000 | 8.05006 | 1.03458 | 1.76188 |

70| 80| 10.0000 | 8.05006 | 1.03458 | 1.76188 |

80| 90| 10.0000 | 8.05006 | 1.03458 | 1.76188 |

90| 100| 10.0000 | 8.05006 | 1.03458 | 1.76188 |

100| 110| 10.0000 | 8.05006 | 1.03458 | 1.76188 |

110| 120| 10.0000 | 8.05006 | 1.03458 | 1.76188 |

120| 130| 70.0000 | 63.1190 | 1.03458 | No Calc |

130| 140| 70.0000 | 63.1190 | 1.03458 | No Calc |

140| 150| 10.0000 | 8.32179 | 1.03458 | 1.62389 |

150| 160| 10.0000 | 8.32179 | 1.03458 | 1.62389 |

160| 170| 10.0000 | 8.32179 | 1.03458 | 1.62389 |




1

170| 180| 10.0000 | 8.32179 | 1.03458 | 1.62389 |

180| 190| 10.0000 | 8.32179 | 1.03458 | 1.62389 |

190| 200| 10.0000 | 8.32179 | 1.03458 | 1.62389 |

200| 210| 70.0000 | 66.2940 | 1.03458 | No Calc |

210| 220| 70.0000 | 67.3354 | 1.03458 | No Calc |

220| 230| 10.0000 | 2.38870 | 1.03458 | 7.02249 |

230| 240| 10.0000 | 2.78254 | 1.03458 | 5.04965 |

Minimum 1.624


| | Actual Len.| Allow. Len.| Ring Inertia | Ring Inertia |

From| To | Bet. Stiff.| Bet. Stiff.| Required | Available |

| | mm. | mm. | cm**4 | cm**4 |

-------------------------------------------------------------------

10| 20| No Calc | No Calc | No Calc | No Calc |

20| 30| 2908.33 | 63890.9 | No Calc | No Calc |

30| 40| 2908.33 | 63890.9 | No Calc | No Calc |



60| 70| 7605.00 | 156682. | No Calc | No Calc |

70| 80| 7605.00 | 156682. | No Calc | No Calc |

80| 90| 7605.00 | 156682. | No Calc | No Calc |

90| 100| 7605.00 | 156682. | No Calc | No Calc |

100| 110| 7605.00 | 156682. | No Calc | No Calc |

110| 120| 7605.00 | 156682. | No Calc | No Calc |



140| 150| 8210.00 | 175281. | No Calc | No Calc |

150| 160| 8210.00 | 175281. | No Calc | No Calc |




1

160| 170| 8210.00 | 175281. | No Calc | No Calc |

170| 180| 8210.00 | 175281. | No Calc | No Calc |

180| 190| 8210.00 | 175281. | No Calc | No Calc |

190| 200| 8210.00 | 175281. | No Calc | No Calc |



220| 230| 433.333 | 8787.03 | No Calc | No Calc |


Elements Suitable for External Pressure.




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Element and Detail Weights : Step: 11 3:23p Dec 18,2015

1

Element and Detail Weights

| | Element | Element | Corroded | Corroded | Extra due |

From| To | Metal Wgt. | ID Volume |Metal Wgt. | ID Volume | Misc % |

| | kg. | Cm. | kg. | Cm. | kg. |

---------------------------------------------------------------------------

10| 20| 133.386 | 170200. | 133.386 | 170200. | ... |

20| 30| 382.061 | 1.178E+06 | 382.061 | 1.178E+06 | ... |

30| 40| 324.752 | 1.002E+06 | 324.752 | 1.002E+06 | ... |

40| 50| 232.767 | 113903. | 232.767 | 113903. | ... |

50| 60| 232.767 | 113903. | 232.767 | 113903. | ... |

60| 70| 345.129 | 1.064E+06 | 345.129 | 1.064E+06 | ... |

70| 80| 382.061 | 1.178E+06 | 382.061 | 1.178E+06 | ... |

80| 90| 382.061 | 1.178E+06 | 382.061 | 1.178E+06 | ... |

90| 100| 382.061 | 1.178E+06 | 382.061 | 1.178E+06 | ... |

100| 110| 318.385 | 981924. | 318.385 | 981924. | ... |

110| 120| 127.354 | 392769. | 127.354 | 392769. | ... |

120| 130| 232.767 | 113903. | 232.767 | 113903. | ... |

130| 140| 232.767 | 113903. | 232.767 | 113903. | ... |

140| 150| 382.061 | 1.178E+06 | 382.061 | 1.178E+06 | ... |

150| 160| 382.061 | 1.178E+06 | 382.061 | 1.178E+06 | ... |

160| 170| 382.061 | 1.178E+06 | 382.061 | 1.178E+06 | ... |

170| 180| 382.061 | 1.178E+06 | 382.061 | 1.178E+06 | ... |

180| 190| 382.061 | 1.178E+06 | 382.061 | 1.178E+06 | ... |

190| 200| 180.843 | 557733. | 180.843 | 557733. | ... |

200| 210| 232.767 | 113903. | 232.767 | 113903. | ... |

210| 220| 232.767 | 113903. | 232.767 | 113903. | ... |

220| 230| 76.4123 | 235662. | 76.4123 | 235662. | ... |

230| 240| 133.386 | 170200. | 133.386 | 170200. | ... |




1

---------------------------------------------------------------------------

Total 6474 15862646.00 6474 15862646.00 0

Weight of Details

| | Weight of | X Offset, | Y Offset, |

From|Type| Detail | Dtl. Cent. |Dtl. Cent. | Description

| | kg. | mm. | mm. |

-------------------------------------------------

10|Insl| 34.2076 | ... | -100.000 | Ins: 80

10|Nozl| 18.6642 | 1.00000 | -249.999 | N03

10|Nozl| 5.72848 | 350.000 | -178.536 | N04

20|Insl| 97.9815 | ... | 750.000 | Ins: 80

20|Nozl| 2.46482 | 519.050 | 150.000 | LI1

30|Pack| ... | ... | ... | Pack:[1 of 1]

30|Insl| 83.2843 | ... | 637.500 | Ins: 80

30|Nozl| 86.8724 | 693.675 | 750.000 | N02

30|Nozl| 12.8687 | 519.050 | 200.000 | LI-2

40|Insl| 8.86817 | ... | 72.5000 | Ins: 80

50|Insl| 8.86817 | ... | 72.5000 | Ins: 80

60|Pack| 767.837 | ... | 812.498 | Mellapack-1

60|Insl| 88.5099 | ... | 677.500 | Ins: 80

70|Pack| 1061.53 | ... | 750.000 | Mellapack-2

70|Insl| 97.9815 | ... | 750.000 | Ins: 80

70|Lugs| 140.000 | ... | 1001.00 | SUPPORT LUG

80|Pack| 1061.53 | ... | 750.000 | Mellapack-3

80|Insl| 97.9815 | ... | 750.000 | Ins: 80

90|Pack| 1061.53 | ... | 750.000 | Mellapack-4

90|Insl| 97.9815 | ... | 750.000 | Ins: 80

100|Pack| 403.381 | ... | 285.000 | Mellapack-5




1

100|Insl| 81.6512 | ... | 625.000 | Ins: 80

100|Nozl| 14.0218 | 580.734 | 1000.00 | LG2

100|Nozl| 14.0218 | 580.734 | 1000.00 | SG2

110|Insl| 32.6605 | ... | 250.000 | Ins: 80

120|Insl| 8.86817 | ... | 72.5000 | Ins: 80

130|Insl| 8.86817 | ... | 72.5000 | Ins: 80

140|Pack| 452.919 | ... | 1180.00 | Mellapack-6

140|Insl| 97.9815 | ... | 750.000 | Ins: 80

150|Pack| 1061.53 | ... | 750.000 | Mellapack-7

150|Insl| 97.9815 | ... | 750.000 | Ins: 80

160|Pack| 1061.53 | ... | 750.000 | Mellapack-8

160|Insl| 97.9815 | ... | 750.000 | Ins: 80

170|Pack| 10615.3 | ... | 750.000 | Mellapack-9

170|Insl| 97.9815 | ... | 750.000 | Ins: 80

180|Pack| 665.225 | ... | 470.000 | Mellapack-10

180|Insl| 97.9815 | ... | 750.000 | Ins: 80

190|Insl| 46.3779 | ... | 355.000 | Ins: 80

190|Nozl| 8.60826 | 538.964 | 500.000 | N01

200|Insl| 8.86817 | ... | 72.5000 | Ins: 80

210|Insl| 8.86817 | ... | 72.5000 | Ins: 80

220|Insl| 19.5963 | ... | 150.000 | Ins: 80

230|Insl| 34.2076 | ... | 150.000 | Ins: 80

230|Nozl| 90.3460 | ... | 554.800 | N5

60|Pliq| 255.54 | 0.00000 | 812.49847 |

70|Pliq| 353.28 | 0.00000 | 750.00000 |

80|Pliq| 353.28 | 0.00000 | 750.00000 |

90|Pliq| 353.28 | 0.00000 | 750.00000 |

100|Pliq| 134.25 | 0.00000 | 285.00000 |

140|Pliq| 150.73 | 0.00000 |1180.00000 |

160|Pliq| 353.28 | 0.00000 | 750.00000 |




1

170|Pliq| 353.28 | 0.00000 | 750.00000 |

180|Pliq| 221.39 | 0.00000 | 470.00000 |

Total Weight of Each Detail Type

Total Weight of Packing 18212.3

Total Weight of Packing Liquid 2528.3

Total Weight of Insulation 1355.5

Total Weight of Nozzles 253.6

Total Weight of Lugs 140.0

---------------------------------------------------------------

Sum of the Detail Weights 22489.7 kg.

Weight Summation

Fabricated Shop Test Shipping Erected Empty Operating

------------------------------------------------------------------------------

6474.8 6868.4 6474.8 6868.4 6474.8 26436.2

... 15853.0 ... 18212.3 ... ...

253.6 ... 253.6 ... ... ...

... ... ... 1355.5 18212.3 2528.3

140.0 ... 140.0 ... 1355.5 ...

... ... ... ... ... ...

... ... ... ... ... ...

... ... ... ... 253.6 ...

... ... ... ... 140.0 ...

------------------------------------------------------------------------------

6868.4 22721.4 26436.2 26436.2 26436.2 28964.5 kg.




1

Note: The shipping total has been modified because some items have

been specified as being installed in the shop.

Weight Summary

Fabricated Wt. - Bare Weight W/O Removable Internals 6868.4 kg.

Shop Test Wt. - Fabricated Weight + Water ( Full ) 22721.4 kg.

Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 26436.2 kg.

Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 26436.2 kg.

Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 26436.2 kg.

Operating Wt. - Empty Wt + Operating Liq. Uncorroded 28964.5 kg.

Field Test Wt. - Empty Weight + Water (Full) 35328.3 kg.

Mass of the Upper 1/3 of the Vertical Vessel 16574.5 kg.

Outside Surface Areas of Elements

| | Surface |

From| To | Area |

| | cm² |

----------------------------

10| 20| 12974.9 |

20| 30| 48066.4 |

30| 40| 40856.4 |

40| 50| 8592.26 |

50| 60| 8592.26 |

60| 70| 43420.0 |

70| 80| 48066.4 |

80| 90| 48066.4 |

90| 100| 48066.4 |




1

100| 110| 40055.3 |

110| 120| 16022.1 |

120| 130| 8592.26 |

130| 140| 8592.26 |

140| 150| 48066.4 |

150| 160| 48066.4 |

160| 170| 48066.4 |

170| 180| 48066.4 |

180| 190| 48066.4 |

190| 200| 22751.4 |

200| 210| 8592.26 |

210| 220| 8592.26 |

220| 230| 9613.28 |

230| 240| 12974.9 |

----------------------------

Total 682819.312 cm²

Element and Detail Weights

| To | Total Ele.| Total. Ele.|Total. Ele.| Total Dtl.| Oper. Wgt. |

From| To | Empty Wgt.| Oper. Wgt.|Hydro. Wgt.| Offset Mom.| No Liquid |

| | kg. | kg. | kg. | Kg-m. | kg. |

---------------------------------------------------------------------------

10| 20| 191.987 | 191.987 | 362.083 | 2.02367 | 191.987 |

20| 30| 482.508 | 482.508 | 1660.10 | 1.27939 | 482.508 |

30| 40| 507.778 | 507.778 | 1508.73 | 66.9420 | 507.778 |

40| 50| 241.635 | 241.635 | 355.469 | ... | 241.635 |

50| 60| 241.635 | 241.635 | 355.469 | ... | 241.635 |

60| 70| 1201.48 | 1457.01 | 1668.98 | ... | 1201.48 |

70|Lugs| 899.250 | 1105.33 | 1105.33 | ... | 899.250 |




1

Lugs| 80| 642.322 | 789.520 | 789.520 | ... | 642.322 |

80| 90| 1541.57 | 1894.85 | 1894.85 | ... | 1541.57 |

90| 100| 1541.57 | 1894.85 | 1894.85 | ... | 1541.57 |

100| 110| 831.461 | 965.706 | 1499.55 | 16.2862 | 831.461 |

110| 120| 160.014 | 160.014 | 552.544 | ... | 160.014 |

120| 130| 241.635 | 241.635 | 355.469 | ... | 241.635 |

130| 140| 241.635 | 241.635 | 355.469 | ... | 241.635 |

140| 150| 932.962 | 1083.69 | 1758.84 | ... | 932.962 |

150| 160| 1541.57 | 1541.57 | 1657.63 | ... | 1541.57 |

160| 170| 1541.57 | 1894.85 | 1894.85 | ... | 1541.57 |

170| 180| 11095.3 | 11448.6 | 11448.6 | ... | 11095.3 |

180| 190| 1145.27 | 1366.65 | 1806.29 | ... | 1145.27 |

190| 200| 235.829 | 235.829 | 793.221 | 4.63963 | 235.829 |

200| 210| 241.635 | 241.635 | 355.469 | ... | 241.635 |

210| 220| 241.635 | 241.635 | 355.469 | ... | 241.635 |

220| 230| 96.0086 | 96.0086 | 331.526 | ... | 96.0086 |

230| 240| 257.940 | 257.940 | 428.036 | ... | 257.940 |

Cumulative Vessel Weight

| | Cumulative Ope | Cumulative | Cumulative |

From| To | Wgt. No Liquid | Oper. Wgt. | Hydro. Wgt. |

| | kg. | kg. | kg. |

-------------------------------------------------------

10| 20| ... | ... | ... |

20| 30| -191.987 | -191.987 | -362.083 |

30| 40| -674.494 | -674.494 | -2022.18 |

40| 50| -1182.27 | -1182.27 | -3530.91 |

50| 60| -1423.91 | -1423.91 | -3886.38 |

60| 70| -1665.54 | -1665.54 | -4241.85 |




1

20| 30| 3.30306 | 3.30306 | 3.30306 |

30| 40| 70.2451 | 70.2451 | 70.2451 |

40| 50| 70.2451 | 70.2451 | 70.2451 |

50| 60| 70.2451 | 70.2451 | 70.2451 |

60| 70| 70.2451 | 70.2451 | 70.2451 |

70|Lugs| 70.2451 | 70.2451 | 70.2451 |

Lugs| 80| 20.9258 | 20.9258 | 20.9258 |

80| 90| 20.9258 | 20.9258 | 20.9258 |

90| 100| 20.9258 | 20.9258 | 20.9258 |

100| 110| 20.9258 | 20.9258 | 20.9258 |

110| 120| 4.63963 | 4.63963 | 4.63963 |

120| 130| 4.63963 | 4.63963 | 4.63963 |

130| 140| 4.63963 | 4.63963 | 4.63963 |

140| 150| 4.63963 | 4.63963 | 4.63963 |

150| 160| 4.63963 | 4.63963 | 4.63963 |

160| 170| 4.63963 | 4.63963 | 4.63963 |

170| 180| 4.63963 | 4.63963 | 4.63963 |

180| 190| 4.63963 | 4.63963 | 4.63963 |

190| 200| 4.63963 | 4.63963 | 4.63963 |

200| 210| ... | ... | ... |

210| 220| ... | ... | ... |

220| 230| ... | ... | ... |

230| 240| ... | ... | ... |




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------

Nozzle Flange MAWP : Step: 12 3:23p Dec 18,2015

1

Nozzle Flange MAWP Results :

Nozzle ----- Flange Rating

Description Operating Ambient Temperature Class Grade|Group

bars bars C

----------------------------------------------------------------------------

N03 13.1 19.0 220 150 GR 2.2

N04 13.1 19.0 220 150 GR 2.2

LI1 13.1 19.0 220 150 GR 2.2

N02 13.1 19.0 220 150 GR 2.2

LI-2 13.1 19.0 220 150 GR 2.2

LG2 13.1 19.0 220 150 GR 2.2

SG2 13.1 19.0 220 150 GR 2.2

N01 13.1 19.0 220 150 GR 2.2

N5 13.1 19.0 220 150 GR 2.2

----------------------------------------------------------------------------

Minimum Rating 13.1 19.0 bars

Note: ANSI Ratings are per ANSI/ASME B16.5 2009 Metric Edition





Natural Frequency Calculation : Step: 13 3:23p Dec 18,2015

1

The Natural Frequencies for the vessel have been computed iteratively

by solving a system of matrices. These matrices describe the mass

and the stiffness of the vessel. This is the generalized eigenvalue/

eigenvector problem and is referenced in some mathematical texts.

The Natural Frequency for the Vessel (Empty.) is 1.59031 Hz.

The Natural Frequency for the Vessel (Ope...) is 1.54759 Hz.





Wind Load Calculation : Step: 14 3:23p Dec 18,2015

1

Wind Load Calculations per India Std. IS-875 (Part-3) - 1987, Amd. 1&2 (2003):

Actual Vessel Height to Diameter ratio 14.831

Force Coefficient per IS:875 Table 23, Cf 0.948

User Entered Basic Wind Speed 170.0 Km/hr

Base Elevation 300.00 mm.

Wind Zone Number 4

Risk Factor (k1) 1.0000

Terrain Category 3

Equipment Class A

Topography Factor (k3) 1.0000

Use Gust Response Factor (Dynamic Analysis) No

User entered Beta Value ( Operating Case ) 0.0100

Checking the requirement for Dynamic Effect of wind (7.1):

Vessel Operating Natural Frequency 1.548 Hz

Vessel Height to Diameter ratio 14.831

Note: Vessel Natural frequency is >= 1 Hz.

Warning: Vessel height to diameter ratio (14.831) is > 5.

Note: As per Section 7.1, Dynamic effects of wind should be considered. The

Cross-Wind dynamic effects can be considered using the Vortex Shedding

which can be invoked from Design Constraints tab. While the Along-Wind

effects can be considered using Gust Response Factor method, which can be

invoked from the Wind Load tab.





1

From fo` FO E S G(ope) G(emp) G(tst)

------------------------------------------------------------------

10 56.02 13.48 0.0354 0.1748 1.0000 1.0000 1.0000

20 56.02 13.48 0.0354 0.1748 1.0000 1.0000 1.0000

30 56.02 13.48 0.0354 0.1748 1.0000 1.0000 1.0000

40 56.02 13.48 0.0354 0.1748 1.0000 1.0000 1.0000

50 56.02 13.48 0.0354 0.1748 1.0000 1.0000 1.0000

60 56.02 13.48 0.0354 0.1748 1.0000 1.0000 1.0000

70 56.02 13.48 0.0354 0.1748 1.0000 1.0000 1.0000

80 56.02 13.48 0.0354 0.1748 1.0000 1.0000 1.0000

90 56.02 13.48 0.0354 0.1748 1.0000 1.0000 1.0000

100 55.86 13.44 0.0354 0.1753 1.0000 1.0000 1.0000

110 54.90 13.21 0.0359 0.1785 1.0000 1.0000 1.0000

120 54.56 13.13 0.0360 0.1796 1.0000 1.0000 1.0000

130 54.41 13.09 0.0361 0.1802 1.0000 1.0000 1.0000

140 53.55 12.88 0.0365 0.1830 1.0000 1.0000 1.0000

150 52.06 12.52 0.0371 0.1880 1.0000 1.0000 1.0000

160 50.70 12.20 0.0378 0.1925 1.0000 1.0000 1.0000

170 49.62 11.94 0.0383 0.1961 1.0000 1.0000 1.0000

180 48.59 11.69 0.0389 0.1995 1.0000 1.0000 1.0000

190 47.86 11.51 0.0393 0.2019 1.0000 1.0000 1.0000

200 47.58 11.45 0.0394 0.2029 1.0000 1.0000 1.0000

210 47.49 11.42 0.0395 0.2032 1.0000 1.0000 1.0000

220 47.39 11.40 0.0395 0.2035 1.0000 1.0000 1.0000

230 47.25 11.37 0.0396 0.2039 1.0000 1.0000 1.0000

Design Wind Speed (Vz):

= Basic Wind Speed * k1 * k2 * k3





1

Height Factor :

= 0.6 * Vz²

Element Wind Load :

= Wind Area * Cf * Height Factor

From Height k1 k2 k3 Vz Cf

mm. m/sec

------------------------------------------------------------

10 568.50 1.0000 0.9287 1.0000 43.85 0.9483

20 1350.00 1.0000 0.9287 1.0000 43.85 0.9483

30 2737.50 1.0000 0.9287 1.0000 43.85 0.9483

40 3447.50 1.0000 0.9287 1.0000 43.85 0.9483

50 3592.50 1.0000 0.9287 1.0000 43.85 0.9483

60 4342.50 1.0000 0.9287 1.0000 43.85 0.9483

70 5770.00 1.0000 0.9287 1.0000 43.85 0.9483

80 7270.00 1.0000 0.9287 1.0000 43.85 0.9483

90 8770.00 1.0000 0.9287 1.0000 43.85 0.9483

100 10145.00 1.0000 0.9304 1.0000 43.93 0.9483

110 11020.00 1.0000 0.9396 1.0000 44.37 0.9483

120 11342.50 1.0000 0.9429 1.0000 44.52 0.9483

130 11487.50 1.0000 0.9443 1.0000 44.59 0.9483

140 12310.00 1.0000 0.9521 1.0000 44.96 0.9483

150 13810.00 1.0000 0.9650 1.0000 45.57 0.9483

160 15310.00 1.0000 0.9765 1.0000 46.11 0.9483

170 16810.00 1.0000 0.9870 1.0000 46.61 0.9483

180 18310.00 1.0000 0.9966 1.0000 47.06 0.9483

190 19415.00 1.0000 1.0032 1.0000 47.37 0.9483

200 19842.50 1.0000 1.0056 1.0000 47.49 0.9483

210 19987.50 1.0000 1.0065 1.0000 47.52 0.9483





1

220 20210.00 1.0000 1.0077 1.0000 47.58 0.9483

230 20561.50 1.0000 1.0096 1.0000 47.67 0.9483

Wind Vibration Calculations

This evaluation is based on work by Kanti Mahajan and Ed Zorilla

Nomenclature

Cf - Correction factor for natural frequency

D - Average internal diameter of vessel mm.

Df - Damping Factor < 0.75 Unstable, > 0.95 Stable

Dr - Average internal diameter of top half of vessel mm.

f - Natural frequency of vibration (Hertz)

f1 - Natural frequency of bare vessel based on a unit value of (D/L²)(10 4)

L - Total height of structure mm.

Lc - Total length of conical section(s) of vessel mm.

tb - Uncorroded plate thickness at bottom of vessel mm.

V30 - Design Wind Speed provided by user Km/hr

Vc - Critical wind velocity Km/hr

Vw - Maximum wind speed at top of structure Km/hr

W - Total corroded weight of structure Kgf

Ws - Cor. vessel weight excl. weight of parts which do not effect stiff. Kgf

Z - Maximum amplitude of vibration at top of vessel mm.

Dl - Logarithmic decrement ( taken as 0.03 for Welded Structures )

Vp - Vib. Chance, <= 0.320E-06 (High); 0.320E-06 < 0.400E-06 (Probable)

P30 - wind pressure 30 feet above the base

Check other Conditions and Basic Assumptions:





1

#1 - Total Cone Length / Total Length < 0.5

0.000/19860.000 = 0.000

#2 - ( D / L² ) * 10 4 < 8.0 (English Units)

- ( 4.39/65.16² ) * 10 4 = 10.348 [Geometry Violation]

Compute the vibration possibility. If Vp > 0.400E-06 no chance. [Vp]:

= W / ( L * Dr²)

= 28964/( 19860.00 * 1000.000² )

= 0.14584E-05

Since Vp is > 0.400E-06 no further vibration analysis is required !


Wind Load Calculation

| | Wind | Wind | Wind | Wind | Element |

From| To | Height | Diameter | Area | Pressure | Wind Load |

| | mm. | mm. | cm² | Kgs/m² | Kgf |

---------------------------------------------------------------------------

10| 20| 568.500 | 1608.00 | 6108.27 | 117.719 | 68.1645 |

20| 30| 1350.00 | 1608.00 | 24120.0 | 117.719 | 269.164 |

30| 40| 2737.50 | 1608.00 | 20502.0 | 117.719 | 228.790 |

40| 50| 3447.50 | 1584.00 | 2296.80 | 117.719 | 25.6309 |

50| 60| 3592.50 | 1584.00 | 2296.80 | 117.719 | 25.6309 |

60| 70| 4342.50 | 1608.00 | 21788.4 | 117.719 | 243.145 |

70| 80| 5770.00 | 1608.00 | 24120.0 | 117.719 | 269.164 |

80| 90| 7270.00 | 1608.00 | 24120.0 | 117.719 | 269.164 |

90| 100| 8770.00 | 1608.00 | 24120.0 | 117.719 | 269.164 |





1

100| 110| 10145.0 | 1608.00 | 20100.0 | 118.129 | 225.085 |

110| 120| 11020.0 | 1608.00 | 8040.00 | 120.498 | 91.8397 |

120| 130| 11342.5 | 1584.00 | 2296.80 | 121.330 | 26.4171 |

130| 140| 11487.5 | 1584.00 | 2296.80 | 121.697 | 26.4970 |

140| 150| 12310.0 | 1608.00 | 24120.0 | 123.706 | 282.852 |

150| 160| 13810.0 | 1608.00 | 24120.0 | 127.081 | 290.571 |

160| 170| 15310.0 | 1608.00 | 24120.0 | 130.147 | 297.581 |

170| 180| 16810.0 | 1608.00 | 24120.0 | 132.958 | 304.007 |

180| 190| 18310.0 | 1608.00 | 24120.0 | 135.555 | 309.945 |

190| 200| 19415.0 | 1608.00 | 11416.8 | 137.349 | 148.649 |

200| 210| 19842.5 | 1584.00 | 2296.80 | 138.019 | 30.0508 |

210| 220| 19987.5 | 1584.00 | 2296.80 | 138.244 | 30.0996 |

220| 230| 20210.0 | 1608.00 | 4824.00 | 138.585 | 63.3748 |

230| 240| 20561.5 | 1608.00 | 6108.27 | 139.118 | 80.5552 |




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Earthquake Load Calculation : Step: 15 3:23p Dec 18,2015

1

Seismic Analysis Results per IS-1893 (1984), Seismic Coefficient Method.

Soil Factor ß 1.3000

Importance Factor as Entered by User I 1.0000

Zone Number 3

Value of Alpha o per table 2 and Zone 0.0400

Horizontal Seismic Coefficient (Alpha h):

= ß * I * Alpha o

= 1.3000 * 1.0000 * 0.0400

= 0.0520

Earthquake Element Load, for the first Element:

= Earthquake Weight * Alpha h

= 191.99 * 0.0520

= 10.0 Kgf


Earthquake Load Calculation

| | Earthquake | Earthquake | Element | Element |

From| To | Height | Weight | Ope Load | Emp Load |

| | mm. | Kgf | Kgf | Kgf |

--------------------------------------------------------------

10| 20| 25.0000 | 191.987 | 9.98330 | 9.98330 |

20| 30| 800.000 | 482.508 | 25.0904 | 25.0904 |

30| 40| 2187.50 | 507.778 | 26.4044 | 26.4044 |

40| 50| 2897.50 | 241.635 | 12.5650 | 12.5650 |

50| 60| 3042.50 | 241.635 | 12.5650 | 12.5650 |



C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Earthquake Load Calculation : Step: 15 3:23p Dec 18,2015

1

60| 70| 3792.50 | 1457.01 | 75.7646 | 62.4768 |

70|Lugs| 5345.00 | 1105.33 | 57.4771 | 46.7610 |

Lugs| 80| 5657.50 | 789.520 | 41.0551 | 33.4007 |

80| 90| 6720.00 | 1894.85 | 98.5321 | 80.1617 |

90| 100| 8220.00 | 1894.85 | 98.5321 | 80.1617 |

100| 110| 9595.00 | 965.706 | 50.2167 | 43.2360 |

110| 120| 10470.0 | 160.014 | 8.32075 | 8.32075 |

120| 130| 10792.5 | 241.635 | 12.5650 | 12.5650 |

130| 140| 10937.5 | 241.635 | 12.5650 | 12.5650 |

140| 150| 11760.0 | 1083.69 | 56.3520 | 48.5140 |

150| 160| 13260.0 | 1541.57 | 80.1617 | 80.1617 |

160| 170| 14760.0 | 1894.85 | 98.5321 | 80.1617 |

170| 180| 16260.0 | 11448.6 | 595.328 | 576.957 |

180| 190| 17760.0 | 1366.65 | 71.0660 | 59.5539 |

190| 200| 18865.0 | 235.829 | 12.2631 | 12.2631 |

200| 210| 19292.5 | 241.635 | 12.5650 | 12.5650 |

210| 220| 19437.5 | 241.635 | 12.5650 | 12.5650 |

220| 230| 19660.0 | 96.0086 | 4.99245 | 4.99245 |

230| 240| 19835.0 | 257.940 | 13.4129 | 13.4129 |





Wind/Earthquake Shear, Bending : Step: 16 3:23p Dec 18,2015

1

The following table is for the Operating Case.

Wind/Earthquake Shear, Bending

| | Distance to| Cumulative |Earthquake | Wind | Earthquake |

From| To | Support| Wind Shear | Shear | Bending | Bending |

| | mm. | Kgf | Kgf | Kg-m. | Kg-m. |

---------------------------------------------------------------------------

10| 20| 5496.50 | ... | ... | ... | ... |

20| 30| 4545.00 | 68.1645 | 9.98330 | 10.3271 | 1.51250 |

30| 40| 3157.50 | 337.329 | 35.0737 | 314.453 | 35.3059 |

40| 50| 2447.50 | 566.119 | 61.4781 | 890.413 | 96.8589 |

50| 60| 2302.50 | 591.750 | 74.0432 | 974.359 | 106.684 |

60| 70| 1552.50 | 617.380 | 86.6082 | 1062.02 | 118.332 |

70|Lugs| 437.500 | 860.526 | 162.373 | 2063.32 | 287.020 |

Lugs| 80| 312.500 | 3718.53 | 1441.40 | 19033.8 | 10461.9 |

80| 90| 1375.00 | 2745.85 | 1237.97 | 20167.6 | 10129.6 |

90| 100| 2875.00 | 2476.69 | 1139.44 | 16250.6 | 8346.51 |

100| 110| 4250.00 | 2207.52 | 1040.91 | 12737.3 | 6711.22 |

110| 120| 5125.00 | 1982.44 | 990.689 | 10118.6 | 5441.44 |

120| 130| 5447.50 | 1890.60 | 982.368 | 9150.29 | 4948.17 |

130| 140| 5592.50 | 1864.18 | 969.803 | 8878.06 | 4806.64 |

140| 150| 6415.00 | 1837.69 | 957.238 | 8609.67 | 4666.92 |

150| 160| 7915.00 | 1554.83 | 900.886 | 6065.23 | 3273.30 |

160| 170| 9415.00 | 1264.26 | 820.724 | 3950.87 | 1982.07 |

170| 180| 10915.0 | 966.682 | 722.192 | 2277.63 | 824.856 |

180| 190| 12415.0 | 662.674 | 126.865 | 1055.58 | 188.051 |

190| 200| 13520.0 | 352.730 | 55.7985 | 294.015 | 51.0507 |

200| 210| 13947.5 | 204.080 | 43.5354 | 96.3438 | 15.7865 |




Wind/Earthquake Shear, Bending : Step: 16 3:23p Dec 18,2015

1

210| 220| 14092.5 | 174.030 | 30.9704 | 68.9304 | 10.3847 |

220| 230| 14315.0 | 143.930 | 18.4053 | 45.8778 | 6.80492 |

230| 240| 14616.5 | 80.5552 | 13.4129 | 12.2044 | 2.03209 |





Wind Deflection : Step: 17 3:23p Dec 18,2015

1

Wind Deflection Calculations:

The following table is for the Operating Case.

Wind Deflection

| | Cumulative | Centroid | Elem. End | Elem. Ang. |

From| To | Wind Shear | Deflection |Deflection | Rotation |

| | Kgf | mm. | mm. | |

--------------------------------------------------------------

10| 20| ... | 1.20342 | 1.21078 | 0.00007 |

20| 30| 68.1645 | 0.97667 | 1.19606 | 0.00007 |

30| 40| 337.329 | 0.58172 | 0.76085 | 0.00006 |

40| 50| 566.119 | 0.38947 | 0.40874 | 0.00004 |

50| 60| 591.750 | 0.35096 | 0.37021 | 0.00004 |

60| 70| 617.380 | 0.15841 | 0.33172 | 0.00004 |

70|Lugs| 860.526 | -0.073523 | ... | ... |

Lugs| 80| 3718.53 | -0.015962 | 0.092335 | -0.00006 |

80| 90| 2745.85 | 0.45076 | 0.93694 | 0.00028447 |

90| 100| 2476.69 | 1.53746 | 2.23961 | 0.00055564 |

100| 110| 2207.52 | 2.89369 | 3.60344 | 0.00073386 |

110| 120| 1982.44 | 3.90151 | 4.20712 | 0.00079406 |

120| 130| 1890.60 | 4.29683 | 4.38662 | 0.00079602 |

130| 140| 1864.18 | 4.47648 | 4.56640 | 0.00079791 |

140| 150| 1837.69 | 5.52570 | 6.53629 | 0.00093485 |

150| 160| 1554.83 | 7.58959 | 8.67779 | 0.0010281 |

160| 170| 1264.26 | 9.79384 | 10.9315 | 0.0010858 |

170| 180| 966.682 | 12.0852 | 13.2503 | 0.0011163 |





1

180| 190| 662.674 | 14.4228 | 15.5998 | 0.0011283 |

190| 200| 352.730 | 16.1578 | 16.7160 | 0.0011299 |

200| 210| 204.080 | 16.8301 | 16.9441 | 0.0011299 |

210| 220| 174.030 | 17.0581 | 17.1722 | 0.0011299 |

220| 230| 143.930 | 17.4081 | 17.6440 | 0.0011300 |

230| 240| 80.5552 | 17.6834 | 17.7227 | 0.0011300 |

Critical Wind Velocity for Tower Vibration

| | 1st Crit. | 2nd Crit. |

From| To | Wind Speed | Wind Speed |

| | Km/hr | Km/hr |

-------------------------------------

10| 20| 44.6729 | 279.206 |

20| 30| 44.6729 | 279.206 |

30| 40| 44.6729 | 279.206 |

40| 50| 44.0061 | 275.038 |

50| 60| 44.0061 | 275.038 |

60| 70| 44.6729 | 279.206 |

70| 80| 44.6729 | 279.206 |

80| 90| 44.6729 | 279.206 |

90| 100| 44.6729 | 279.206 |

100| 110| 44.6729 | 279.206 |

110| 120| 44.6729 | 279.206 |

120| 130| 44.0061 | 275.038 |

130| 140| 44.0061 | 275.038 |

140| 150| 44.6729 | 279.206 |

150| 160| 44.6729 | 279.206 |

160| 170| 44.6729 | 279.206 |

170| 180| 44.6729 | 279.206 |





1

180| 190| 44.6729 | 279.206 |

190| 200| 44.6729 | 279.206 |

200| 210| 44.0061 | 275.038 |

210| 220| 44.0061 | 275.038 |

220| 230| 44.6729 | 279.206 |

230| 240| 44.6729 | 279.206 |

Allowable deflection at the Tower Top (Ope)( 6.000"/100ft. Criteria)

Allowable deflection : 99.300 Actual Deflection : 17.723 mm.




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Longitudinal Stress Constants : Step: 18 3:23p Dec 18,2015

1




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Longitudinal Allowable Stresses : Step: 19 3:23p Dec 18,2015

1

Longitudinal Allowable Stresses

| | | Hydrotest | | Hydrotest |

From| To | Tensile | Tensile | Compressive | Compressive |

| | N./mm² | N./mm² | N./mm² | N./mm² |

-------------------------------------------------------------------

10| 20| 127.800 | 179.640 | -61.5546 | -93.1460 |

20| 30| 127.800 | 179.640 | -61.5546 | -93.1460 |

30| 40| 127.800 | 179.640 | -61.5546 | -93.1460 |

40| 50| 127.800 | 179.640 | -61.5546 | -93.1460 |

50| 60| 127.800 | 179.640 | -61.5546 | -93.1460 |

60| 70| 127.800 | 179.640 | -61.5546 | -93.1460 |

70|Lugs| 127.800 | 179.640 | -61.5546 | -93.1460 |

Lugs| 80| 127.800 | 179.640 | -61.5546 | -93.1460 |

80| 90| 127.800 | 179.640 | -61.5546 | -93.1460 |

90| 100| 127.800 | 179.640 | -61.5546 | -93.1460 |

100| 110| 127.800 | 179.640 | -61.5546 | -93.1460 |

110| 120| 127.800 | 179.640 | -61.5546 | -93.1460 |

120| 130| 127.800 | 179.640 | -61.5546 | -93.1460 |

130| 140| 127.800 | 179.640 | -61.5546 | -93.1460 |

140| 150| 127.800 | 179.640 | -61.5546 | -93.1460 |

150| 160| 127.800 | 179.640 | -61.5546 | -93.1460 |

160| 170| 127.800 | 179.640 | -61.5546 | -93.1460 |

170| 180| 127.800 | 179.640 | -61.5546 | -93.1460 |

180| 190| 127.800 | 179.640 | -61.5546 | -93.1460 |

190| 200| 127.819 | 179.629 | -61.5546 | -93.1460 |

200| 210| 127.819 | 179.629 | -61.5546 | -93.1460 |

210| 220| 127.819 | 179.629 | -61.5546 | -93.1460 |

220| 230| 127.819 | 179.629 | -61.5546 | -93.1460 |



C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Longitudinal Allowable Stresses : Step: 19 3:23p Dec 18,2015

1

230| 240| 127.819 | 179.629 | -61.5546 | -93.1460 |




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Longitudinal Stresses Due to . . . Step: 20 3:23p Dec 18,2015

1

Longitudinal Stress Report

Note: Longitudinal Operating and Empty Stresses are computed in the

corroded condition. Stresses due to loads in the hydrostatic test

cases have been computed in the new and cold condition.

Longitudinal Stresses Due to . . .

| | Long. Str. | Long. Str. |Long. Str. |

From| To | Int. Pres. | Ext. Pres. |Hyd. Pres. |

| | N./mm² | N./mm² | N./mm² |

-------------------------------------------------

10| 20| 7.44043 | -2.66444 | 10.2181 |

20| 30| 7.44043 | -2.66444 | 10.2181 |

30| 40| 7.44043 | -2.66444 | 10.2181 |

40| 50| ... | ... | ... |

50| 60| ... | ... | ... |

60| 70| 7.44043 | -2.66444 | 10.2181 |

70| 80| 7.44043 | -2.66444 | 10.2181 |

80| 90| 7.44043 | -2.66444 | 10.2181 |

90| 100| 7.44043 | -2.66444 | 10.2181 |

100| 110| 7.44043 | -2.66444 | 10.2181 |

110| 120| 7.44043 | -2.66444 | 10.2181 |

120| 130| ... | ... | ... |

130| 140| ... | ... | ... |

140| 150| 7.44043 | -2.66444 | 10.2181 |

150| 160| 7.44043 | -2.66444 | 10.2181 |

160| 170| 7.44043 | -2.66444 | 10.2181 |

170| 180| 7.44043 | -2.66444 | 10.2181 |




1

170| 180| -4.11485 | -4.29246 | ... | 0.0057346 | 0.0057346 |

180| 190| -0.68561 | -0.75404 | ... | 0.0057346 | 0.0057346 |

190| 200| -0.33165 | -0.33165 | ... | 0.0057346 | 0.0057346 |

200| 210| -0.25876 | -0.25876 | ... | ... | ... |

210| 220| -0.18408 | -0.18408 | ... | ... | ... |

220| 230| -0.10939 | -0.10939 | ... | ... | ... |

230| 240| -0.079721 | -0.079721 | ... | ... | ... |


| | Wght. Str. | Bend. Str. |Bend. Str. | Bend. Str. | Bend. Str. |

From| To | Hyd. Mom. | Oper. Wind |Oper. Equ. | Hyd. Wind | Hyd. Equ. |

| | N./mm² | N./mm² | N./mm² | N./mm² | N./mm² |

---------------------------------------------------------------------------

10| 20| ... | ... | ... | ... | ... |

20| 30| ... | 0.012764 | 0.0018695 | ... | ... |

30| 40| ... | 0.38867 | 0.043639 | ... | ... |

40| 50| ... | 1.10056 | 0.11972 | ... | ... |

50| 60| ... | 1.20432 | 0.13186 | ... | ... |

60| 70| ... | 1.31267 | 0.14626 | ... | ... |

70|Lugs| ... | 2.55029 | 0.35476 | ... | ... |

Lugs| 80| ... | 23.5260 | 12.9311 | ... | ... |

80| 90| ... | 24.9274 | 12.5203 | ... | ... |

90| 100| ... | 20.0859 | 10.3164 | ... | ... |

100| 110| ... | 15.7435 | 8.29514 | ... | ... |

110| 120| ... | 12.5067 | 6.72569 | ... | ... |

120| 130| ... | 11.3099 | 6.11600 | ... | ... |

130| 140| ... | 10.9734 | 5.94106 | ... | ... |

140| 150| ... | 10.6417 | 5.76837 | ... | ... |

150| 160| ... | 7.49670 | 4.04584 | ... | ... |




1

160| 170| ... | 4.88332 | 2.44986 | ... | ... |

170| 180| ... | 2.81517 | 1.01953 | ... | ... |

180| 190| ... | 1.30471 | 0.23243 | ... | ... |

190| 200| ... | 0.36341 | 0.063099 | ... | ... |

200| 210| ... | 0.11908 | 0.019512 | ... | ... |

210| 220| ... | 0.085199 | 0.012836 | ... | ... |

220| 230| ... | 0.056706 | 0.0084110 | ... | ... |

230| 240| ... | 0.015085 | 0.0025117 | ... | ... |


| | Long. Str. | Long. Str. |Long. Str. | EarthQuake |

From| To | Vortex Ope.| Vortex Emp.|Vortex Tst.| Empty |

| | N./mm² | N./mm² | N./mm² | N./mm² |

--------------------------------------------------------------

10| 20| ... | ... | ... | ... |

20| 30| ... | ... | ... | 0.0018695 |

30| 40| ... | ... | ... | 0.043639 |

40| 50| ... | ... | ... | 0.11972 |

50| 60| ... | ... | ... | 0.13186 |

60| 70| ... | ... | ... | 0.14626 |

70|Lugs| ... | ... | ... | 0.34363 |

Lugs| 80| ... | ... | ... | 12.1258 |

80| 90| ... | ... | ... | 11.7638 |

90| 100| ... | ... | ... | 9.72791 |

100| 110| ... | ... | ... | 7.84064 |

110| 120| ... | ... | ... | 6.36325 |

120| 130| ... | ... | ... | 5.78822 |

130| 140| ... | ... | ... | 5.62333 |

140| 150| ... | ... | ... | 5.46070 |




1

130| 140| ... | ... | ... | ... |

140| 150| ... | ... | ... | ... |

150| 160| ... | ... | ... | ... |

160| 170| ... | ... | ... | ... |

170| 180| ... | ... | ... | ... |

180| 190| ... | ... | ... | ... |

190| 200| ... | ... | ... | ... |

200| 210| ... | ... | ... | ... |

210| 220| ... | ... | ... | ... |

220| 230| ... | ... | ... | ... |

230| 240| ... | ... | ... | ... |




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Stress due to Combined Loads : Step: 21 3:23p Dec 18,2015

1

Stress Combination Load Cases for Vertical Vessels:

Load Case Definition Key

IP = Longitudinal Stress due to Internal Pressure

EP = Longitudinal Stress due to External Pressure

HP = Longitudinal Stress due to Hydrotest Pressure

NP = No Pressure

EW = Longitudinal Stress due to Weight (No Liquid)

OW = Longitudinal Stress due to Weight (Operating)

HW = Longitudinal Stress due to Weight (Hydrotest)

WI = Bending Stress due to Wind Moment (Operating)

EQ = Bending Stress due to Earthquake Moment (Operating)

EE = Bending Stress due to Earthquake Moment (Empty)

HI = Bending Stress due to Wind Moment (Hydrotest)

HE = Bending Stress due to Earthquake Moment (Hydrotest)

WE = Bending Stress due to Wind Moment (Empty) (no CA)

WF = Bending Stress due to Wind Moment (Filled) (no CA)

CW = Longitudinal Stress due to Weight (Empty) (no CA)

VO = Bending Stress due to Vortex Shedding Loads ( Ope )

VE = Bending Stress due to Vortex Shedding Loads ( Emp )

VF = Bending Stress due to Vortex Shedding Loads ( Test No CA. )

FW = Axial Stress due to Vertical Forces for the Wind Case

FS = Axial Stress due to Vertical Forces for the Seismic Case

BW = Bending Stress due to Lat. Forces for the Wind Case, Corroded

BS = Bending Stress due to Lat. Forces for the Seismic Case, Corroded

BN = Bending Stress due to Lat. Forces for the Wind Case, UnCorroded

BU = Bending Stress due to Lat. Forces for the Seismic Case, UnCorroded




1

General Notes:

Case types HI and HE are in the Un-Corroded condition.

Case types WE, WF, and CW are in the Un-Corroded condition.

A blank stress and stress ratio indicates that the corresponding

stress comprising those components that did not contribute to that

type of stress.

An asterisk (*) in the final column denotes overstress.

Analysis of Load Case 1 : NP+EW+WI+FW+BW

From Tensile All. Tens. Comp. All. Comp. Tens. Comp.

Node Stress Stress Stress Stress Ratio Ratio

10 0.00 127.80 0.00 61.55 0.0000 0.0000

20 0.08 127.80 61.55 0.0006

30 0.68 127.80 -0.27 61.55 0.0054 0.0043

60 1.91 127.80 -0.88 61.55 0.0150 0.0144

70 3.52 127.80 -1.75 61.55 0.0276 0.0284

70 16.59 127.80 -30.52 61.55 0.1298 0.4957

80 18.19 127.80 -31.72 61.55 0.1423 0.5153

90 13.82 127.80 -26.40 61.55 0.1082 0.4289

100 9.96 127.80 -21.58 61.55 0.0779 0.3506

110 6.96 127.80 -18.07 61.55 0.0544 0.2935

140 5.29 127.80 -16.00 61.55 0.0414 0.2600

150 2.43 127.80 -12.57 61.55 0.0191 0.2042

160 0.30 127.80 -9.48 61.55 0.0023 0.1540




1

170 127.80 -6.94 61.55 0.1127

180 0.62 127.80 -2.00 61.55 0.0049 0.0324

190 0.04 127.82 -0.70 61.55 0.0003 0.0114

220 127.82 -0.17 61.55 0.0027

230 127.82 -0.09 61.55 0.0015

Analysis of Load Case 2 : NP+EW+EE+FS+BS



10 0.00 127.80 0.00 61.55 0.0000 0.0000

20 0.07 127.80 61.55 0.0005

30 0.34 127.80 61.55 0.0027

60 0.75 127.80 61.55 0.0059

70 1.32 127.80 61.55 0.0103

70 5.19 127.80 -19.12 61.55 0.0406 0.3105

80 5.02 127.80 -18.55 61.55 0.0393 0.3014

90 3.47 127.80 -16.04 61.55 0.0271 0.2606

100 2.05 127.80 -13.68 61.55 0.0161 0.2222

110 0.81 127.80 -11.92 61.55 0.0064 0.1937

140 0.11 127.80 -10.82 61.55 0.0009 0.1758

150 127.80 -8.91 61.55 0.1447

160 127.80 -6.93 61.55 0.1125

170 127.80 -5.09 61.55 0.0827

180 127.80 -0.91 61.55 0.0148

190 127.82 -0.40 61.55 0.0065

220 127.82 -0.12 61.55 0.0019

230 127.82 -0.08 61.55 0.0013

Analysis of Load Case 3 : NP+OW+WI+FW+BW





1


10 0.00 127.80 0.00 61.55 0.0000 0.0000

20 0.08 127.80 61.55 0.0006

30 0.68 127.80 -0.27 61.55 0.0054 0.0043

60 1.91 127.80 -0.88 61.55 0.0150 0.0144

70 3.60 127.80 -1.67 61.55 0.0282 0.0272

70 15.95 127.80 -31.15 61.55 0.1248 0.5061

80 17.60 127.80 -32.31 61.55 0.1377 0.5249

90 13.34 127.80 -26.88 61.55 0.1044 0.4368

100 9.58 127.80 -21.96 61.55 0.0750 0.3567

110 6.62 127.80 -18.40 61.55 0.0518 0.2989

140 4.96 127.80 -16.34 61.55 0.0388 0.2654

150 2.15 127.80 -12.86 61.55 0.0168 0.2089

160 0.01 127.80 -9.77 61.55 0.0001 0.1587

170 127.80 -7.11 61.55 0.1156

180 0.56 127.80 -2.06 61.55 0.0044 0.0335

190 0.04 127.82 -0.70 61.55 0.0003 0.0114

220 127.82 -0.17 61.55 0.0027

230 127.82 -0.09 61.55 0.0015

Analysis of Load Case 4 : NP+OW+EQ+FS+BS



10 0.00 127.80 0.00 61.55 0.0000 0.0000

20 0.07 127.80 61.55 0.0005

30 0.34 127.80 61.55 0.0027

60 0.75 127.80 61.55 0.0059

70 1.41 127.80 61.55 0.0110

70 5.35 127.80 -20.56 61.55 0.0419 0.3340

80 5.19 127.80 -19.90 61.55 0.0406 0.3234




1

90 3.57 127.80 -17.11 61.55 0.0279 0.2780

100 2.13 127.80 -14.51 61.55 0.0167 0.2357

110 0.84 127.80 -12.62 61.55 0.0066 0.2050

140 0.08 127.80 -11.46 61.55 0.0007 0.1862

150 127.80 -9.41 61.55 0.1528

160 127.80 -7.33 61.55 0.1191

170 127.80 -5.32 61.55 0.0864

180 127.80 -0.99 61.55 0.0161

190 127.82 -0.40 61.55 0.0065

220 127.82 -0.12 61.55 0.0019

230 127.82 -0.08 61.55 0.0013

Analysis of Load Case 5 : NP+HW+HI



10 0.00 179.64 0.00 93.15 0.0000 0.0000

20 0.00 179.64 0.00 93.15 0.0000 0.0000

30 0.00 179.64 0.00 93.15 0.0000 0.0000

60 0.00 179.64 0.00 93.15 0.0000 0.0000

70 0.00 179.64 0.00 93.15 0.0000 0.0000

70 0.00 179.64 0.00 93.15 0.0000 0.0000

80 0.00 179.64 0.00 93.15 0.0000 0.0000

90 0.00 179.64 0.00 93.15 0.0000 0.0000

100 0.00 179.64 0.00 93.15 0.0000 0.0000

110 0.00 179.64 0.00 93.15 0.0000 0.0000

140 0.00 179.64 0.00 93.15 0.0000 0.0000

150 0.00 179.64 0.00 93.15 0.0000 0.0000

160 0.00 179.64 0.00 93.15 0.0000 0.0000

170 0.00 179.64 0.00 93.15 0.0000 0.0000

180 0.00 179.64 0.00 93.15 0.0000 0.0000




1

190 0.00 179.63 0.00 93.15 0.0000 0.0000

220 0.00 179.63 0.00 93.15 0.0000 0.0000

230 0.00 179.63 0.00 93.15 0.0000 0.0000

Analysis of Load Case 6 : NP+HW+HE



10 0.00 179.64 0.00 93.15 0.0000 0.0000

20 0.00 179.64 0.00 93.15 0.0000 0.0000

30 0.00 179.64 0.00 93.15 0.0000 0.0000

60 0.00 179.64 0.00 93.15 0.0000 0.0000

70 0.00 179.64 0.00 93.15 0.0000 0.0000

70 0.00 179.64 0.00 93.15 0.0000 0.0000

80 0.00 179.64 0.00 93.15 0.0000 0.0000

90 0.00 179.64 0.00 93.15 0.0000 0.0000

100 0.00 179.64 0.00 93.15 0.0000 0.0000

110 0.00 179.64 0.00 93.15 0.0000 0.0000

140 0.00 179.64 0.00 93.15 0.0000 0.0000

150 0.00 179.64 0.00 93.15 0.0000 0.0000

160 0.00 179.64 0.00 93.15 0.0000 0.0000

170 0.00 179.64 0.00 93.15 0.0000 0.0000

180 0.00 179.64 0.00 93.15 0.0000 0.0000

190 0.00 179.63 0.00 93.15 0.0000 0.0000

220 0.00 179.63 0.00 93.15 0.0000 0.0000

230 0.00 179.63 0.00 93.15 0.0000 0.0000

Analysis of Load Case 7 : IP+OW+WI+FW+BW



10 7.44 127.80 61.55 0.0582




1

20 7.52 127.80 61.55 0.0588

30 8.12 127.80 61.55 0.0636

60 9.35 127.80 61.55 0.0732

70 11.04 127.80 61.55 0.0864

70 23.39 127.80 -23.71 61.55 0.1830 0.3852

80 25.04 127.80 -24.87 61.55 0.1959 0.4040

90 20.78 127.80 -19.44 61.55 0.1626 0.3159

100 17.02 127.80 -14.52 61.55 0.1332 0.2358

110 14.06 127.80 -10.96 61.55 0.1101 0.1781

140 12.40 127.80 -8.90 61.55 0.0970 0.1445

150 9.59 127.80 -5.42 61.55 0.0750 0.0880

160 7.45 127.80 -2.33 61.55 0.0583 0.0378

170 5.97 127.80 61.55 0.0467

180 8.00 127.80 61.55 0.0626

190 7.48 127.82 61.55 0.0585

220 7.39 127.82 61.55 0.0578

230 7.38 127.82 61.55 0.0577

Analysis of Load Case 8 : IP+OW+EQ+FS+BS



10 7.44 127.80 61.55 0.0582

20 7.51 127.80 61.55 0.0587

30 7.78 127.80 61.55 0.0609

60 8.19 127.80 61.55 0.0641

70 8.85 127.80 61.55 0.0692

70 12.80 127.80 -13.12 61.55 0.1001 0.2131

80 12.63 127.80 -12.46 61.55 0.0988 0.2025

90 11.01 127.80 -9.67 61.55 0.0862 0.1572

100 9.57 127.80 -7.07 61.55 0.0749 0.1148




1

110 8.28 127.80 -5.18 61.55 0.0648 0.0841

140 7.53 127.80 -4.02 61.55 0.0589 0.0654

150 6.14 127.80 -1.97 61.55 0.0480 0.0319

160 5.02 127.80 61.55 0.0393

170 4.17 127.80 61.55 0.0327

180 6.92 127.80 61.55 0.0542

190 7.18 127.82 61.55 0.0562

220 7.34 127.82 61.55 0.0574

230 7.36 127.82 61.55 0.0576

Analysis of Load Case 9 : EP+OW+WI+FW+BW



10 127.80 -2.67 61.55 0.0433

20 127.80 -2.62 61.55 0.0426

30 127.80 -2.93 61.55 0.0476

60 127.80 -3.55 61.55 0.0577

70 0.94 127.80 -4.34 61.55 0.0073 0.0704

70 13.29 127.80 -33.82 61.55 0.1040 0.5494

80 14.93 127.80 -34.98 61.55 0.1168 0.5682

90 10.67 127.80 -29.55 61.55 0.0835 0.4800

100 6.92 127.80 -24.62 61.55 0.0541 0.4000

110 3.96 127.80 -21.07 61.55 0.0310 0.3422

140 2.29 127.80 -19.00 61.55 0.0179 0.3087

150 127.80 -15.52 61.55 0.2522

160 127.80 -12.43 61.55 0.2020

170 127.80 -9.78 61.55 0.1588

180 127.80 -4.73 61.55 0.0768

190 127.82 -3.37 61.55 0.0547

220 127.82 -2.83 61.55 0.0460




1

230 127.82 -2.76 61.55 0.0448

Analysis of Load Case 10 : EP+OW+EQ+FS+BS



10 127.80 -2.67 61.55 0.0433

20 127.80 -2.61 61.55 0.0424

30 127.80 -2.59 61.55 0.0420

60 127.80 -2.38 61.55 0.0387

70 127.80 -2.14 61.55 0.0348

70 2.69 127.80 -23.22 61.55 0.0211 0.3773

80 2.52 127.80 -22.57 61.55 0.0197 0.3666

90 0.91 127.80 -19.78 61.55 0.0071 0.3213

100 127.80 -17.17 61.55 0.2790

110 127.80 -15.28 61.55 0.2483

140 127.80 -14.13 61.55 0.2295

150 127.80 -12.07 61.55 0.1961

160 127.80 -10.00 61.55 0.1624

170 127.80 -7.98 61.55 0.1297

180 127.80 -3.66 61.55 0.0594

190 127.82 -3.06 61.55 0.0498

220 127.82 -2.78 61.55 0.0452

230 127.82 -2.75 61.55 0.0446

Analysis of Load Case 11 : HP+HW+HI



10 10.22 179.64 93.15 0.0569

20 10.22 179.64 93.15 0.0569

30 10.22 179.64 93.15 0.0569




1

60 10.22 179.64 93.15 0.0569

70 10.22 179.64 93.15 0.0569

70 10.22 179.64 93.15 0.0569

80 10.22 179.64 93.15 0.0569

90 10.22 179.64 93.15 0.0569

100 10.22 179.64 93.15 0.0569

110 10.22 179.64 93.15 0.0569

140 10.22 179.64 93.15 0.0569

150 10.22 179.64 93.15 0.0569

160 10.22 179.64 93.15 0.0569

170 10.22 179.64 93.15 0.0569

180 10.22 179.64 93.15 0.0569

190 10.22 179.63 93.15 0.0569

220 10.22 179.63 93.15 0.0569

230 10.22 179.63 93.15 0.0569

Analysis of Load Case 12 : HP+HW+HE



10 10.22 179.64 93.15 0.0569

20 10.22 179.64 93.15 0.0569

30 10.22 179.64 93.15 0.0569

60 10.22 179.64 93.15 0.0569

70 10.22 179.64 93.15 0.0569

70 10.22 179.64 93.15 0.0569

80 10.22 179.64 93.15 0.0569

90 10.22 179.64 93.15 0.0569

100 10.22 179.64 93.15 0.0569

110 10.22 179.64 93.15 0.0569

140 10.22 179.64 93.15 0.0569




1

Analysis of Load Case 14 : IP+WF+CW



10 7.44 127.80 61.55 0.0582

20 7.50 127.80 61.55 0.0587

30 7.65 127.80 61.55 0.0599

60 7.96 127.80 61.55 0.0622

70 8.41 127.80 61.55 0.0658

70 127.80 -0.16 61.55 0.0026

80 0.08 127.80 61.55 0.0006

90 0.67 127.80 61.55 0.0052

100 1.25 127.80 61.55 0.0098

110 1.55 127.80 61.55 0.0121

140 1.75 127.80 61.55 0.0137

150 2.09 127.80 61.55 0.0163

160 2.56 127.80 61.55 0.0200

170 3.15 127.80 61.55 0.0246

180 6.69 127.80 61.55 0.0523

190 7.11 127.82 61.55 0.0556

220 7.33 127.82 61.55 0.0574

230 7.36 127.82 61.55 0.0576

Analysis of Load Case 15 : IP+VO+OW



10 7.44 127.80 61.55 0.0582

20 7.50 127.80 61.55 0.0587

30 7.74 127.80 61.55 0.0605

60 8.04 127.80 61.55 0.0629

70 8.49 127.80 61.55 0.0665




1

70 127.80 -0.19 61.55 0.0030

80 0.11 127.80 61.55 0.0008

90 0.69 127.80 61.55 0.0054

100 1.28 127.80 61.55 0.0100

110 1.56 127.80 61.55 0.0122

140 1.76 127.80 61.55 0.0137

150 2.09 127.80 61.55 0.0164

160 2.57 127.80 61.55 0.0201

170 3.15 127.80 61.55 0.0247

180 6.69 127.80 61.55 0.0524

190 7.11 127.82 61.55 0.0557

220 7.33 127.82 61.55 0.0574

230 7.36 127.82 61.55 0.0576

Analysis of Load Case 16 : IP+VE+EW



10 7.44 127.80 61.55 0.0582

20 7.50 127.80 61.55 0.0587

30 7.74 127.80 61.55 0.0605

60 8.04 127.80 61.55 0.0629

70 8.41 127.80 61.55 0.0658

70 0.50 127.80 61.55 0.0039

80 0.70 127.80 61.55 0.0055

90 1.18 127.80 61.55 0.0092

100 1.65 127.80 61.55 0.0129

110 1.89 127.80 61.55 0.0148

140 2.09 127.80 61.55 0.0164

150 2.38 127.80 61.55 0.0186

160 2.85 127.80 61.55 0.0223




1

170 3.33 127.80 61.55 0.0261

180 6.76 127.80 61.55 0.0529

190 7.11 127.82 61.55 0.0557

220 7.33 127.82 61.55 0.0574

230 7.36 127.82 61.55 0.0576

Analysis of Load Case 17 : NP+VO+OW



10 0.00 127.80 0.00 61.55 0.0000 0.0000

20 0.06 127.80 61.55 0.0005

30 0.30 127.80 61.55 0.0023

60 0.60 127.80 61.55 0.0047

70 1.05 127.80 61.55 0.0082

70 127.80 -7.63 61.55 0.1239

80 127.80 -7.38 61.55 0.1200

90 127.80 -6.80 61.55 0.1104

100 127.80 -6.21 61.55 0.1009

110 127.80 -5.89 61.55 0.0958

140 127.80 -5.70 61.55 0.0925

150 127.80 -5.36 61.55 0.0871

160 127.80 -4.88 61.55 0.0793

170 127.80 -4.30 61.55 0.0698

180 127.80 -0.76 61.55 0.0123

190 127.82 -0.34 61.55 0.0055

220 127.82 -0.11 61.55 0.0018

230 127.82 -0.08 61.55 0.0013

Analysis of Load Case 18 : FS+BS+IP+OW





1


10 7.44 127.80 61.55 0.0582

20 7.50 127.80 61.55 0.0587

30 7.74 127.80 61.55 0.0605

60 8.04 127.80 61.55 0.0629

70 8.49 127.80 61.55 0.0665

70 127.80 -0.19 61.55 0.0030

80 0.11 127.80 61.55 0.0008

90 0.69 127.80 61.55 0.0054

100 1.28 127.80 61.55 0.0100

110 1.56 127.80 61.55 0.0122

140 1.76 127.80 61.55 0.0137

150 2.09 127.80 61.55 0.0164

160 2.57 127.80 61.55 0.0201

170 3.15 127.80 61.55 0.0247

180 6.69 127.80 61.55 0.0524

190 7.11 127.82 61.55 0.0557

220 7.33 127.82 61.55 0.0574

230 7.36 127.82 61.55 0.0576

Analysis of Load Case 19 : FS+BS+EP+OW



10 127.80 -2.67 61.55 0.0433

20 127.80 -2.61 61.55 0.0424

30 127.80 -2.54 61.55 0.0413

60 127.80 -2.24 61.55 0.0363

70 127.80 -1.79 61.55 0.0290

70 127.80 -10.29 61.55 0.1672

80 127.80 -10.05 61.55 0.1632




1

90 127.80 -9.46 61.55 0.1537

100 127.80 -8.88 61.55 0.1442

110 127.80 -8.56 61.55 0.1390

140 127.80 -8.36 61.55 0.1358

150 127.80 -8.02 61.55 0.1304

160 127.80 -7.55 61.55 0.1226

170 127.80 -6.96 61.55 0.1131

180 127.80 -3.42 61.55 0.0556

190 127.82 -3.00 61.55 0.0488

220 127.82 -2.77 61.55 0.0451

230 127.82 -2.74 61.55 0.0446

Absolute Maximum of the all of the Stress Ratio's 0.5682

Governing Element: Shell-5

Governing Load Case 9 : EP+OW+WI+FW+BW




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Center of Gravity Calculation : Step: 22 3:23p Dec 18,2015

1

Shop/Field Installation Options :

Packing is installed in the Shop.

Insulation is installed in the Shop.

Note : The CG is computed from the first Element From Node

Center of Gravity of Packing 13597.805 mm.

Center of Gravity of Insulation 9926.966 mm.

Center of Gravity of Nozzles 9859.157 mm.

Center of Gravity of Lugs 5471.000 mm.

Center of Gravity of Bare Shell New and Cold 10136.275 mm.

Center of Gravity of Bare Shell Corroded 10136.275 mm.

Vessel CG in the Operating Condition 12482.876 mm.

Vessel CG in the Fabricated (Shop/Empty) Condition 12482.876 mm.




C-1023OT Distillation ColumnPV Elite 2012 Licensee: IBI CHEMATUR ENGINEERING & CONSULTANCY LTD.FileName : C-1023--------------------------------------------Sup. Lug Calcs: Ope : Lugs: 2 3:23p Dec 18,2015

1

Suppor t L ug Calcula t ions : Opera t ing Case

INPUT ECHO OF SUPPORT LUG INPUT

Type of Geometry : Gussets with Top Plate

Number of Support Lugs Nlug 4

Distance from Vessel OD to Lug Contact Point Dlug 300.0000 mm.

Lug Support Force Bearing Width Wfb 125.0000 mm.

Lug Material SA-516 70

Lug Yield Stress 221.20 N./mm²

Radial Width of bottom Support Lug Plate Wpl 350.0000 mm.

Effective Force Bearing Length Lpl 300.0000 mm.

Thickness of bottom Support Lug Plate Tpl 30.0000 mm.

Distance between Gussets Dgp 200.0000 mm.

Mean Width of Gusset Plate Wgp 170.0000 mm.

Height of Gusset Plate Hgp 252.0000 mm.

Thickness of Gusset Plate Tgp 25.0000 mm.

Radial Width of Top Bar Plate Wtp 150.0000 mm.

Thickness of Top Plate Ttp 25.0000 mm.

Pad Width along Circumference C11P 350.000 mm.

Pad Length along Vessel Axis C22P 400.000 mm.

Pad Thickness Tpad 10.000 mm.


Bolt Allowable Stress at Design Temperature 172.38 N./mm²

Thread Series TEMA Metric

Bolt Diameter 30.00 mm.




1

Results for Support Lugs: Description: SUPPORT LUG

Overturning Moment at Support Lug 19034. Kg-m.

Weight Load at the top of one Lug 7206. Kgf

Force on one Lug, Operating Condition [Flug]:

= ( W/Nlug + Mlug/( Rlug * Nlug/2 ) )

= ( 28824/4 + 19033/( 810.00 * 4/2 ))

= 18955.16 Kgf

Force on one lug in the Empty Condition [Flugemp]:

= ( -Wemp/Nlug + Mlugemp/( Rlug * Nlug/2 ) )

= ( -23767/4 + 19033/( 810.00 * 4/2 ))

= 5807.04 Kgf

Top Bar Plate Stress per Bednar p.154 [Stpl]:

= 0.75*( Flug*Dlug*Lpl )/( Ttp*Wtp²*Hgp )

= 0.75*( 18955 *300.000 *300.000 )/( 25.0000 *150.000²*252.000 )

= 88.52 N./mm²

Required Thickness of Top Plate 15.0070 mm.

Bottom Support Plate Bending Stress (Point Load) [Spl]:

= ( Flugemp/2*Dgp/2)/((Wpl/6)*Tpl²) (Uplift Condition)

= ( 5807/2*200.000/2)/((350.00/6)*30.0000²)

= 54.24 N./mm²

Bottom Plate Required Thickness (Point Load) 18.1939 mm.

Bottom Plate required thickness for Uplift per ADM S 3/4 [trUpl]:




1

= 0.72 * sqrt( Flugemp * Dgp / ( ( Wpl - dt ) * Spa ) )

= 0.72 * sqrt( 5807.0 * 200.00/( ( 350.00 - 33.17 ) * 147.463 ) )

= 11.24 mm.

Bearing Area [Ba]:

= Lpl * Wfb

= 300.000 * 125.000

= 375.00 cm²

Bending Stress in bottom Plate (Unif. Load) Per Bednar p.156 [Spl2]:

= Beta1 * Flug/Ba * Wfb² / Tpl² per Roark & Young 5th Ed.

= 1.475 * 18955.2/375.000 * 125.000²/30.000²

= 126.90 N./mm²

Bottom Plate Required Thickness (Uniform Load) 27.8301 mm.

Bottom Plate Required Thickness based on ADM S 3/4 [trAD]:

= 0.71 * Dgp * (( Flug / ( Lpl * Wfb ))/Spa )½

= 0.71*200.00*((18955/(300.00*125.00))/147.463)½

= 26.035 mm.

Note: If using the AD Code recommendations, the force bearing width (Wfb) must

be greater than or equal to 1/3 of the bottom plate radial width (Wpl)

plus the pad thickness (Padthk), if there is a pad.

Bottom Support Plate Allowable Stress [Spa]:

= 2/3 * Ylug

= 2/3 * 221

= 147.46 N./mm²




1

Input Echo, WRC107 Item 1, Description: SUPPORT LUG

Diameter Basis for Vessel Vbasis ID

Cylindrical or Spherical Vessel Cylsph Cylindrical

Internal Corrosion Allowance Cas 0.0000 mm.

Vessel Diameter Dv 1000.000 mm.

Vessel Thickness Tv 10.000 mm.

Design Temperature 220.00 C

Attachment Type Type Rectangular

Parameter C11 C11 200.00 mm.

Parameter C22 C22 252.00 mm.

Thickness of Reinforcing Pad Tpad 10.000 mm.

Pad Parameter C11P C11p 350.000 mm.

Pad Parameter C22P C22p 400.000 mm.

Design Internal Pressure Dp 3.000 bars

Include Pressure Thrust No

Vessel Centerline Direction Cosine Vx 0.000

Vessel Centerline Direction Cosine Vy 1.000

Vessel Centerline Direction Cosine Vz 0.000

Nozzle Centerline Direction Cosine Nx 1.000

Nozzle Centerline Direction Cosine Ny 0.000

Nozzle Centerline Direction Cosine Nz 0.000

Global Force (SUS) Fx 0.0 Kgf

Global Force (SUS) Fy 7206.1 Kgf




1

Global Force (SUS) Fz 0.0 Kgf

Global Moment (SUS) Mx 0.0 Kg-m.

Global Moment (SUS) My 0.0 Kg-m.

Global Moment (SUS) Mz 2161.9 Kg-m.

Internal Pressure (SUS) P 3.00 bars


Global Force (OCC) Fx 968.9 Kgf

Global Force (OCC) Fy 11749.0 Kgf

Global Force (OCC) Fz 0.0 Kgf

Global Moment (OCC) Mx 0.0 Kg-m.

Global Moment (OCC) My 290.7 Kg-m.

Global Moment (OCC) Mz 3524.8 Kg-m.

Occasional Internal Pressure (OCC) Pvar 0.00 bars

Use Interactive Control No

WRC107 Version Version March 1979

Include Pressure Stress Indices per Div. 2 No

Compute Pressure Stress per WRC-368 No

WRC 107 Stress Calculation for SUStained loads:

Radial Load P 0.0 Kgf

Circumferential Shear VC 0.0 Kgf

Longitudinal Shear VL 7206.1 Kgf

Circumferential Moment MC 0.0 Kg-m.




1

Longitudinal Moment ML -2161.9 Kg-m.

Torsional Moment MT 0.0 Kg-m.

Dimensionless Parameters used : Gamma = 25.50

Dimensionless Loads for Cylindrical Shells at Attachment Junction:

-------------------------------------------------------------------

Curves read for 1979 Beta Figure Value Location

-------------------------------------------------------------------

N(PHI) / ( P/Rm ) 0.249 4C 3.498 (A,B)

N(PHI) / ( P/Rm ) 0.249 3C 2.206 (C,D)

M(PHI) / ( P ) 0.213 2C1 0.043 (A,B)

M(PHI) / ( P ) 0.213 1C 0.073 (C,D)

N(PHI) / ( MC/(Rm**2 * Beta) ) 0.212 3A 1.045 (A,B,C,D)

M(PHI) / ( MC/(Rm * Beta) ) 0.234 1A 0.081 (A,B,C,D)

N(PHI) / ( ML/(Rm**2 * Beta) ) 0.229 3B 2.716 (A,B,C,D)

M(PHI) / ( ML/(Rm * Beta) ) 0.230 1B 0.027 (A,B,C,D)

N(x) / ( P/Rm ) 0.232 3C 2.358 (A,B)

N(x) / ( P/Rm ) 0.232 4C 3.606 (C,D)

M(x) / ( P ) 0.235 1C1 0.067 (A,B)

M(x) / ( P ) 0.235 2C ! 0.036 (C,D)

N(x) / ( MC/(Rm**2 * Beta) ) 0.212 4A 1.756 (A,B,C,D)

M(x) / ( MC/(Rm * Beta) ) 0.269 2A 0.035 (A,B,C,D)

N(x) / ( ML/(Rm**2 * Beta) ) 0.229 4B 1.024 (A,B,C,D)

M(x) / ( ML/(Rm * Beta) ) 0.246 2B 0.042 (A,B,C,D)

Note - The ! mark next to the figure name denotes curve value exceeded.




1

Stress Concentration Factors Kn = 1.00, Kb = 1.00

Stresses in the Vessel at the Attachment Junction

------------------------------------------------------------------------

| Stress Values at

Type of | (N./mm² )

---------------|--------------------------------------------------------

Stress Load| Au Al Bu Bl Cu Cl Du Dl

---------------|--------------------------------------------------------

Circ. Memb. P | 0 0 0 0 0 0 0 0

Circ. Bend. P | 0 0 0 0 0 0 0 0

Circ. Memb. MC | 0 0 0 0 0 0 0 0

Circ. Bend. MC | 0 0 0 0 0 0 0 0

Circ. Memb. ML | 42 42 -42 -42 0 0 0 0

Circ. Bend. ML | 72 -72 -72 72 0 0 0 0

|

Tot. Circ. Str.| 115.5 -29.7 -115.5 29.7 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Long. Memb. P | 0 0 0 0 0 0 0 0

Long. Bend. P | 0 0 0 0 0 0 0 0

Long. Memb. MC | 0 0 0 0 0 0 0 0

Long. Bend. MC | 0 0 0 0 0 0 0 0

Long. Memb. ML | 18 18 -18 -18 0 0 0 0

Long. Bend. ML | 105 -105 -105 105 0 0 0 0

|

Tot. Long. Str.| 124.6 -87.3 -124.6 87.3 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 -7 -7 7 7




1

Shear MT | 0 0 0 0 0 0 0 0

|

Tot. Shear| 0.0 0.0 0.0 0.0 -7.0 -7.0 7.0 7.0

------------------------------------------------------------------------

Str. Int. | 124.56 87.34 124.56 87.34 14.02 14.02 14.02 14.02

------------------------------------------------------------------------


Dimensionless Loads for Cylindrical Shells at Pad edge:

-------------------------------------------------------------------


-------------------------------------------------------------------

N(PHI) / ( P/Rm ) 0.400 4C 3.948 (A,B)

N(PHI) / ( P/Rm ) 0.400 3C 1.504 (C,D)

M(PHI) / ( P ) 0.363 2C1 0.009 (A,B)

M(PHI) / ( P ) 0.363 1C ! 0.065 (C,D)





N(x) / ( P/Rm ) 0.383 3C 1.626 (A,B)

N(x) / ( P/Rm ) 0.383 4C 4.140 (C,D)

M(x) / ( P ) 0.386 1C1 0.020 (A,B)

M(x) / ( P ) 0.386 2C ! 0.033 (C,D)








1



Stresses in the Vessel at the Edge of Reinforcing Pad

------------------------------------------------------------------------

| Stress Values at


---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Memb. P | 0 0 0 0 0 0 0 0

Circ. Bend. P | 0 0 0 0 0 0 0 0

Circ. Memb. MC | 0 0 0 0 0 0 0 0

Circ. Bend. MC | 0 0 0 0 0 0 0 0

Circ. Memb. ML | 47 47 -47 -47 0 0 0 0

Circ. Bend. ML | 39 -39 -39 39 0 0 0 0

|

Tot. Circ. Str.| 87.3 7.6 -87.3 -7.6 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Long. Memb. P | 0 0 0 0 0 0 0 0

Long. Bend. P | 0 0 0 0 0 0 0 0

Long. Memb. MC | 0 0 0 0 0 0 0 0

Long. Bend. MC | 0 0 0 0 0 0 0 0

Long. Memb. ML | 29 29 -29 -29 0 0 0 0

Long. Bend. ML | 53 -53 -53 53 0 0 0 0

|

Tot. Long. Str.| 83.6 -24.1 -83.6 24.1 0.0 0.0 0.0 0.0




2

Circ. Memb. MC | 0 0 0 0 2 2 -2 -2

Circ. Bend. MC | 0 0 0 0 28 -28 -28 28

Circ. Memb. ML | 69 69 -69 -69 0 0 0 0

Circ. Bend. ML | 118 -118 -118 118 0 0 0 0

|

Tot. Circ. Str.| 178.9 -45.6 -197.6 51.2 18.7 -18.4 -43.6 35.0

------------------------------------------------------------------------

Long. Memb. P | -2 -2 -2 -2 -3 -3 -3 -3

Long. Bend. P | -9 9 -9 9 -5 5 -5 5

Long. Memb. MC | 0 0 0 0 3 3 -3 -3

Long. Bend. MC | 0 0 0 0 10 -10 -10 10

Long. Memb. ML | 30 30 -30 -30 0 0 0 0

Long. Bend. ML | 172 -172 -172 172 0 0 0 0

|

Tot. Long. Str.| 191.3 -135.0 -214.9 149.8 6.2 -5.2 -23.2 8.7

------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 -11 -11 11 11

Shear MT | 0 0 0 0 0 0 0 0

|

Tot. Shear| 0.0 0.0 0.0 0.0 -11.4 -11.4 11.4 11.4

------------------------------------------------------------------------

Str. Int. | 191.30 135.01 214.86 149.79 26.05 26.39 48.70 39.29

------------------------------------------------------------------------




------------------------------------------------------------------------




2

| Stress Values at


---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Memb. P | -7 -7 -7 -7 -2 -2 -2 -2

Circ. Bend. P | -5 5 -5 5 -37 37 -37 37

Circ. Memb. MC | 0 0 0 0 3 3 -3 -3

Circ. Bend. MC | 0 0 0 0 49 -49 -49 49

Circ. Memb. ML | 77 77 -77 -77 0 0 0 0

Circ. Bend. ML | 64 -64 -64 64 0 0 0 0

|

Tot. Circ. Str.| 129.8 9.9 -154.8 -14.7 12.6 -11.3 -92.7 80.0

------------------------------------------------------------------------

Long. Memb. P | -3 -3 -3 -3 -7 -7 -7 -7

Long. Bend. P | -11 11 -11 11 -19 19 -19 19

Long. Memb. MC | 0 0 0 0 13 13 -13 -13

Long. Bend. MC | 0 0 0 0 17 -17 -17 17

Long. Memb. ML | 48 48 -48 -48 0 0 0 0

Long. Bend. ML | 87 -87 -87 87 0 0 0 0

|

Tot. Long. Str.| 121.8 -31.0 -150.6 47.5 3.7 6.9 -57.4 15.7

------------------------------------------------------------------------

Shear VC | 0 0 0 0 0 0 0 0

Shear VL | 0 0 0 0 -14 -14 14 14

Shear MT | 0 0 0 0 0 0 0 0

|

Tot. Shear| 0.0 0.0 0.0 0.0 -14.4 -14.4 14.4 14.4

------------------------------------------------------------------------

Str. Int. | 129.79 40.93 154.75 62.20 30.17 34.08 97.80 83.09




2

------------------------------------------------------------------------

WRC 107 Stress Summations:

Vessel Stress Summation at Attachment Junction

------------------------------------------------------------------------

Type of | Stress Values at

Stress Int. | (N./mm² )

---------------|--------------------------------------------------------

Location | Au Al Bu Bl Cu Cl Du Dl

---------------|--------------------------------------------------------

Circ. Pm (SUS) | 7 7 7 7 7 7 7 7

Circ. Pm (OCC) | 0 0 0 0 0 0 0 0

Circ. Pm(TOTAL)| 7.4 7.7 7.4 7.7 7.4 7.7 7.4 7.7

Circ. Pl (SUS) | 42 42 -42 -42 0 0 0 0

Circ. Pl (OCC) | 66 66 -73 -73 0 0 -4 -4

Circ. Pl(TOTAL)| 109.5 109.5 -116.1 -116.1 0.2 0.2 -4.3 -4.3

Circ. Q (SUS) | 72 -72 -72 72 0 0 0 0

Circ. Q (OCC) | 112 -112 -124 124 18 -18 -39 39

Circ. Q (TOTAL)| 184.8 -184.8 -197.0 197.0 18.5 -18.5 -39.3 39.3

------------------------------------------------------------------------

Long. Pm (SUS) | 3 3 3 3 3 3 3 3

Long. Pm (OCC) | 0 0 0 0 0 0 0 0

Long. Pm(TOTAL)| 3.7 3.7 3.7 3.7 3.7 3.7 3.7 3.7

Long. Pl (SUS) | 18 18 -18 -18 0 0 0 0

Long. Pl (OCC) | 28 28 -32 -32 0 0 -7 -7

Long. Pl(TOTAL)| 46.8 46.8 -51.1 -51.1 0.5 0.5 -7.2 -7.2

Long. Q (SUS) | 105 -105 -105 105 0 0 0 0

Long. Q (OCC) | 163 -163 -182 182 5 -5 -15 15

Long. Q (TOTAL)| 269.1 -269.1 -288.3 288.3 5.7 -5.7 -16.0 16.0




2

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pm (OCC) | 0 0 0 0 0 0 0 0

Shear Pm(TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0

Shear Pl (SUS) | 0 0 0 0 -7 -7 7 7

Shear Pl (OCC) | 0 0 0 0 -11 -11 11 11

Shear Pl(TOTAL)| 0.0 0.0 0.0 0.0 -18.4 -18.4 18.4 18.4

Shear Q (SUS) | 0 0 0 0 0 0 0 0

Shear Q (OCC) | 0 0 0 0 0 0 0 0

Shear Q (TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Pm (SUS) | 7.4 7.7 7.4 7.7 7.4 7.7 7.4 7.7

------------------------------------------------------------------------

Pm (SUS+OCC) | 7.4 7.7 7.4 7.7 7.4 7.7 7.4 7.7

------------------------------------------------------------------------

Pm+Pl (SUS) | 50.2 50.5 35.5 35.2 14.5 14.6 14.5 14.6

------------------------------------------------------------------------

Pm+Pl (SUS+OCC)| 116.9 117.2 108.7 108.4 37.0 37.1 37.5 37.5

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 319.5 218.7 335.7 240.8 40.3 38.0 48.1 51.4

------------------------------------------------------------------------

------------------------------------------------------------------------

Type of | Max. S.I. S.I. Allowable | Result

Stress Int. | N./mm² |

---------------|--------------------------------------------------------

Pm (SUS) | 7.65 106.50 | Passed

Pm (SUS+OCC) | 7.65 127.80 | Passed

Pm+Pl (SUS) | 50.54 159.75 | Passed

Pm+Pl (SUS+OCC)| 117.19 191.70 | Passed




2

Pm+Pl+Q (TOTAL)| 335.74 332.40 | Failed

------------------------------------------------------------------------


Vessel Stress Summation at Reinforcing Pad Edge

------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Pm (SUS) | 14 15 14 15 14 15 14 15

Circ. Pm (OCC) | 0 0 0 0 0 0 0 0

Circ. Pm(TOTAL)| 14.9 15.2 14.9 15.2 14.9 15.2 14.9 15.2

Circ. Pl (SUS) | 47 47 -47 -47 0 0 0 0

Circ. Pl (OCC) | 69 69 -84 -84 0 0 -6 -6

Circ. Pl(TOTAL)| 117.3 117.3 -132.1 -132.1 0.7 0.7 -6.3 -6.3

Circ. Q (SUS) | 39 -39 -39 39 0 0 0 0

Circ. Q (OCC) | 59 -59 -70 70 11 -11 -86 86

Circ. Q (TOTAL)| 99.8 -99.8 -109.9 109.9 12.0 -12.0 -86.3 86.3

------------------------------------------------------------------------

Long. Pm (SUS) | 7 7 7 7 7 7 7 7

Long. Pm (OCC) | 0 0 0 0 0 0 0 0

Long. Pm(TOTAL)| 7.4 7.4 7.4 7.4 7.4 7.4 7.4 7.4

Long. Pl (SUS) | 29 29 -29 -29 0 0 0 0

Long. Pl (OCC) | 45 45 -51 -51 5 5 -20 -20

Long. Pl(TOTAL)| 75.2 75.2 -81.3 -81.3 5.3 5.3 -20.9 -20.9

Long. Q (SUS) | 53 -53 -53 53 0 0 0 0

Long. Q (OCC) | 76 -76 -99 99 -1 1 -36 36




2

Long. Q (TOTAL)| 130.2 -130.2 -152.9 152.9 -1.6 1.6 -36.5 36.5

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pm (OCC) | 0 0 0 0 0 0 0 0

Shear Pm(TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0

Shear Pl (SUS) | 0 0 0 0 -8 -8 8 8

Shear Pl (OCC) | 0 0 0 0 -14 -14 14 14

Shear Pl(TOTAL)| 0.0 0.0 0.0 0.0 -23.2 -23.2 23.2 23.2

Shear Q (SUS) | 0 0 0 0 0 0 0 0

Shear Q (OCC) | 0 0 0 0 0 0 0 0

Shear Q (TOTAL)| 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0

------------------------------------------------------------------------

Pm (SUS) | 14.9 15.2 14.9 15.2 14.9 15.2 14.9 15.2

------------------------------------------------------------------------

Pm (SUS+OCC) | 14.9 15.2 14.9 15.2 14.9 15.2 14.9 15.2

------------------------------------------------------------------------

Pm+Pl (SUS) | 62.3 62.6 32.6 32.3 20.7 20.9 20.7 20.9

------------------------------------------------------------------------

Pm+Pl (SUS+OCC)| 132.1 132.4 117.3 117.0 46.6 46.6 51.4 51.5

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 231.9 80.3 227.2 86.1 49.3 47.6 91.0 102.0

------------------------------------------------------------------------

------------------------------------------------------------------------



---------------|--------------------------------------------------------

Pm (SUS) | 15.15 106.50 | Passed

Pm (SUS+OCC) | 15.15 127.80 | Passed

Pm+Pl (SUS) | 62.56 159.75 | Passed




2

Pm+Pl (SUS+OCC)| 132.43 191.70 | Passed

Pm+Pl+Q (TOTAL)| 231.91 332.40 | Passed

------------------------------------------------------------------------





Nozzle Calcs. : N03 Nozl: 10 3:23p Dec 18,2015

2

INPUT VALUES, Nozzle Description: N03 From : 10

Pressure for Reinforcement Calculations P 3.000 bars

Temperature for Internal Pressure Temp 220 C

Design External Pressure Pext 1.03 bars

Temperature for External Pressure Tempex 220 C

Shell Material SA-240 316L

Shell Allowable Stress at Temperature S 106.50 N./mm²

Shell Allowable Stress At Ambient Sa 115.10 N./mm²

Inside Diameter of Elliptical Head D 1000.00 mm.

Aspect Ratio of Elliptical Head Ar 2.00

Head Finished (Minimum) Thickness t 10.0000 mm.

Head Internal Corrosion Allowance c 0.0000 mm.

Head External Corrosion Allowance co 0.0000 mm.

Distance from Head Centerline L1 1.0000 mm.

User Entered Minimum Design Metal Temperature -5.00 C

Type of Element Connected to the Shel l : Nozzle

Material SA-312 TP316

Material UNS Number S31600

Material Specification/Type Wld. pipe

Allowable Stress at Temperature Sn 110.96 N./mm²

Allowable Stress At Ambient Sna 117.22 N./mm²





2

Diameter Basis (for tr calc only) ID

Layout Angle 0.00 deg

Diameter 200.0000 mm.

Size and Thickness Basis Nominal

Nominal Thickness tn 10S

Flange Material SA-182 F316

Flange Type Weld Neck Flange

Corrosion Allowance can 0.0000 mm.

Joint Efficiency of Shell Seam at Nozzle E1 1.00

Joint Efficiency of Nozzle Neck En 1.00

Outside Projection ho 200.0000 mm.

Weld leg size between Nozzle and Pad/Shell Wo 9.5250 mm.

Groove weld depth between Nozzle and Vessel Wgnv 6.0000 mm.

Inside Projection h 8.0000 mm.

Weld leg size, Inside Element to Shell Wi 0.0000 mm.

Pad Material SA-240 316L

Pad Allowable Stress at Temperature Sp 106.52 N./mm²

Pad Allowable Stress At Ambient Spa 115.15 N./mm²

Diameter of Pad along vessel surface Dp 319.0750 mm.

Thickness of Pad te 4.0000 mm.

Weld leg size between Pad and Shell Wp 3.0000 mm.

Groove weld depth between Pad and Nozzle Wgpn 4.0000 mm.

Reinforcing Pad Width 50.0000 mm.

ASME Code Weld Type per UW-16 None





2

Class of attached Flange 150

Grade of attached Flange GR 2.2

The Pressure Design option was Design Pressure + static head.

Nozzle Sketch (may not represent actual weld type/configuration)

| |

| |

| |

| |

__________/| |

____/|__________\| |

| \ | |

| \ | |

|________________\| |

\| |

|__|

Insert Nozzle With Pad, with Inside projection

Reinforcement CALCULATION, Description: N03

ASME Code, Section VIII, Division 1, 2010, 2011a, UG-37 to UG-45

Actual Inside Diameter Used in Calculation 211.557 mm.

Actual Thickness Used in Calculation 3.759 mm.

Nozzle input data check completed without errors.





2

Reqd thk per UG-37(a)of Elliptical Head, Tr [Int. Press]

= (P*K1*D))/(2*S*E-0.2*P) per UG-37(a)(3)

= (3.00*0.900*1000.0000)/(2 *106.50*1.00-0.2*3.00)

= 1.2680 mm.

Reqd thk per UG-37(a)of Nozzle Wall, Trn [Int. Press]

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*105.78)/(110*1.00-0.6*3.00)

= 0.2865 mm.

Required Nozzle thickness under External Pressure per UG-28 : 0.7109 mm.

UG-40, Limits of Reinforcement : [Internal Pressure]

Parallel to Vessel Wall (Diameter Limit) Dl 423.1132 mm.

Parallel to Vessel Wall, opening length d 211.5566 mm.

Normal to Vessel Wall (Thickness Limit), pad side Tlwp 13.3980 mm.

Normal to Vessel Wall, Inward 8.0000 mm.

Weld Strength Reduction Factor [fr1]:

= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sp/S )





2

= min( 1, 106.5/106.5 )

= 1.000


= min( fr2, fr4 )

= min( 1.0 , 1.0 )

= 1.000

Results of Nozzle Reinforcement Area Calculations:

AREA AVAILABLE, A1 to A5 Design External Mapnc

Area Required Ar 2.683 2.943 NA cm²

Area in Shell A1 18.473 15.269 NA cm²

Area in Nozzle Wall A2 0.931 0.817 NA cm²

Area in Inward Nozzle A3 0.601 0.601 NA cm²

Area in Welds A41+A42+A43 0.997 0.997 NA cm²

Area in Element A5 3.000 3.000 NA cm²

TOTAL AREA AVAILABLE Atot 24.002 20.684 NA cm²

The External Pressure Case Governs the Analysis.

Nozzle Angle Used in Area Calculations 90.00 Degs.

The area available without a pad is Sufficient.

The area available with the given pad is Sufficient.

Area Required [A]:

= 0.5( d * tr*F + 2 * tn * tr*F * (1-fr1) ) per UG-37(d) or UG-39

= 0.5(211.5566*2.7825*1+2*3.7592*2.7825*1*(1-1.00))

= 2.943 cm²





2

Reinforcement Areas per Figure UG-37.1

Area Available in Shell [A1]:

= d( E1*t - F*tr ) - 2 * tn( E1*t - F*tr ) * ( 1 - fr1 )

= 211.557 ( 1.00 * 10.0000 - 1.0 * 2.783 ) - 2 * 3.759

( 1.00 * 10.0000 - 1.0 * 2.7825 ) * ( 1 - 1.000 )

= 15.269 cm²

Area Available in Nozzle Wall Projecting Outward [A2]:

= ( 2 * Tlwp ) * ( tn - trn ) * fr2

= ( 2 * 13.40 ) * ( 3.76 - 0.71 ) * 1.0000

= 0.817 cm²

Area Available in Inward Nozzle [A3]:

= 2 * ti * min( h, Tl, 2.5 * ti) * fr2

= 2 * 3.7592 * ( 8.0000 ) * 1.0000

= 0.601 cm²

Area Available in Welds [A41 + A42 + A43]:

= (Wo² - Ar Lost)*Fr3+((Wi-can/0.707)² - Ar Lost)*fr2 + Wp²*fr4

= (0.9071 ) * 1.00 + (0.0000 ) * 1.00 + 9.0000² * 1.00

= 0.997 cm²

Area Available in Element [A5]:

= (min(Dp,DL)-(Nozzle OD))*(min(tp,Tlwp,te))*fr4

= ( 319.0750 - 219.0750 ) * 4.0000 * 1.0000

= 3.000 cm²

Note: Per user request, A5 multiplied by 0.75, see UG-37(h).





2

UG-45 Minimum Nozzle Neck Thickness Requirement: [Int. Press.]

Wall Thickness for Internal/External pressures ta = 0.7109 mm.

Wall Thickness per UG16(b), tr16b = 1.5000 mm.

Wall Thickness, shell/head, internal pressure trb1 = 1.4089 mm.

Wall Thickness tb1 = max(trb1, tr16b) = 1.5000 mm.

Wall Thickness, shell/head, external pressure trb2 = 0.4858 mm.


Wall Thickness per table UG-45 tb3 = 7.1600 mm.

Determine Nozzle Thickness candidate [tb]:

= min[ tb3, max( tb1,tb2) ]

= min[ 7.160 , max( 1.500 , 1.500 ) ]

= 1.5000 mm.

Minimum Wall Thickness of Nozzle Necks [tUG-45]:

= max( ta, tb )

= max( 0.7109 , 1.5000 )

= 1.5000 mm.

Available Nozzle Neck Thickness = 0.875 * 3.759 = 3.289 mm. --> OK

Stresses on Nozzle due to External and Pressure L oads per th e ASME

B31.3 Pipi ng Co de (see 319.4.4 and 302.3.5):

Sustained : 59.7, Allowable : 111.0 N./mm² Passed

Expansion : 0.0, Allowable : 225.5 N./mm² Passed

Occasional : 4.1, Allowable : 147.6 N./mm² Passed

Shear : 41.6, Allowable : 77.7 N./mm² Passed

Note : The number of cycles on this nozzle was assumed to be 7000 or less for

the determination of the expansion stress allowable.





2

Weld Size Calculations, Description: N03

Intermediate Calc. for nozzle/shell Welds Tmin 3.7592 mm.

Intermediate Calc. for pad/shell Welds TminPad 4.0000 mm.

Intermediate Calc. for Inward Weld TminIns 3.7592 mm.

Results Per UW-16.1:

Required Thickness Actual Thickness

Nozzle Weld 2.6314 = 0.7 * tmin. 6.7342 = 0.7 * Wo mm.

Pad Weld 2.0000 = 0.5*TminPad 2.1210 = 0.7 * Wp mm.

Inward Weld 2.6314 = 0.7 * TMinIn 0.0000 = 0.7 * Wi-Can mm.

Weld Strength and Weld Loads per UG-41.1, Sketch (a) or (b)

Weld Load [W]:

= (A-A1+2*tn*fr1*(E1*t-tr))*Sv

= (2.9433 - 15.2690 + 2 * 3.7592 * 1.0000 *

(1.00 * 10.0000 - 2.7825 ) ) * 106

= 0.00 Kgf

Note: F is always set to 1.0 throughout the calculation.

Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv

= ( 0.8168 + 3.0000 + 0.9971 - 0.0000 * 1.00 ) * 106

= 5227.82 Kgf

Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv

= ( 0.8168 + 0.6015 + 0.9071 + ( 0.7518 ) ) * 106





2

= 3341.81 Kgf

Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S

= ( 0.8168 + 0.6015 + 0.9971 + 3.0000 + ( 0.7518 ) ) * 106

= 6697.48 Kgf

Strength of Connection Elements for Failure Path Analysis

Shear, Outward Nozzle Weld [Sonw]:

= (pi/2) * Dlo * Wo * 0.49 * Snw

= ( 3.1416/2.0 ) * 219.0750 * 9.5250 * 0.49 * 106

= 17445. Kgf

Shear, Pad Element Weld [Spew]:

= (pi/2) * DP * WP * 0.49 * SEW

= ( 3.1416/2.0 ) * 319.0750 * 3.0000 * 0.49 * 106

= 8001. Kgf

Shear, Nozzle Wall [Snw]:

= (pi *( Dlr + Dlo )/4 ) * ( Thk - Can ) * 0.7 * Sn

= (3.1416 * 107.6579 ) * ( 3.7592 - 0.0000 ) * 0.7 * 110

= 10070. Kgf

Tension, Pad Groove Weld [Tpgw]:

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg

= (3.1416/2 ) * 219.0750 * 4.0000 * 0.74 * 110

= 11525. Kgf

Tension, Shell Groove Weld [Tngw]:





2

= (pi/2) * Dlo * (Wgnvi-Cas) * 0.74 * Sng

= ( 3.1416/2.0 ) * 219.0750 * ( 6.0000 - 0.0000 ) * 0.74 * 110

= 17287. Kgf

Strength of Failure Paths:

PATH11 = ( SPEW + SNW ) = ( 8001 + 10069 ) = 18070 Kgf

PATH22 = ( Sonw + Tpgw + Tngw + Sinw )

= ( 17444 + 11524 + 17287 + 0 ) = 46256 Kgf

PATH33 = ( Spew + Tngw + Sinw )

= ( 8001 + 17287 + 0 ) = 25288 Kgf

Summary of Failure Path Calculations:

Path 1-1 = 18070 Kgf, must exceed W = 0 Kgf or W1 = 5227 Kgf



Maximum Allowable Pressure for this Nozzle at this Location:

Converged Max. Allow. Pressure in Operating case 5.160 bars

Note: The MAWP of this junction was limited by the parent Shell/Head.

Nozzle is O.K. for the External Pressure 1.035 bars

The Drop for this Nozzle is : 6.6313 mm.

The Cut Length for this Nozzle is, Drop + Ho + H + T : 218.0000 mm.

Input Echo, WRC107 Item 1, Description: N03 :






2

Cylindrical or Spherical Vessel Cylsph Spherical





Vessel Material SA-240 316L

Vessel Cold S.I. Allowable Smc 115.10 N./mm²

Vessel Hot S.I. Allowable Smh 106.50 N./mm²

Attachment Type Type Round

WRC107 Attachment Classification Holsol Hollow

Diameter Basis for Nozzle Nbasis ID

Corrosion Allowance for Nozzle Can 0.0000 mm.

Nozzle Diameter Dn 211.557 mm.

Nozzle Thickness Tn 3.759 mm.

Nozzle Material SA-312 TP316

Nozzle Cold S.I. Allowable SNmc 117.22 N./mm²

Nozzle Hot S.I. Allowable SNmh 110.96 N./mm²


Diameter of Reinforcing Pad Dpad 319.075 mm.



External Forces and Moments in WRC 107 Convention:

Radial Load (SUS) P -1020.0 Kgf

Longitudinal Shear (SUS) (Vl) V1 1020.0 Kgf





2

Circumferential Shear (SUS) (Vc) V2 1020.0 Kgf

Circumferential Moment (SUS) (Mc) M1 490.0 Kg-m.

Longitudinal Moment (SUS) (Ml) M2 653.0 Kg-m.

Torsional Moment (SUS) Mt 816.0 Kg-m.






Radial Load P -1020.0 Kgf

Circumferential Shear (VC) V2 1020.0 Kgf

Longitudinal Shear (VL) V1 1020.0 Kgf

Circumferential Moment (MC) M1 490.0 Kg-m.

Longitudinal Moment (ML) M2 653.0 Kg-m.


Dimensionless Param: U = 0.97 TAU = 28.64 RHO = 4.00 ( 3.72)

Dimensionless Loads for Spherical Shells at Attachment Junction:

------------------------------------------------------------

Curves read for 1979 Figure Value Location

------------------------------------------------------------

N(x) * T / P SP 7 0.02168 (A,B,C,D)

M(x) / P SP 7 0.01015 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / MC SM 7 0.03733 (A,B,C,D)

M(x) * SQRT(Rm * T ) / MC SM 7 0.01891 (A,B,C,D)





2

N(x) * T * SQRT(Rm * T ) / ML SM 7 0.03733 (A,B,C,D)

M(x) * SQRT(Rm * T ) / ML SM 7 0.01891 (A,B,C,D)

N(y) * T / P SP 7 0.21681 (A,B,C,D)

M(y) / P SP 7 0.02755 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / MC SM 7 0.27592 (A,B,C,D)

M(y) * SQRT(Rm * T ) / MC SM 7 0.06375 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / ML SM 7 0.27592 (A,B,C,D)

M(y) * SQRT(Rm * T ) / ML SM 7 0.06375 (A,B,C,D)



------------------------------------------------------------------------

| Stress Values at


---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Memb. P | 1 1 1 1 1 1 1 1

Rad. Bend. P | 3 -3 3 -3 3 -3 3 -3

Rad. Memb. MC | 0 0 0 0 -8 -8 8 8

Rad. Bend. MC | 0 0 0 0 -24 24 24 -24

Rad. Memb. ML | -10 -10 10 10 0 0 0 0

Rad. Bend. ML | -32 32 32 -32 0 0 0 0

|

Tot. Rad. Str.| -39.5 20.1 47.9 -24.1 -28.6 14.6 37.0 -18.6

------------------------------------------------------------------------

Tang. Memb. P | 11 11 11 11 11 11 11 11

Tang. Bend. P | 8 -8 8 -8 8 -8 8 -8





2

Tang. Memb. MC | 0 0 0 0 -60 -60 60 60

Tang. Bend. MC | 0 0 0 0 -83 83 83 -83

Tang. Memb. ML | -79 -79 79 79 0 0 0 0

Tang. Bend. ML | -110 110 110 -110 0 0 0 0

|

Tot. Tang. Str.| -171.4 33.5 210.4 -28.3 -123.8 25.8 162.8 -20.6

------------------------------------------------------------------------

Shear VC | 2 2 -2 -2 0 0 0 0

Shear VL | 0 0 0 0 -2 -2 2 2

Shear MT | 7 7 7 7 7 7 7 7

|

Tot. Shear| 9.7 9.7 5.5 5.5 5.5 5.5 9.7 9.7

------------------------------------------------------------------------

Str. Int. | 172.11 38.58 210.60 32.07 124.07 28.07 163.49 29.27

------------------------------------------------------------------------

Unitless Prm: U = 1.68 TAU = 0.00 ( 41.94) RHO = 0.00 ( 2.66)

Dimensionless Loads for Spherical Shells at Pad edge:

------------------------------------------------------------


------------------------------------------------------------

N(x) * T / P SR 2 0.03232 (A,B,C,D)

M(x) / P SR 2 0.01560 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / MC SR 3 0.03057 (A,B,C,D)

M(x) * SQRT(Rm * T ) / MC SR 3 0.02132 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / ML SR 3 0.03057 (A,B,C,D)

M(x) * SQRT(Rm * T ) / ML SR 3 0.02132 (A,B,C,D)

N(y) * T / P SR 2 0.00964 (A,B,C,D)





2

M(y) / P SR 2 0.00468 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / MC SR 3 0.00917 (A,B,C,D)

M(y) * SQRT(Rm * T ) / MC SR 3 0.00629 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / ML SR 3 0.00917 (A,B,C,D)

M(y) * SQRT(Rm * T ) / ML SR 3 0.00629 (A,B,C,D)



------------------------------------------------------------------------

| Stress Values at


---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Memb. P | 3 3 3 3 3 3 3 3

Rad. Bend. P | 9 -9 9 -9 9 -9 9 -9

Rad. Memb. MC | 0 0 0 0 -15 -15 15 15

Rad. Bend. MC | 0 0 0 0 -64 64 64 -64

Rad. Memb. ML | -20 -20 20 20 0 0 0 0

Rad. Bend. ML | -86 86 86 -86 0 0 0 0

|

Tot. Rad. Str.| -94.1 59.4 119.3 -71.7 -67.5 43.1 92.7 -55.3

------------------------------------------------------------------------

Tang. Memb. P | 0 0 0 0 0 0 0 0

Tang. Bend. P | 2 -2 2 -2 2 -2 2 -2

Tang. Memb. MC | 0 0 0 0 -4 -4 4 4

Tang. Bend. MC | 0 0 0 0 -19 19 19 -19

Tang. Memb. ML | -6 -6 6 6 0 0 0 0

Tang. Bend. ML | -25 25 25 -25 0 0 0 0





2

|

Tot. Tang. Str.| -27.8 17.4 35.4 -21.1 -19.9 12.6 27.5 -16.3

------------------------------------------------------------------------

Shear VC | 1 1 -1 -1 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

Shear MT | 5 5 5 5 5 5 5 5

|

Tot. Shear| 7.0 7.0 3.0 3.0 3.0 3.0 7.0 7.0

------------------------------------------------------------------------

Str. Int. | 94.84 60.55 119.41 71.86 67.66 43.35 93.41 56.54

------------------------------------------------------------------------



------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Pm (SUS) | 9 9 9 9 9 9 9 9

Rad. Pl (SUS) | -9 -9 11 11 -7 -7 9 9

Rad. Q (SUS) | -29 29 35 -35 -21 21 27 -27

------------------------------------------------------------------------

Long. Pm (SUS) | 9 9 9 9 9 9 9 9

Long. Pl (SUS) | -68 -68 91 91 -48 -48 71 71

Long. Q (SUS) | -102 102 119 -119 -74 74 91 -91

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0





2

Shear Pl (SUS) | 2 2 -2 -2 -2 -2 2 2

Shear Q (SUS) | 7 7 7 7 7 7 7 7

------------------------------------------------------------------------

Pm (SUS) | 9.6 9.6 9.6 9.6 9.6 9.6 9.6 9.6

------------------------------------------------------------------------

Pm+Pl (SUS) | 59.4 59.4 100.8 100.8 42.2 42.2 80.8 80.8

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 162.5 48.2 220.2 22.4 114.4 37.7 173.1 19.6

------------------------------------------------------------------------

------------------------------------------------------------------------



---------------|--------------------------------------------------------

Pm (SUS) | 9.64 106.50 | Passed

Pm+Pl (SUS) | 100.76 159.75 | Passed


------------------------------------------------------------------------



------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Pm (SUS) | 13 13 13 13 13 13 13 13

Rad. Pl (SUS) | -17 -17 23 23 -12 -12 18 18





2

Rad. Q (SUS) | -76 76 95 -95 -55 55 73 -73

------------------------------------------------------------------------

Long. Pm (SUS) | 13 13 13 13 13 13 13 13

Long. Pl (SUS) | -5 -5 7 7 -3 -3 5 5

Long. Q (SUS) | -22 22 28 -28 -16 16 21 -21

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1

Shear Q (SUS) | 5 5 5 5 5 5 5 5

------------------------------------------------------------------------

Pm (SUS) | 13.5 13.5 13.5 13.5 13.5 13.5 13.5 13.5

------------------------------------------------------------------------

Pm+Pl (SUS) | 12.8 12.8 37.5 37.5 10.3 10.3 32.5 32.5

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 81.3 74.1 132.9 58.4 54.2 56.8 106.9 43.0

------------------------------------------------------------------------

------------------------------------------------------------------------



---------------|--------------------------------------------------------

Pm (SUS) | 13.50 106.50 | Passed

Pm+Pl (SUS) | 37.55 159.75 | Passed


------------------------------------------------------------------------






2


























2





| |

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__________/| |

____/|__________\| |

| \ | |

| \ | |

|________________\| |

\| |

|__|


Note : Checking Nozzle in the Meridional direction.









2



= (P*D*K)/(2*S*E-0.2*P) Appendix 1-4(c)

= (3.00*1000.0000*1.000)/( 2*106.50*1.00-0.2*3.00)

= 1.4089 mm.


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*27.39)/(110*1.00-0.6*3.00)

= 0.0742 mm.







Note : The Pad diameter is greater than the Diameter Limit, the

excess will not be considered .

Note:

Taking a UG-36(c)(3)(a) exemption for nozzle: N04.

This calculation is valid for nozzles that meet all the requirements of

paragraph UG-36. Please check the Code carefully, especially for nozzles

that are not isolated or do not meet Code spacing requirements. To force

the computation of areas for small nozzles go to Tools->Configuration





2

and check the box to force the UG-37 area or App 1-10 computation.










NOTE : Skipping the nozzle attachment weld strength calculations.

Per UW-15(b)(2) the nozzles exempted by UG-36(c)(3)(a)

(small nozzles) do not require a weld strength check.




Note : Checking Nozzle in the Latitudinal direction.








2




= (P*D*K)/(2*S*E-0.2*P) Appendix 1-4(c)

= (3.00*1000.0000*1.000)/( 2*106.50*1.00-0.2*3.00)

= 1.4089 mm.


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*27.39)/(110*1.00-0.6*3.00)

= 0.0742 mm.









Note:








2














= min[ 3.420 , max( 1.500 , 1.500 ) ]

= 1.5000 mm.


= max( ta, tb )

= max( 0.3337 , 1.5000 )

= 1.5000 mm.










2


















Nozzle Calcs. : LI1 Nozl: 12 3:23p Dec 18,2015

2

INPUT VALUES, Nozzle Description: LI1 From : 20








Inside Diameter of Cylindrical Shell D 1000.00 mm.

Design Length of Section L 2908.3335 mm.

Shell Finished (Minimum) Thickness t 10.0000 mm.

Shell Internal Corrosion Allowance c 0.0000 mm.

Shell External Corrosion Allowance co 0.0000 mm.

Distance from Bottom/Left Tangent 200.0000 mm.


Type of Element Connected to th e Shel l : Nozzle










2





















| |

| |





2

| |

| |

____________/| |

| \ | |

| \ | |

|____________\|__|

Insert Nozzle No Pad, no Inside projection

Reinforcement CALCULATION, Description: LI1





Reqd thk per UG-37(a)of Cylindrical Shell, Tr [Int. Press]

= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*500.0000)/(106*1.00-0.6*3.00)

= 1.4109 mm.


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*19.05)/(110*1.00-0.6*3.00)

= 0.0516 mm.






2

UG-40, Limits of Reinforcement : [External Pressure]



Normal to Vessel Wall (Thickness Limit), no pad Tlnp 12.7000 mm.

Note:

Taking a UG-36(c)(3)(a) exemption for nozzle: LI1.
















= min[ 3.220 , max( 1.500 , 1.500 ) ]

= 1.5000 mm.


= max( ta, tb )





2

= max( 0.2617 , 1.5000 )

= 1.5000 mm.


Weld Size Calculations, Description: LI1


















2


























2





Nominal Thickness tn STD
























2


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*500.0000)/(106*1.00-0.6*3.00)

= 1.4109 mm.


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*193.68)/(110*1.00-0.6*3.00)

= 0.5245 mm.








= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sp/S )





2

= min( 1, 106.5/106.5 )

= 1.000


= min( fr2, fr4 )

= min( 1.0 , 1.0 )

= 1.000



Area Required Ar NA 10.223 NA cm²

Area in Shell A1 NA 18.289 NA cm²

Area in Nozzle Wall A2 NA 4.252 NA cm²

Area in Inward Nozzle A3 NA 1.905 NA cm²

Area in Welds A41+A42+A43 NA 2.450 NA cm²

Area in Element A5 NA 21.000 NA cm²

TOTAL AREA AVAILABLE Atot NA 47.896 NA cm²




Area Required [A]:


= 0.5(387.3500*5.2785*1+2*9.5250*5.2785*1*(1-1.00))

= 10.223 cm²






2



= 387.350 ( 1.00 * 10.0000 - 1.0 * 5.278 ) - 2 * 9.525

( 1.00 * 10.0000 - 1.0 * 5.2785 ) * ( 1 - 1.000 )

= 18.289 cm²


= ( 2 * Tlwp ) * ( tn - trn ) * fr2

= ( 2 * 25.00 ) * ( 9.52 - 1.02 ) * 1.0000

= 4.252 cm²


= 2 * ti * min( h, Tl, 2.5 * ti) * fr2

= 2 * 9.5250 * ( 10.0000 ) * 1.0000

= 1.905 cm²


= Wo²*fr3+(Wi-can/0.707)²*fr2+Wp²*fr4

= 10.0000² *1.00 + (9.0000 )² *1.00 + 8.0000² * 1.00

= 2.450 cm²



= ( 686.4000 - 406.4000 ) * 10.0000 * 1.0000

= 21.000 cm²








2









= min[ 8.331 , max( 1.500 , 1.500 ) ]

= 1.5000 mm.


= max( ta, tb )

= max( 1.0215 , 1.5000 )

= 1.5000 mm.



B31.3 Pipi ng C od e (see 319.4.4 and 302.3.5):







Nozzle Calculations per App. 1-10: Internal Pressure Case:





2

Thickness of Nozzle [tn]:

= thickness - corrosion allowance

= 9.525 - 0.000

= 9.525 mm.

Effective Pressure Radius [Reff]:

= Di/2 + corrosion allowance

= 1000.000/2 + 0.000

= 500.000 mm.

Effective Length of Vessel Wall [LR]:

Note : Pad Thk >= 0.5T and Pad Width < 8(Shell Thk + Pad Thk)

= 10 * t

= 10 * 10.000

= 100.000 mm.

Thickness Limit Candidate [LH1]:

= t + 0.78 * sqrt( Rn * tn )

= 10.000 + 0.78 * sqrt( 193.675 * 9.525 )

= 43.501 mm.


= Lpr1 + T

= 200.000 + 10.000

= 210.000 mm.


= 8( t + te )

= 8( 10.000 + 10.000 )





2

Determine Parameter [Lamda]:

= min( 10, ( Dn + Tn )/( sqrt( ( Di + teff ) * teff )) )

= min( 10, (387.35 + 9.525 )/( sqrt((1000.00 + 10.000 ) * 10.000 )) )

= 3.949

Compute Areas A1-A43 (No Pad) or A1-A5 (With Pad) :

Area Contributed by the Vessel Wall [A1]:

= t * LR * max( Lamda/4, 1 )

= 10.000 * 100.000 * max( 3.949/4, 1 )

= 10.000 cm²

Area Contributed by the Nozzle Outside the Vessel Wall [A2]:

= tn * LH

= 9.525 * 43.501

= 4.144 cm²

Area Contributed by the Nozzle Inside the Vessel Wall [A3]:

= ( tn - c ) * L1

= ( 9.525 - 0.000 ) * 10.000

= 0.952 cm²

Area Contributed by the Inside Fillet Weld [A43]:

= 0.5 * Leg43 2

= 0.5 * 9.000 2

= 0.405 cm²

Area Contributed by the Outside Fillet Weld [A41]:

= 0.5 * Leg41 2





2

= 3.000 * 500.000 * 193.675

= 2962.5 Kgf

Area Resisting Internal Pressure [Ap]:

= Rn( LH - t ) + Reff( LR + tn + Rnc )

= 193.675 ( 43.501 - 10.000 ) + 500.000 ( 100.000 + 9.525 + 193.675 )

= 1580.9 cm²

Maximum Allowable Working Pressure Candidate [Pmax1]:

= Sallow /( 2 * Ap/AT - Rxs/teff )

= 159.750/( 2 * 1580.884/26.001 - 500.000/10.000 )

= 22.3 bars


= S[t/Reff]

= 106.500 [10.000/500.000 ]

= 21.3 bars

Maximum Allowable Working Pressure [Pmax]:

= min( Pmax1, Pmax2 )

= min( 22.310 , 21.299 )

= 21.299 bars

Average Primary Membrane Stress [SigmaAvg]:

= ( fN + fS + fY ) / AT

= ( 198.498 + 1675.333 + 2962.521 )/26.001

= 18.241 N./mm²

General Primary Membrane Stress [SigmaCirc]:

= P * Reff / teff





2

= 3.000 * 500.000/10.000

= 15.0 N./mm²

Maximum Local Primary Membrane Stress [PL]:

= max( 2 * SigmaAvg - SigmaCirc, SigmaCirc )

= max( 2 * 18.241 - 15.001 , 15.001 )

= 21.5 N./mm²

Summary of Nozzle Pressure/Stress Results:

Allowed Local Primary Membrane Stress Sallow 159.75 N./mm²

Local Primary Membrane Stress PL 21.48 N./mm²

Maximum Allowable Working Pressure Pmax 21.30 bars

Strength of Nozzle Attachment Welds per 1-10 and U-2(g)

Discontinuity Force Factor [ky]:

= ( Rnc + tn ) / Rnc

= ( 193.675 + 9.525 )/193.675

= 1.049 For set-in Nozzles

Weld Length of Nozzle to Shell Weld [Ltau]:

= pi/2 * ( Rn + tn )

= pi/2 * ( 193.675 + 9.525 )

= 319.186 mm.

Weld Length of Pad to Shell Weld [LtauP]:

= pi/2 * ( Rn + tn + W )

= pi/2 * ( 193.675 + 9.525 + 140.000 )

= 539.097 mm.





2

Weld Throat Dimensions, (0.7071*Leg Dimensions) [L41T, L42T, L43T]:

= 7.071, 5.657, 6.364, mm.

Weld Load Value [fwelds]:

= min( fy * ky, 1.5 * Sn( A2 + A3 ), pi/4*P*Rn^2*ky^2 )

= min(2962*1.05,1.5*111.0(4.144+0.952),pi/4*3.0*193.68^2*1.05^2)

= 992.099 Kgf

Discontinuity Force [fws]:

= fwelds * t * S/( t * S + te * Sp )

= 992.1*10.00*106/(10.000*106+10.000*106)

= 496.012 Kgf

Discontinuity Force [fwp]:

= fwelds * te * Sp / ( t * S + te * Sp )

= 992.1*10.00*106/(10.000*106+10.000*106)

= 496.087 Kgf

Shear Stress [tau1]:

= fws / ( Ltau * ( 0.6 * tw1 + 0.49 * L43T ) )

= 496.012/( 319.186 * ( 0.6 * 6.000 + 0.49 * 6.364 ) )

= 2.268 N./mm²


= fwp / ( Ltau * ( 0.6 * tw2 + 0.49 * L41T ) )

= 496.087/( 319.186 * ( 0.6 * 10.000 + 0.49 * 7.071 ) )

= 1.610 N./mm²


= fwp / ( Ltau * ( 0.49 * L42T ) )





2

= 496.087/( 539.097 * ( 0.49 * 5.657 ) )

= 3.256 N./mm²

Maximum Shear Stress in the Welds:

= max( tau1, tau2, tau3 )

= max( 2.268 , 1.610 , 3.256 )

= 3.3 must be less than or equal to 106.5 N./mm²







Nozzle Weld 6.0000 = Min per Code 7.0700 = 0.7 * Wo mm.


Inward Weld 6.0000 = Min per Code 6.3630 = 0.7 * Wi-Can mm.











2



Cylindrical or Spherical Vessel Cylsph Cylindrical




















External Forces and Moments in WRC 107 Convention:





2

Radial Load (SUS) P -2040.0 Kgf

Longitudinal Shear (SUS) Vl 2040.0 Kgf

Circumferential Shear (SUS) Vc 2040.0 Kgf

Circumferential Moment (SUS) Mc 1958.0 Kg-m.

Longitudinal Moment (SUS) Ml 2610.0 Kg-m.

Torsional Moment (SUS) Mt 1956.0 Kg-m.






Radial Load P -2040.0 Kgf

Circumferential Shear VC 2040.0 Kgf

Longitudinal Shear VL 2040.0 Kgf

Circumferential Moment MC 1958.0 Kg-m.

Longitudinal Moment ML 2610.0 Kg-m.



Dimensionless Loads for Cylindrical Shells at Attachment Junction:

-------------------------------------------------------------------


-------------------------------------------------------------------

N(PHI) / ( P/Rm ) 0.349 4C 2.900 (A,B)

N(PHI) / ( P/Rm ) 0.349 3C 1.527 (C,D)





2

M(PHI) / ( P ) 0.349 2C1 0.018 (A,B)

M(PHI) / ( P ) 0.349 1C ! 0.059 (C,D)





N(x) / ( P/Rm ) 0.349 3C 1.527 (A,B)

N(x) / ( P/Rm ) 0.349 4C 2.900 (C,D)

M(x) / ( P ) 0.349 1C1 0.039 (A,B)

M(x) / ( P ) 0.349 2C ! 0.030 (C,D)








------------------------------------------------------------------------

| Stress Values at


---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Memb. P | 5 5 5 5 2 2 2 2





2

Circ. Bend. P | 5 -5 5 -5 17 -17 17 -17

Circ. Memb. MC | 0 0 0 0 -10 -10 10 10

Circ. Bend. MC | 0 0 0 0 -117 117 117 -117

Circ. Memb. ML | -28 -28 28 28 0 0 0 0

Circ. Bend. ML | -33 33 33 -33 0 0 0 0

|

Tot. Circ. Str.| -50.9 5.8 73.0 -5.2 -107.5 91.8 149.2 -121.5

------------------------------------------------------------------------

Long. Memb. P | 2 2 2 2 5 5 5 5

Long. Bend. P | 11 -11 11 -11 8 -8 8 -8

Long. Memb. MC | 0 0 0 0 -24 -24 24 24

Long. Bend. MC | 0 0 0 0 -48 48 48 -48

Long. Memb. ML | -13 -13 13 13 0 0 0 0

Long. Bend. ML | -55 55 55 -55 0 0 0 0

|

Tot. Long. Str.| -54.8 33.5 84.3 -50.9 -59.2 20.7 88.5 -27.3

------------------------------------------------------------------------

Shear VC | 1 1 -1 -1 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

Shear MT | 3 3 3 3 3 3 3 3

|

Tot. Shear| 5.3 5.3 2.1 2.1 2.1 2.1 5.3 5.3

------------------------------------------------------------------------

Str. Int. | 58.46 34.45 84.64 51.03 107.62 91.91 149.64 121.82

------------------------------------------------------------------------

WARNING: Ratio of Pad Radius/Rm (0.680) is not between 0.01 and 0.571.


Dimensionless Loads for Cylindrical Shells at Pad edge:





2

-------------------------------------------------------------------


-------------------------------------------------------------------

N(PHI) / ( P/Rm ) 0.595 4C ! 2.955 (A,B)

N(PHI) / ( P/Rm ) 0.595 3C ! 1.041 (C,D)

M(PHI) / ( P ) 0.595 2C1 ! 0.004 (A,B)

M(PHI) / ( P ) 0.595 1C ! 0.065 (C,D)

N(PHI) / ( MC/(Rm**2 * Beta) ) 0.595 3A ! 0.946 (A,B,C,D)

M(PHI) / ( MC/(Rm * Beta) ) 0.595 1A ! 0.057 (A,B,C,D)

N(PHI) / ( ML/(Rm**2 * Beta) ) 0.595 3B ! 1.545 (A,B,C,D)

M(PHI) / ( ML/(Rm * Beta) ) 0.595 1B ! 0.003 (A,B,C,D)

N(x) / ( P/Rm ) 0.595 3C ! 1.041 (A,B)

N(x) / ( P/Rm ) 0.595 4C ! 2.955 (C,D)

M(x) / ( P ) 0.595 1C1 ! 0.011 (A,B)

M(x) / ( P ) 0.595 2C ! 0.033 (C,D)

N(x) / ( MC/(Rm**2 * Beta) ) 0.595 4A ! 4.429 (A,B,C,D)

M(x) / ( MC/(Rm * Beta) ) 0.595 2A ! 0.023 (A,B,C,D)

N(x) / ( ML/(Rm**2 * Beta) ) 0.595 4B ! 0.987 (A,B,C,D)

M(x) / ( ML/(Rm * Beta) ) 0.595 2B ! 0.006 (A,B,C,D)




------------------------------------------------------------------------

| Stress Values at





2


---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Memb. P | 11 11 11 11 4 4 4 4

Circ. Bend. P | 5 -5 5 -5 78 -78 78 -78

Circ. Memb. MC | 0 0 0 0 -11 -11 11 11

Circ. Bend. MC | 0 0 0 0 -218 218 218 -218

Circ. Memb. ML | -26 -26 26 26 0 0 0 0

Circ. Bend. ML | -17 17 17 -17 0 0 0 0

|

Tot. Circ. Str.| -26.9 -1.9 60.5 15.0 -148.4 132.7 313.2 -281.0

------------------------------------------------------------------------

Long. Memb. P | 4 4 4 4 11 11 11 11

Long. Bend. P | 12 -12 12 -12 40 -40 40 -40

Long. Memb. MC | 0 0 0 0 -56 -56 56 56

Long. Bend. MC | 0 0 0 0 -87 87 87 -87

Long. Memb. ML | -16 -16 16 16 0 0 0 0

Long. Bend. ML | -29 29 29 -29 0 0 0 0

|

Tot. Long. Str.| -29.4 4.3 62.8 -21.3 -91.9 3.2 195.6 -60.1

------------------------------------------------------------------------

Shear VC | 1 1 -1 -1 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

Shear MT | 2 2 2 2 2 2 2 2

|

Tot. Shear| 4.4 4.4 0.7 0.7 0.7 0.7 4.4 4.4

------------------------------------------------------------------------

Str. Int. | 32.73 10.82 63.03 36.31 148.39 132.67 313.38 281.08

------------------------------------------------------------------------





2



------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Pm (SUS) | 7 7 7 7 7 7 7 7

Circ. Pl (SUS) | -22 -22 33 33 -7 -7 13 13

Circ. Q (SUS) | -28 28 39 -39 -99 99 135 -135

------------------------------------------------------------------------

Long. Pm (SUS) | 3 3 3 3 3 3 3 3

Long. Pl (SUS) | -10 -10 16 16 -19 -19 30 30

Long. Q (SUS) | -44 44 67 -67 -39 39 57 -57

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1

Shear Q (SUS) | 3 3 3 3 3 3 3 3

------------------------------------------------------------------------

Pm (SUS) | 7.4 7.7 7.4 7.7 7.4 7.7 7.4 7.7

------------------------------------------------------------------------

Pm+Pl (SUS) | 15.4 15.2 41.4 41.7 15.7 15.7 34.5 34.5

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 53.8 38.3 88.5 49.9 100.3 99.6 157.0 114.2

------------------------------------------------------------------------

------------------------------------------------------------------------





2



---------------|--------------------------------------------------------

Pm (SUS) | 7.65 106.50 | Passed

Pm+Pl (SUS) | 41.65 159.75 | Passed


------------------------------------------------------------------------



------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Circ. Pm (SUS) | 14 15 14 15 14 15 14 15

Circ. Pl (SUS) | -14 -14 37 37 -7 -7 16 16

Circ. Q (SUS) | -12 12 22 -22 -140 140 297 -297

------------------------------------------------------------------------

Long. Pm (SUS) | 7 7 7 7 7 7 7 7

Long. Pl (SUS) | -12 -12 20 20 -44 -44 67 67

Long. Q (SUS) | -16 16 42 -42 -47 47 127 -127

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1

Shear Q (SUS) | 2 2 2 2 2 2 2 2

------------------------------------------------------------------------

Pm (SUS) | 14.9 15.2 14.9 15.2 14.9 15.2 14.9 15.2





2

------------------------------------------------------------------------

Pm+Pl (SUS) | 6.7 7.0 52.8 53.1 44.1 44.4 75.3 75.3

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 23.6 17.0 75.5 44.0 133.5 147.8 328.2 265.9

------------------------------------------------------------------------

------------------------------------------------------------------------



---------------|--------------------------------------------------------

Pm (SUS) | 15.15 106.50 | Passed

Pm+Pl (SUS) | 75.28 159.75 | Passed


------------------------------------------------------------------------





Nozzle Calcs. : LI-2 Nozl: 14 3:23p Dec 18,2015

2

INPUT VALUES, Nozzle Description: LI-2 From : 30

























2





























2





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Insert Nozzle With Pad, no Inside projection

Reinforcement CALCULATION, Description: LI-2






= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*500.0000)/(106*1.00-0.6*3.00)





2

= 1.4109 mm.


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*19.05)/(110*1.00-0.6*3.00)

= 0.0516 mm.








Note:

Taking a UG-36(c)(3)(a) exemption for nozzle: LI-2.














2







= min[ 3.220 , max( 1.500 , 1.500 ) ]

= 1.5000 mm.


= max( ta, tb )

= max( 0.2940 , 1.5000 )

= 1.5000 mm.


Weld Size Calculations, Description: LI-2














2










Nozzle Calcs. : LG2 Nozl: 15 3:23p Dec 18,2015

2

INPUT VALUES, Nozzle Description: LG2 From : 100

























2





























2





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Reinforcement CALCULATION, Description: LG2









2


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*500.0000)/(106*1.00-0.6*3.00)

= 1.4109 mm.


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*80.73)/(110*1.00-0.6*3.00)

= 0.2187 mm.








= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sp/S )





2

= min( 1, 106.5/106.5 )

= 1.000


= min( fr2, fr4 )

= min( 1.0 , 1.0 )

= 1.000











The area available without a pad is Insufficient.


SELECTION OF POSSIBLE REINFORCING PADS: Diameter Thickness

Based on given Pad Thickness: 170.6189 10.0000 mm.

Based on given Pad Diameter: 268.2750 0.2344 mm.

Based on Shell or Nozzle Thickness: 175.1617 3.4036 mm.

Area Required [A]:






2

= 0.5(161.4678*8.0501*1+2*3.4036*8.0501*1*(1-1.00))

= 6.499 cm²




= 161.468 ( 1.00 * 10.0000 - 1.0 * 8.050 ) - 2 * 3.404

( 1.00 * 10.0000 - 1.0 * 8.0501 ) * ( 1 - 1.000 )

= 3.149 cm²


= ( 2 * Tlwp ) * ( tn - trn ) * fr2

= ( 2 * 18.51 ) * ( 3.40 - 0.61 ) * 1.0000

= 1.035 cm²


= 2 * ti * min( h, Tl, 2.5 * ti) * fr2

= 2 * 3.4036 * ( 8.0000 ) * 1.0000

= 0.545 cm²



= (0.8969 ) * 1.00 + (0.0000 ) * 1.00 + 64.0000² * 1.00

= 1.537 cm²



= ( 268.2750 - 168.2750 ) * 10.0000 * 1.0000

= 7.500 cm²





2












= min[ 6.220 , max( 1.500 , 1.500 ) ]

= 1.5000 mm.


= max( ta, tb )

= max( 0.6085 , 1.5000 )

= 1.5000 mm.





= 3.404 - 0.000

= 3.404 mm.





2



= 1000.000/2 + 0.000

= 500.000 mm.



= 10 * t

= 10 * 10.000

= 100.000 mm.


= t + 0.78 * sqrt( Rn * tn )

= 10.000 + 0.78 * sqrt( 80.734 * 3.404 )

= 22.930 mm.


= Lpr1 + T

= 200.000 + 10.000

= 210.000 mm.


= 8( t + te )

= 8( 10.000 + 10.000 )

= 160.000 mm.

Effective Nozzle Wall Length Outside the Vessel [LH]:

= min[ LH1, LH2, LH3 ]

= min[ 22.930 , 210.000 , 160.000 )





2

= 22.930 mm.

Thickness Limit Candidate, Inside [LI1]:

= 0.78 * sqrt( Rn * tn )

= 0.78 * sqrt( 80.734 * 3.404 )

= 12.930 mm.

Nozzle Projection from the Inside of the Vessel Wall [Lpr2, LI2]:

= LI - c

= 8.000 - 0.000

= 8.000 mm.


= 8 * ( t + te )

= 8 * ( 10.000 + 10.000 )

= 160.000 mm.

Effective Nozzle Wall Length Inside the Vessel [LI]:

= min( LI1, LI2, LI3 )

= min( 12.930 , 8.000 , 160.000 )

= 8.000 mm.

Effective Vessel Thickness [teff]:

= t

= 10.000 mm.



= min( 10, (161.47 + 3.404 )/( sqrt((1000.00 + 10.000 ) * 10.000 )) )

= 1.641





2



= t * LR * max( Lamda/4, 1 )

= 10.000 * 100.000 * max( 1.641/4, 1 )

= 10.000 cm²


= tn * LH

= 3.404 * 22.930

= 0.780 cm²


= ( tn - c ) * L1

= ( 3.404 - 0.000 ) * 8.000

= 0.272 cm²


= 0.5 * Leg43 2

= 0.5 * 0.000 2

= 0.000 cm²

Area Contributed by the Pad Fillet Weld [A42]:

= 0.5 * Leg42 2

= 0.5 * 8.000 2

= 0.320 cm²


= 0.5 * Leg41 2 - Area cut by thickness limit





2

= 0.5 * 9.525 2 - 0.217

= 0.236 cm²

Area Contributed by the Reinforcing Pad [A5]:

= min( W * te , LR * te )

= min( 50.000 * 10.000 , 100.000 * 10.000 )

= 5.000 cm²

The total area contributed by A1 through A5 [AT]:

= A1 + frn( A2 + A3 ) + A41 + A42 + A43 + frp( A5 )

= 10.000+1.000(0.780+0.272)+0.236+0.320+0.000+1.000(5.000)

= 16.609 cm²

Allowable Local Primary Membrane Stress [Sallow]:

= 1.5 * S * E

= 1.5 * 106.500 * 1.000

= 159.7 N./mm²

Determine Force acting on the Nozzle [fN]:

= P * Rn( LH - t )

= 3.000 * 80.734 ( 22.930 - 10.000 )

= 31.9 Kgf

Determine Force acting on the Shell [fS]:

= P * Reff * ( LR + tn )

= 3.000 * 500.000 * ( 100.000 + 3.404 )

= 1581.7 Kgf

Discontinuity Force from Internal Pressure [fY]:

= P * Reff * Rnc





2

= 3.000 * 500.000 * 80.734

= 1234.9 Kgf



= 80.734 ( 22.930 - 10.000 ) + 500.000 ( 100.000 + 3.404 + 80.734 )

= 931.1 cm²



= 159.750/( 2 * 931.126/16.609 - 500.000/10.000 )

= 25.7 bars


= S[t/Reff]

= 106.500 [10.000/500.000 ]

= 21.3 bars



= min( 25.713 , 21.299 )

= 21.299 bars


= ( fN + fS + fY ) / AT

= ( 31.935 + 1581.698 + 1234.934 )/16.609

= 16.820 N./mm²


= P * Reff / teff





2

= 3.000 * 500.000/10.000

= 15.0 N./mm²



= max( 2 * 16.820 - 15.001 , 15.001 )

= 18.6 N./mm²








= ( 80.734 + 3.404 )/80.734



= pi/2 * ( Rn + tn )

= pi/2 * ( 80.734 + 3.404 )

= 132.163 mm.


= pi/2 * ( Rn + tn + W )

= pi/2 * ( 80.734 + 3.404 + 50.000 )

= 210.703 mm.





2


= 6.735, 5.657, 0.000, mm.



= min(1234*1.04,1.5*111.0(0.780+0.272),pi/4*3.0*80.73^2*1.04^2)

= 170.093 Kgf


= fwelds * t * S/( t * S + te * Sp )

= 170.1*10.00*106/(10.000*106+10.000*106)

= 85.040 Kgf



= 170.1*10.00*106/(10.000*106+10.000*106)

= 85.053 Kgf


= fws / ( Ltau * ( 0.6 * tw1 + 0.49 * L43T ) )

= 85.040/( 132.163 * ( 0.6 * 10.000 + 0.49 * 0.000 ) )

= 1.052 N./mm²


= fwp / ( Ltau * ( 0.6 * tw2 + 0.49 * L41T ) )

= 85.053/( 132.163 * ( 0.6 * 10.000 + 0.49 * 6.735 ) )

= 0.679 N./mm²


= fwp / ( Ltau * ( 0.49 * L42T ) )





2

= 85.053/( 210.703 * ( 0.49 * 5.657 ) )

= 1.428 N./mm²



= max( 1.052 , 0.679 , 1.428 )


Weld Size Calculations, Description: LG2

















Nozzle Calcs. : SG2 Nozl: 16 3:23p Dec 18,2015

2

INPUT VALUES, Nozzle Description: SG2 From : 100

























2





























2





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Reinforcement CALCULATION, Description: SG2









2


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*500.0000)/(106*1.00-0.6*3.00)

= 1.4109 mm.


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*80.73)/(110*1.00-0.6*3.00)

= 0.2187 mm.








= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sp/S )





2

= min( 1, 106.5/106.5 )

= 1.000


= min( fr2, fr4 )

= min( 1.0 , 1.0 )

= 1.000











The area available without a pad is Insufficient.


SELECTION OF POSSIBLE REINFORCING PADS: Diameter Thickness

Based on given Pad Thickness: 170.6189 10.0000 mm.

Based on given Pad Diameter: 268.2750 0.2344 mm.

Based on Shell or Nozzle Thickness: 175.1617 3.4036 mm.

Area Required [A]:






2

= 0.5(161.4678*8.0501*1+2*3.4036*8.0501*1*(1-1.00))

= 6.499 cm²




= 161.468 ( 1.00 * 10.0000 - 1.0 * 8.050 ) - 2 * 3.404

( 1.00 * 10.0000 - 1.0 * 8.0501 ) * ( 1 - 1.000 )

= 3.149 cm²


= ( 2 * Tlwp ) * ( tn - trn ) * fr2

= ( 2 * 18.51 ) * ( 3.40 - 0.61 ) * 1.0000

= 1.035 cm²


= 2 * ti * min( h, Tl, 2.5 * ti) * fr2

= 2 * 3.4036 * ( 8.0000 ) * 1.0000

= 0.545 cm²



= (0.8969 ) * 1.00 + (0.0000 ) * 1.00 + 64.0000² * 1.00

= 1.537 cm²



= ( 268.2750 - 168.2750 ) * 10.0000 * 1.0000

= 7.500 cm²





2












= min[ 6.220 , max( 1.500 , 1.500 ) ]

= 1.5000 mm.


= max( ta, tb )

= max( 0.6085 , 1.5000 )

= 1.5000 mm.





= 3.404 - 0.000

= 3.404 mm.





2



= 1000.000/2 + 0.000

= 500.000 mm.



= 10 * t

= 10 * 10.000

= 100.000 mm.


= t + 0.78 * sqrt( Rn * tn )

= 10.000 + 0.78 * sqrt( 80.734 * 3.404 )

= 22.930 mm.


= Lpr1 + T

= 200.000 + 10.000

= 210.000 mm.


= 8( t + te )

= 8( 10.000 + 10.000 )

= 160.000 mm.

Effective Nozzle Wall Length Outside the Vessel [LH]:

= min[ LH1, LH2, LH3 ]

= min[ 22.930 , 210.000 , 160.000 )





2

= 22.930 mm.


= 0.78 * sqrt( Rn * tn )

= 0.78 * sqrt( 80.734 * 3.404 )

= 12.930 mm.

Nozzle Projection from the Inside of the Vessel Wall [Lpr2, LI2]:

= LI - c

= 8.000 - 0.000

= 8.000 mm.


= 8 * ( t + te )

= 8 * ( 10.000 + 10.000 )

= 160.000 mm.

Effective Nozzle Wall Length Inside the Vessel [LI]:

= min( LI1, LI2, LI3 )

= min( 12.930 , 8.000 , 160.000 )

= 8.000 mm.

Effective Vessel Thickness [teff]:

= t

= 10.000 mm.



= min( 10, (161.47 + 3.404 )/( sqrt((1000.00 + 10.000 ) * 10.000 )) )

= 1.641





2



= t * LR * max( Lamda/4, 1 )

= 10.000 * 100.000 * max( 1.641/4, 1 )

= 10.000 cm²


= tn * LH

= 3.404 * 22.930

= 0.780 cm²


= ( tn - c ) * L1

= ( 3.404 - 0.000 ) * 8.000

= 0.272 cm²


= 0.5 * Leg43 2

= 0.5 * 0.000 2

= 0.000 cm²

Area Contributed by the Pad Fillet Weld [A42]:

= 0.5 * Leg42 2

= 0.5 * 8.000 2

= 0.320 cm²


= 0.5 * Leg41 2 - Area cut by thickness limit





2

= 0.5 * 9.525 2 - 0.217

= 0.236 cm²

Area Contributed by the Reinforcing Pad [A5]:

= min( W * te , LR * te )

= min( 50.000 * 10.000 , 100.000 * 10.000 )

= 5.000 cm²

The total area contributed by A1 through A5 [AT]:

= A1 + frn( A2 + A3 ) + A41 + A42 + A43 + frp( A5 )

= 10.000+1.000(0.780+0.272)+0.236+0.320+0.000+1.000(5.000)

= 16.609 cm²

Allowable Local Primary Membrane Stress [Sallow]:

= 1.5 * S * E

= 1.5 * 106.500 * 1.000

= 159.7 N./mm²

Determine Force acting on the Nozzle [fN]:

= P * Rn( LH - t )

= 3.000 * 80.734 ( 22.930 - 10.000 )

= 31.9 Kgf

Determine Force acting on the Shell [fS]:

= P * Reff * ( LR + tn )

= 3.000 * 500.000 * ( 100.000 + 3.404 )

= 1581.7 Kgf

Discontinuity Force from Internal Pressure [fY]:

= P * Reff * Rnc





2

= 3.000 * 500.000 * 80.734

= 1234.9 Kgf



= 80.734 ( 22.930 - 10.000 ) + 500.000 ( 100.000 + 3.404 + 80.734 )

= 931.1 cm²



= 159.750/( 2 * 931.126/16.609 - 500.000/10.000 )

= 25.7 bars


= S[t/Reff]

= 106.500 [10.000/500.000 ]

= 21.3 bars



= min( 25.713 , 21.299 )

= 21.299 bars


= ( fN + fS + fY ) / AT

= ( 31.935 + 1581.698 + 1234.934 )/16.609

= 16.820 N./mm²


= P * Reff / teff





2

= 3.000 * 500.000/10.000

= 15.0 N./mm²



= max( 2 * 16.820 - 15.001 , 15.001 )

= 18.6 N./mm²








= ( 80.734 + 3.404 )/80.734



= pi/2 * ( Rn + tn )

= pi/2 * ( 80.734 + 3.404 )

= 132.163 mm.


= pi/2 * ( Rn + tn + W )

= pi/2 * ( 80.734 + 3.404 + 50.000 )

= 210.703 mm.





2


= 6.735, 5.657, 0.000, mm.



= min(1234*1.04,1.5*111.0(0.780+0.272),pi/4*3.0*80.73^2*1.04^2)

= 170.093 Kgf


= fwelds * t * S/( t * S + te * Sp )

= 170.1*10.00*106/(10.000*106+10.000*106)

= 85.040 Kgf



= 170.1*10.00*106/(10.000*106+10.000*106)

= 85.053 Kgf


= fws / ( Ltau * ( 0.6 * tw1 + 0.49 * L43T ) )

= 85.040/( 132.163 * ( 0.6 * 10.000 + 0.49 * 0.000 ) )

= 1.052 N./mm²


= fwp / ( Ltau * ( 0.6 * tw2 + 0.49 * L41T ) )

= 85.053/( 132.163 * ( 0.6 * 10.000 + 0.49 * 6.735 ) )

= 0.679 N./mm²


= fwp / ( Ltau * ( 0.49 * L42T ) )





2

= 85.053/( 210.703 * ( 0.49 * 5.657 ) )

= 1.428 N./mm²



= max( 1.052 , 0.679 , 1.428 )


Weld Size Calculations, Description: SG2


















2


























3





























3





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Insert Nozzle With Pad, no Inside projection







= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*500.0000)/(106*1.00-0.6*3.00)





3

= 1.4107 mm.


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*38.96)/(110*1.00-0.6*3.00)

= 0.1055 mm.








Note:















3







= min[ 4.800 , max( 1.500 , 1.500 ) ]

= 1.5000 mm.


= max( ta, tb )

= max( 0.4194 , 1.5000 )

= 1.5000 mm.
















3











3





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3


= (P*K1*D))/(2*S*E-0.2*P) per UG-37(a)(3)

= (3.00*0.900*1000.0000)/(2 *106.52*1.00-0.2*3.00)

= 1.2678 mm.


= (P*R)/(S*E-0.6*P) per UG-27 (c)(1)

= (3.00*198.42)/(110*1.00-0.6*3.00)

= 0.5374 mm.








= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sn/S )

= min( 1, 111.0/106.5 )

= 1.000


= min( 1, Sp/S )





3

= min( 1, 106.5/106.5 )

= 1.000


= min( fr2, fr4 )

= min( 1.0 , 1.0 )

= 1.000



Area Required Ar 5.031 5.521 NA cm²

Area in Shell A1 34.654 28.642 NA cm²

Area in Nozzle Wall A2 1.859 1.647 NA cm²

Area in Inward Nozzle A3 0.764 0.764 NA cm²

Area in Welds A41+A42+A43 1.360 1.360 NA cm²

Area in Element A5 15.000 15.000 NA cm²

TOTAL AREA AVAILABLE Atot 53.637 47.413 NA cm²

The External Pressure Case Governs the Analysis.




Area Required [A]:


= 0.5(396.8496*2.7825*1+2*4.7752*2.7825*1*(1-1.00))

= 5.521 cm²





3




= 396.850 ( 1.00 * 10.0000 - 1.0 * 2.783 ) - 2 * 4.775

( 1.00 * 10.0000 - 1.0 * 2.7825 ) * ( 1 - 1.000 )

= 28.642 cm²


= ( 2 * Tlwp ) * ( tn - trn ) * fr2

= ( 2 * 21.94 ) * ( 4.78 - 1.02 ) * 1.0000

= 1.647 cm²


= 2 * ti * min( h, Tl, 2.5 * ti) * fr2

= 2 * 4.7752 * ( 8.0000 ) * 1.0000

= 0.764 cm²


= Wo²*fr3+(Wi-can/0.707)²*fr2+Wp²*fr4

= 6.0000² *1.00 + (6.0000 )² *1.00 + 8.0000² * 1.00

= 1.360 cm²



= ( 606.4000 - 406.4000 ) * 10.0000 * 1.0000

= 15.000 cm²






3











= min[ 8.331 , max( 1.500 , 1.500 ) ]

= 1.5000 mm.


= max( ta, tb )

= max( 1.0215 , 1.5000 )

= 1.5000 mm.



B31.3 Pipi ng Co de (see 319.4.4 and 302.3.5):











3










Weld Strength and Weld Loads per UG-41.1, Sketch (a) or (b)

Weld Load [W]:

= (A-A1+2*tn*fr1*(E1*t-tr))*Sv

= (5.5213 - 28.6425 + 2 * 4.7752 * 1.0000 *

(1.00 * 10.0000 - 2.7825 ) ) * 106

= 0.00 Kgf

Note: F is always set to 1.0 throughout the calculation.

Weld Load [W1]:

= (A2+A5+A4-(Wi-Can/.707)²*fr2)*Sv

= ( 1.6470 + 15.0000 + 1.3600 - 1.4173 * 1.00 ) * 106

= 19167.12 Kgf

Weld Load [W2]:

= (A2 + A3 + A4 + (2 * tn * t * fr1)) * Sv

= ( 1.6470 + 0.7640 + 0.7200 + ( 0.9550 ) ) * 106





3

= 4438.02 Kgf

Weld Load [W3]:

= (A2+A3+A4+A5+(2*tn*t*fr1))*S

= ( 1.6470 + 0.7640 + 1.3600 + 15.0000 + ( 0.9550 ) ) * 106

= 21425.28 Kgf

Strength of Connection Elements for Failure Path Analysis

Shear, Outward Nozzle Weld [Sonw]:

= (pi/2) * Dlo * Wo * 0.49 * Snw

= ( 3.1416/2.0 ) * 406.4000 * 6.0000 * 0.49 * 106

= 20385. Kgf

Shear, Inward Nozzle Weld [Sinw]:

= (pi/2) * Dlo * Wo * 0.49 * Snw

= ( 3.1416/2.0 ) * 406.4000 * 6.0000 * 0.49 * 106

= 20385. Kgf

Shear, Pad Element Weld [Spew]:

= (pi/2) * DP * WP * 0.49 * SEW

= ( 3.1416/2.0 ) * 606.4000 * 8.0000 * 0.49 * 106

= 40556. Kgf

Shear, Nozzle Wall [Snw]:

= (pi *( Dlr + Dlo )/4 ) * ( Thk - Can ) * 0.7 * Sn

= (3.1416 * 200.8124 ) * ( 4.7752 - 0.0000 ) * 0.7 * 110

= 23859. Kgf

Tension, Pad Groove Weld [Tpgw]:





3

= ( pi/2) * Dlo * Wgpn * 0.74 * Seg

= (3.1416/2 ) * 406.4000 * 10.0000 * 0.74 * 110

= 53448. Kgf

Tension, Shell Groove Weld [Tngw]:

= (pi/2) * Dlo * (Wgnvi-Cas) * 0.74 * Sng

= ( 3.1416/2.0 ) * 406.4000 * ( 6.0000 - 0.0000 ) * 0.74 * 110

= 32069. Kgf

Strength of Failure Paths:

PATH11 = ( SPEW + SNW ) = ( 40555 + 23859 ) = 64414 Kgf

PATH22 = ( Sonw + Tpgw + Tngw + Sinw )

= ( 20384 + 53447 + 32068 + 20384 ) = 126286 Kgf

PATH33 = ( Spew + Tngw + Sinw )

= ( 40555 + 32068 + 20384 ) = 93009 Kgf

Summary of Failure Path Calculations:













3




Cylindrical or Spherical Vessel Cylsph Spherical









WRC107 Attachment Classification Holsol Hollow















3

------------------------------------------------------------

N(x) * T / P SP 7 0.01342 (A,B,C,D)

M(x) / P SP 7 0.00613 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / MC SM 7 0.01673 (A,B,C,D)

M(x) * SQRT(Rm * T ) / MC SM 7 0.00833 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / ML SM 7 0.01673 (A,B,C,D)

M(x) * SQRT(Rm * T ) / ML SM 7 0.00833 (A,B,C,D)

N(y) * T / P SP 7 0.14990 (A,B,C,D)

M(y) / P SP 7 0.01254 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / MC SM 7 0.15363 (A,B,C,D)

M(y) * SQRT(Rm * T ) / MC SM 7 0.02002 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / ML SM 7 0.15363 (A,B,C,D)

M(y) * SQRT(Rm * T ) / ML SM 7 0.02002 (A,B,C,D)



------------------------------------------------------------------------

| Stress Values at


---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Memb. P | 0 0 0 0 0 0 0 0

Rad. Bend. P | 1 -1 1 -1 1 -1 1 -1

Rad. Memb. MC | 0 0 0 0 -7 -7 7 7

Rad. Bend. MC | 0 0 0 0 -23 23 23 -23

Rad. Memb. ML | -5 -5 5 5 0 0 0 0

Rad. Bend. ML | -17 17 17 -17 0 0 0 0





3

|

Tot. Rad. Str.| -21.2 10.7 26.2 -13.0 -29.1 14.6 34.1 -16.9

------------------------------------------------------------------------

Tang. Memb. P | 7 7 7 7 7 7 7 7

Tang. Bend. P | 3 -3 3 -3 3 -3 3 -3

Tang. Memb. MC | 0 0 0 0 -72 -72 72 72

Tang. Bend. MC | 0 0 0 0 -56 56 56 -56

Tang. Memb. ML | -54 -54 54 54 0 0 0 0

Tang. Bend. ML | -42 42 42 -42 0 0 0 0

|

Tot. Tang. Str.| -86.2 -8.2 108.7 15.6 -118.6 -12.1 141.1 19.6

------------------------------------------------------------------------

Shear VC | 1 1 -1 -1 0 0 0 0

Shear VL | 0 0 0 0 -1 -1 1 1

Shear MT | 6 6 6 6 6 6 6 6

|

Tot. Shear| 7.7 7.7 4.6 4.6 4.6 4.6 7.7 7.7

------------------------------------------------------------------------

Str. Int. | 87.07 24.38 108.93 30.08 118.84 28.29 141.67 39.69

------------------------------------------------------------------------

Unitless Prm: U = 3.19 TAU = 0.00 ( 62.99) RHO = 0.00 ( 2.09)

Dimensionless Loads for Spherical Shells at Pad edge:

------------------------------------------------------------


------------------------------------------------------------

N(x) * T / P SR 2 0.02175 (A,B,C,D)

M(x) / P SR 2 0.00990 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / MC SR 3 0.01691 (A,B,C,D)





3

M(x) * SQRT(Rm * T ) / MC SR 3 0.01053 (A,B,C,D)

N(x) * T * SQRT(Rm * T ) / ML SR 3 0.01691 (A,B,C,D)

M(x) * SQRT(Rm * T ) / ML SR 3 0.01053 (A,B,C,D)

N(y) * T / P SR 2 0.00650 (A,B,C,D)

M(y) / P SR 2 0.00300 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / MC SR 3 0.00507 (A,B,C,D)

M(y) * SQRT(Rm * T ) / MC SR 3 0.00317 (A,B,C,D)

N(y) * T * SQRT(Rm * T ) / ML SR 3 0.00507 (A,B,C,D)

M(y) * SQRT(Rm * T ) / ML SR 3 0.00317 (A,B,C,D)



------------------------------------------------------------------------

| Stress Values at


---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Memb. P | 4 4 4 4 4 4 4 4

Rad. Bend. P | 11 -11 11 -11 11 -11 11 -11

Rad. Memb. MC | 0 0 0 0 -45 -45 45 45

Rad. Bend. MC | 0 0 0 0 -169 169 169 -169

Rad. Memb. ML | -34 -34 34 34 0 0 0 0

Rad. Bend. ML | -127 127 127 -127 0 0 0 0

|

Tot. Rad. Str.| -145.4 85.8 177.9 -100.9 -199.2 116.9 231.7 -132.0

------------------------------------------------------------------------

Tang. Memb. P | 1 1 1 1 1 1 1 1





3

Tang. Bend. P | 3 -3 3 -3 3 -3 3 -3

Tang. Memb. MC | 0 0 0 0 -13 -13 13 13

Tang. Bend. MC | 0 0 0 0 -51 51 51 -51

Tang. Memb. ML | -10 -10 10 10 0 0 0 0

Tang. Bend. ML | -38 38 38 -38 0 0 0 0

|

Tot. Tang. Str.| -43.8 25.9 53.6 -30.5 -60.0 35.3 69.8 -39.9

------------------------------------------------------------------------

Shear VC | 2 2 -2 -2 0 0 0 0

Shear VL | 0 0 0 0 -2 -2 2 2

Shear MT | 5 5 5 5 5 5 5 5

|

Tot. Shear| 7.6 7.6 3.4 3.4 3.4 3.4 7.6 7.6

------------------------------------------------------------------------

Str. Int. | 145.97 86.78 177.95 101.05 199.31 117.05 232.04 132.59

------------------------------------------------------------------------



------------------------------------------------------------------------



---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Pm (SUS) | 6 6 6 6 6 6 6 6

Rad. Pl (SUS) | -5 -5 6 6 -7 -7 8 8

Rad. Q (SUS) | -15 15 19 -19 -21 21 25 -25

------------------------------------------------------------------------





3

Long. Pm (SUS) | 6 6 6 6 6 6 6 6

Long. Pl (SUS) | -47 -47 62 62 -65 -65 80 80

Long. Q (SUS) | -38 38 46 -46 -53 53 60 -60

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 1 1 -1 -1 -1 -1 1 1

Shear Q (SUS) | 6 6 6 6 6 6 6 6

------------------------------------------------------------------------

Pm (SUS) | 6.8 6.8 6.8 6.8 6.8 6.8 6.8 6.8

------------------------------------------------------------------------

Pm+Pl (SUS) | 42.0 42.0 69.0 69.0 58.7 58.7 87.1 87.1

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 80.3 24.4 115.7 30.1 112.1 28.3 148.4 39.7

------------------------------------------------------------------------

------------------------------------------------------------------------



---------------|--------------------------------------------------------

Pm (SUS) | 6.75 106.52 | Passed

Pm+Pl (SUS) | 87.15 159.77 | Passed


------------------------------------------------------------------------



------------------------------------------------------------------------







3

---------------|--------------------------------------------------------


---------------|--------------------------------------------------------

Rad. Pm (SUS) | 13 13 13 13 13 13 13 13

Rad. Pl (SUS) | -29 -29 38 38 -41 -41 49 49

Rad. Q (SUS) | -115 115 139 -139 -158 158 181 -181

------------------------------------------------------------------------

Long. Pm (SUS) | 13 13 13 13 13 13 13 13

Long. Pl (SUS) | -8 -8 11 11 -12 -12 14 14

Long. Q (SUS) | -34 34 42 -42 -47 47 54 -54

------------------------------------------------------------------------

Shear Pm (SUS) | 0 0 0 0 0 0 0 0

Shear Pl (SUS) | 2 2 -2 -2 -2 -2 2 2

Shear Q (SUS) | 5 5 5 5 5 5 5 5

------------------------------------------------------------------------

Pm (SUS) | 13.5 13.5 13.5 13.5 13.5 13.5 13.5 13.5

------------------------------------------------------------------------

Pm+Pl (SUS) | 21.3 21.3 52.2 52.2 29.1 29.1 63.5 63.5

------------------------------------------------------------------------

Pm+Pl+Q (Total)| 132.5 100.3 191.5 87.5 185.8 130.5 245.5 119.1

------------------------------------------------------------------------

------------------------------------------------------------------------



---------------|--------------------------------------------------------

Pm (SUS) | 13.50 106.52 | Passed

Pm+Pl (SUS) | 63.49 159.77 | Passed


------------------------------------------------------------------------





3





Nozzle Schedule : Step: 33 3:23p Dec 18,2015

3

Nozzle Schedule:

Nominal Flange Noz. Wall Re-Pad Cut

Description Size Sch/Type O/Dia Thk ODia Thick Length

mm Cls mm mm. mm. mm. mm.

------------------------------------------------------------------------------

LI1 40 80S WNF 48.260 5.080 - - 162

LI-2 40 80S WNF 48.260 5.080 520.00 6.00 210

N04 50 10S WNF 60.325 2.769 319.08 4.00 224

N01 80 40S WNF 88.900 5.486 188.90 10.00 211

LG2 150 10S WNF 168.275 3.404 268.27 10.00 218

SG2 150 10S WNF 168.275 3.404 268.27 10.00 218

N03 200 10S WNF 219.075 3.759 319.08 4.00 217

N02 400 STD WNF 406.400 9.525 686.40 10.00 253

N5 400 10S WNF 406.400 4.775 606.40 10.00 233

General Notes for the above table:

The Cut Length is the Outside Projection + Inside Projection + Drop +

In Plane Shell Thickness. This value does not include weld gaps,

nor does it account for shrinkage.

In the case of Oblique Nozzles, the Outside Diameter must

be increased. The Re-Pad WIDTH around the nozzle is calculated as follows:

Width of Pad = (Pad Outside Dia. (per above) - Nozzle Outside Dia.)/2

For hub nozzles, the thickness and diameter shown are those of the smaller

and thinner section.





3

Nozzle Material and Weld Fillet Leg Size Details:

Shl Grve Noz Shl/Pad Pad OD Pad Grve Inside

Nozzle Material Weld Weld Weld Weld Weld

mm. mm. mm. mm. mm.

------------------------------------------------------------------------------

LI1 SA-312 TP316 10.000 9.525 - - -

LI-2 SA-312 TP316 6.000 9.525 5.000 6.000 -

N04 SA-312 TP316 6.000 9.525 3.000 4.000 -

N01 SA-312 TP316 10.000 9.525 8.000 10.000 -

LG2 SA-312 TP316 10.000 9.525 8.000 10.000 -

SG2 SA-312 TP316 10.000 9.525 8.000 10.000 -

N03 SA-312 TP316 6.000 9.525 3.000 4.000 -

N02 SA-312 TP316 6.000 10.000 8.000 10.000 9.000

N5 SA-312 TP316 6.000 6.000 8.000 10.000 6.000

Note: The Outside projections below do not include the flange thickness.

Nozzle Miscellaneous Data:

Elevation/Distance Layout Projection Installed In

Nozzle From Datum Angle Outside Inside Component

mm. deg. mm. mm.

----------------------------------------------------------------------------

LI1 ********* 180.00 152.40 0.00 Shell-1

LI-2 ********* 180.00 200.00 0.00 Shell-2

N04 0.00 200.00 5.00 Bottom Dish

N01 -1817.998 0.00 200.00 0.00 Shell-14

LG2 ********* 0.00 200.00 8.00 Shell-7

SG2 ********* 135.00 200.00 8.00 Shell-7

N03 0.00 200.00 8.00 Bottom Dish





3

N02 ********* 0.00 200.00 10.00 Shell-2

N5 0.00 200.00 8.00 Top Dish





Nozzle Summary : Step: 34 3:23p Dec 18,2015

3

Nozzle Calculation Summary:

Description MAWP Ext MAPNC UG45 [tr] Weld Areas or

bars bars Path Stresses

---------------------------------------------------------------------------

N03 5.16 OK ... OK 1.50 OK Passed

N04 5.16 ... ... OK 1.50 OK NoCalc[*]

N04 5.16 ... ... OK 1.50 OK NoCalc[*]

LI1 5.16 ... ... OK 1.50 OK NoCalc[*]

N02 5.16 OK ... OK 1.50 OK Passed

LI-2 5.16 ... ... OK 1.50 OK NoCalc[*]

LG2 5.16 OK ... OK 1.50 OK Passed

SG2 5.16 OK ... OK 1.50 OK Passed

N01 5.16 ... ... OK 1.50 OK NoCalc[*]

N5 5.16 OK ... OK 1.50 OK Passed

---------------------------------------------------------------------------

Min. - Nozzles 5.16 N5

Min. Shell&Flgs 5.16 40 50 19.00

Computed Vessel M.A.W.P. 5.16 bars

[*] - This was a small opening and the areas were not computed or

the MAWP of this connection could not be computed because

the longitudinal bending stress was greater than the hoop stress.

Note: MAWPs (Internal Case) shown above are at the High Point.

Check the Spatial Relationship between the Nozzles




Nozzle Summary : Step: 34 3:23p Dec 18,2015

3

From Node Nozzle Description Y Coordinate, Layout Angle, Dia. Limit

10 N03 0.000 0.000 423.113

10 N04 0.000 0.000 109.576

20 LI1 200.000 180.000 76.200

30 N02 2300.000 0.000 774.700

30 LI-2 1750.000 180.000 76.200

100 LG2 9970.001 0.000 368.275

100 SG2 9970.001 135.000 368.275

190 N01 19010.002 0.000 155.854

230 N5 0.000 0.000 793.699

The nozzle spacing is computed by the following:

= Sqrt( ll ² + lc ² ) where

ll - Arc length along the inside vessel surface in the long. direction.

lc - Arc length along the inside vessel surface in the circ. direction

If any interferences/violations are found, they will be noted below.

No interference violations have been detected !





Vessel Design Summary : Step: 35 3:23p Dec 18,2015

3

Design Code: ASME Code Section VIII Division 1, 2010, 2011a

Diameter Spec : 1000.000 mm. ID

Vessel Design Length, Tangent to Tangent 19860.00 mm.

Distance of Bottom Tangent above Grade 300.00 mm.

Specified Datum Line Distance 20828.00 mm.

Shell Material Specification SA-240 316L

Lug Material Specification SA-516 70

Nozzle Material Specification SA-312 TP316

Re-Pad Material Specification SA-240 316L

Internal Design Temperature 220 C

Internal Design Pressure 3.000 bars

External Design Temperature 220 C

External Design Pressure 1.035 bars

Maximum Allowable Working Pressure 5.160 bars

External Max. Allowable Working Pressure 1.624 bars

Hydrostatic Test Pressure 4.120 bars

Wind Design Code IS-875

Earthquake Design Code IS-1893 SCM

Element Pressures and MAWP: bars

Element Desc | Design Pres. | External | M.A.W.P | Corrosion

| + Stat. head | Pressure | | Allowance





3

---------------------------------------------------------------------

Bottom Dish 3.000 1.035 21.256 0.0000

Shell-1 3.000 1.035 21.046 0.0000

Shell-2 3.000 1.035 21.046 0.0000

BF-1 3.000 1.035 18.911 0.0000

BF-2 3.000 1.035 19.058 0.0000

Shell-3 3.000 1.035 21.046 0.0000

Shell-4 3.000 1.035 21.046 0.0000

Shell-5 3.000 1.035 21.046 0.0000

Shell-6 3.000 1.035 21.046 0.0000

Shell-7 3.000 1.035 21.046 0.0000

Shell-8 3.000 1.035 21.046 0.0000

BF-3 3.000 1.035 19.058 0.0000

BF-4 3.000 1.035 19.058 0.0000

Shell-9 3.000 1.035 21.046 0.0000

Shell-10 3.000 1.035 21.046 0.0000

Shell-11 3.000 1.035 21.046 0.0000

Shell-12 3.000 1.035 21.046 0.0000

Shell-13 3.000 1.035 21.046 0.0000

Shell-14 3.000 1.035 21.049 0.0000

BF-5 3.000 1.035 18.914 0.0000

BF-6 3.000 1.035 18.914 0.0000

Shell-15 3.000 1.035 21.049 0.0000

Top Dish 3.000 1.035 21.259 0.0000

Element "To" Elev Length Element Thk R e q d T h k Joint Eff

Type mm. mm. mm. Int. Ext. Long Circ

-----------------------------------------------------------------------

Ellipse -20778.0 50.0 12.0 1.5 2.8 1.00 1.00

Cylinder -19278.0 1500.0 10.0 1.5 5.3 1.00 1.00





3

Cylinder -18003.0 1275.0 10.0 1.5 5.3 1.00 1.00

Body Flg -17858.0 145.0 70.0 67.4 67.4 1.00 1.00

Body Flg -17713.0 145.0 70.0 63.1 63.1 1.00 1.00

Cylinder -16358.0 1355.0 10.0 1.5 8.1 1.00 1.00

Cylinder -14858.0 1500.0 10.0 1.5 8.1 1.00 1.00

Cylinder -13358.0 1500.0 10.0 1.5 8.1 1.00 1.00

Cylinder -11858.0 1500.0 10.0 1.5 8.1 1.00 1.00

Cylinder -10608.0 1250.0 10.0 1.5 8.1 1.00 1.00

Cylinder -10108.0 500.0 10.0 1.5 8.1 1.00 1.00

Body Flg -9963.0 145.0 70.0 63.1 63.1 1.00 1.00

Body Flg -9818.0 145.0 70.0 63.1 63.1 1.00 1.00

Cylinder -8318.0 1500.0 10.0 1.5 8.3 1.00 1.00

Cylinder -6818.0 1500.0 10.0 1.5 8.3 1.00 1.00

Cylinder -5318.0 1500.0 10.0 1.5 8.3 1.00 1.00

Cylinder -3818.0 1500.0 10.0 1.5 8.3 1.00 1.00

Cylinder -2318.0 1500.0 10.0 1.5 8.3 1.00 1.00

Cylinder -1608.0 710.0 10.0 1.5 8.3 1.00 1.00

Body Flg -1463.0 145.0 70.0 66.3 66.3 1.00 1.00

Body Flg -1318.0 145.0 70.0 67.3 67.3 1.00 1.00

Cylinder -1018.0 300.0 10.0 1.5 2.4 1.00 1.00

Ellipse -968.0 50.0 12.0 1.5 2.8 1.00 1.00

Element thicknesses are shown as Nominal if specified, otherwise are Minimum

Total Wind Shear on Support 3876. Kgf

Total Earthquake Shear on Support 1499. Kgf

Wind Moment on Support 19034. Kg-m.

Earthquake Moment on Support 10462. Kg-m.

Design Calculation Column C1023

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