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METALCOLMESA

SOACHA

COLOMBIA

CODE CALCULATIONS

Item: SCRUBBERVessel No: R-SEP-36-1-3Customer: ECOPETROL

Calculations: 1651-1-MC-0001 Rev. 0Designer: HERNAN FERRER

Date: mi rcoles, marzo 20, 2013Location: CASABE SUR

Purchaser: ECOPETROLVessel Name: SCRUBBER 1651

Service: GAS SCRUBBER

Tag Number: R-SEP-36-1-3

You can edit this page by selecting Cover Page settings... in the report menu.


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Deficiencies Summary

No deficiencies found.

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Revision History

No. Date Operator Notes

0 3/20/2013 Andres New vessel created ASME Section VIII Division 1 [COMPRESS 2013 Build 7300]

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Settings Summary

COMPRESS 2013 Build 7300

Units: U.S. Customary

Datum Line Location: 0,00" from bottom seam

Design

ASME Section VIII Division 1, 2010 Edition, A11 Addenda

Design or Rating: Get Thickness from PressureMinimum thickness: 0,0625" per UG-16(b)Design for cold shut down only: NoDesign for lethal service (full radiography required): NoDesign nozzles for: Design P onlyCorrosion weight loss: 100% of theoretical lossUG-23 Stress Increase: 1,20Skirt/legs stress increase: 1,0

Minimum nozzle projection: 6"Juncture calculations for > 30 only: YesPreheat P-No 1 Materials > 1,25" and


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UG-22(d)(2) Vessel supports such as lugs, rings, skirts, saddles and legs: YesUG-22(f) Wind reactions: YesUG-22(f) Seismic reactions: YesUG-22(j) Test pressure and coincident static head acting during the test: YesNote: UG-22(b),(c) and (f) loads only considered when supports are present.

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Pressure Summary

Pressure Summary for Chamber bounded by BOTTOM HEAD and TOP HEAD

Ide ntifierP

Design( psi)

T

Design( F)

MAWP( psi)

MAP( psi)

MDMT( F)

MDMTExemption

ImpactTested

TOP HEAD 100 150 105,37 206,18 -55 Note 1 No

Straight Flange on TOP HEAD 100 150 199,76 300,35 -55 Note 2 No

Cylinder #1 100 150 148,82 250 -55 Note 3 No

Cylinder #2 100 150 147,26 250 -55 Note 4 No

Straight Flange o n BOTTOM HEA D 100 150 197,32 300,35 -55 Note 6 No

BOTTOM HEAD 100 150 102,62 206,18 -55 Note 5 No

MANHOLE (M1) 100 150 100 100 -55 Nozzle Note 7 No

Pad Note 8 No

ENTRADA (N1) 100 150 100 100 -55 Note 9 No

PG (N11) 100 150 100 100 -55 Note 9 No

SALIDA DE GAS (N2) 100 150 100 100 -47,3 Nozzle Note 10 No

Pad Note 11 No

ALIVIO (N3) 100 150 100 100 -55 Note 9 No

PDIT (N4A) 100 150 100 100 -55 Note 9 No

PDIT (N4B) 100 150 100 100 -55 Note 9 No

DRENAJE (N5) 100 150 100 100 -45,1 Note 12 No

TIT (N6) 100 150 100 100 -55 Note 9 No

SALIDA DE CONDENSADOS (N7) 100 150 100 100 -55 Note 9 No

LIT (N8A) 100 150 100 100 -55 Note 9 No

LIT (N8B) 100 150 100 100 -55 Note 9 No

LG (N9A) 100 150 100 100 -55 Note 9 No

LG (N9B) 100 150 100 100 -55 Note 9 No

Chamber design MDMT is -20 FChamber rated MDMT is -45,1 F @ 100 psi

Chamber MAWP hot & corroded is 100 psi @ 150 F

Chamber MAP cold & new is 100 psi @ 50 F

This pressure chamber is not designed for external pressure.

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Notes for MDMT R ating:

Note # Exemption Details

1. Straight Flange governs MDMT

2.Material impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 79,9 F, (coincident ratio = 0,424)Rated MDMT of -99,9F is limited to -55F by UCS-66(b)(2)

UCS-66 governing thickness = 0,3125 in





5. Straight Flange governs MDMT



7. Nozzle is impact test exempt to -155 F per UCS-66(b)(3) (coincident ratio = 0,3089).

8.Pad impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 46,2 F, (coincident ratio = 0,5667)Rated MDMT of -66,2F is limited to -55F by UCS-66(b)(2)

UCS-66 governing thickness = 0,3125 in.

9. Flange rating governs: UCS-66(b)(1)(b)

10.Nozzle impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 27,3 F, (coincident ratio = 0,7273) UCS-66 governing thickness = 0,2818 in.

11. Pad impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 27,3 F, (coincident ratio = 0,7273) UCS-66 governing thickness = 0,2818 in.

12. Nozzle impact test exemption temperature from Fig UCS -66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 25,1 F, (coincident ratio = 0,7485) UCS-66 governing thickness = 0,255 in.

Design notes are available on the Settings Summary page.

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Thickness Summary

Com ponentIdentifier

Materia l Diameter(in)

Length(in)

Nominal t(in)

Design t(in)

Total Corrosion(in)

JointE

Load

TOP HEAD SA-516 70 42 ID 10,755 0,255* 0,2484 0,125 0,85 Internal

Straight Flange on TOP HEAD SA-516 70 42 ID 2 0,375 0,2498 0,125 0,85 Internal

Cylinder #1 SA-516 70 42,125 ID 96 0,3125 0,2512 0,125 0,85 Internal

Cylinder #2 SA-516 70 42,125 ID 54 0,3125 0,2531 0,125 0,85 Internal

Straight Flange on BOTTOM HEAD SA-516 70 42 ID 2 0,375 0,2528 0,125 0,85 Internal

BOTTOM HEAD SA-516 70 42 ID 10,755 0,255* 0,2518 0,125 0,85 Internal

Support Skirt #1 SA-516 70 42,546 ID 44 0,375 0,013 0 0,55 Wind

Nominal t: Vessel wall nominal thickness

Design t: Required vessel thickness due to governing loading + corrosion

Joint E: Longitudinal seam joint efficiency

* Head minimum thickness after forming

Load

internal: Circumferential stress due to internal pressure governs

external: External pressure governs

Wind: Combined longitudinal stress of pressure + weight + wind governs

Seismic: Combined longitudinal stress of pressure + weight + seismic governs

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Nozzle Schedule

Nozzlemark Service Size Materials

ImpactTested Normalized

FineGrain Flange Blind

M1 MANHOLE 20 OD x 0,3125Nozzle SA-516 70 No No No NPS 20 Class

150SO A105

NPS 20 Class150A105Pad SA-516 70 No No No

N1 ENTRADA NPS 6 Sch 40(Std) NozzleSA-106 B Smlspipe No No No

NPS 6 Class 150WN A105 No

N11 PG NPS 2 Sch 160 NozzleSA-106 B Smlspipe No No No


N2 SALIDA DE GAS NPS 8 Sch 40(Std)Nozzle SA-106 B Smlspipe No No No NPS 8 Class 150WN A105 No

Pad SA-516 70 No No No

N3 ALIVIO NPS 3 Sch 80(XS) NozzleSA-106 B Smlspipe No No No


N4A PDIT NPS 2 Sch 160 Nozzle SA-106 B Smlspipe No No NoNPS 2 Class 150WN A105 No

N4B PDIT NPS 2 Sch 160 Nozzle SA-106 B Smlspipe No No NoNPS 2 Class 150WN A105 No

N5 DRENAJE NPS 3 Sch 80(XS) NozzleSA-106 B Smlspipe No No No


N6 TIT NPS 2 Sch 160 NozzleSA-106 B Smlspipe No No No


N7 SALIDA DECONDE NSA DOSNPS 3 Sch 80(XS) Nozzle

SA-106 B Smlspipe No No No


N8A LIT NPS 2 Sch 160 Nozzle SA-106 B Smlspipe No No NoNPS 2 Class 150WN A105 No

N8B LIT NPS 2 Sch 160 Nozzle SA-106 B Smlspipe No No NoNPS 2 Class 150WN A105 No

N9A LG NPS 2 Sch 160 Nozzle SA-106 B Smlspipe No No NoNPS 2 Class 150WN A105 No

N9B LG NPS 2 Sch 160 Nozzle SA-106 B Smlspipe No No NoNPS 2 Class 150WN A105 No

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Nozzle Summary

Nozzlemark

OD(in)

tn

(in)Req t

n(in)

A1? A 2?Shell ReinforcementPad Corr

(in)A

a/A

r(%)

Nom t(in)

Design t(in)

User t(in)

Width(in)

tpad(in)

M1 20 0,3125 0,2313 Yes Yes 0,3125 0,2313 2 0,3125 0,125 150,8

N1 6,625 0,28 0,2645 Yes Yes 0,3125 0,2314 N/A N/A 0,125 106,2

N11 2,375 0,344 0,2643 Yes Yes 0,3125 N/A N/A N/A 0,125 Exempt

N2 8,625 0,322 0,2627 Yes Yes 0,255* 0,2196 2 0,3125 0,125 217,5


N4A 2,375 0,344 0,2643 Yes Yes 0,3125 N/A N/A N/A 0,125 Exempt

N4B 2,375 0,344 0,2643 Yes Yes 0,3125 N/A N/A N/A 0,125 Exempt

N5 3,5 0,3 0,2662 Yes Yes 0,255* N/A N/A N/A 0,125 Exempt







tn: Nozzle thicknessReq t n: Nozzle thickness required per UG-45/UG-16Nom t: Vessel wall thicknessDesign t: Required vessel wall thickness due to pressure + corrosion allowance per UG-37User t: Local vessel wall thickness (near opening)Aa : Area available per UG-37, governing conditionAr: Area required per UG-37, governing conditionCorr: Corrosion allowance on nozzle wall

* Head minimum thickness after forming

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Weight Summary

ComponentWeight ( lb) Contributed by Vessel Elements

Surface Areaft2Metal

New*Metal

Corroded * InsulationInsulationSupports Lining

Piping+ Liquid

Operating Liquid Test Liquid

New Corroded New Corroded

TOP HEAD 172,9 93, 2 0 0 0 0 0 0 453,3 463,1 17

Cylinder #1 1 .097 ,9 66 0,7 0 0 0 0 1.154,4 1.168,4 4.895,2 4.955,2 87

Cylinder #2 635,1 382,2 0 0 0 0 2.174,4 2.200,5 2.718 2.750,7 50

BOTTOM HEAD 176,4 95 0 0 0 0 360,7 368,5 450,9 460,6 17

Support Skirt #1 622,5 622,5 0 0 0 0 0 0 0 0 83

Skirt Base Ring #1 132 132 0 0 0 0 0 0 0 0 15

TOTAL: 2.836,8 1.985,6 0 0 0 0 3.689,5 3.737,4 8.517,4 8.629,5 269

* Shells with attached nozzles have weight reduced by material cut out for opening.

Component

Weight ( lb) Contributed by Attachments SurfaceArea

ft2Body FlangesNozzles &Flanges PackedBeds

Ladders &Platforms

Trays TraySupportsRings &

ClipsVerticalLoads

New C orroded New Corroded

TOP HEAD 0 0 50,3 48 0 170,8 0 0 0 0 2

Cylinder #1 0 0 636,9 609,6 0 956,6 0 0 0 0 16

Cylinder #2 0 0 32,4 27,4 0 162 0 0 0 0 2BOTTOM HEAD 0 0 13 11,7 0 126 0 0 0 0 1

Support Skirt #1 0 0 0 0 0 0 0 0 0 0 0

TOTAL: 0 0 732,6 696,9 0 1.415,5 0 0 0 0 21

* Platforms and ladders are not included in surface area.

Vessel operating weight, Corroded: 7.835 lbVessel operating weight, New: 8.674 lbVessel empty weight, Corroded: 4.098 lbVessel empty weight, New: 4.985 lbVessel test weight, New: 12.087 lb

Vessel test weight, Corroded: 11.312 lbVessel surface area: 290 ft 2

Vessel center of gravity location - from datum - lift condition

Vessel Lift Weight, New: 3.569 lbCenter of Gravity: 61,2547"

Vessel Capacity

Vessel Capacity** (New): 1.013 US galVessel Capacity** (Corroded): 1.026 US gal**The vessel capacity does not include volume of nozzle, piping or other attachments.

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Test Report

Shop test pressure determination for Chamber bounded by BOTTOM HEAD and TOP HEAD based on userdefined pressure

Shop test gauge pressure is 134 psi at 50 F

The shop test is performed with the vessel in the horizontal position.

IdentifierLocal testpressure

psi

Test liquidstatic head

psi

Stressduring test

psi

Allowabletest stress

psi

Stressexcessive?

TOP HEAD 135,518 1,518 10.044 34.200 No

Straight Flange on TOP HEAD 135,518 1,518 7.657 34.200 No

Cylinder #1 135,521 1,521 9.202 34.200 No

Cylinder #2 135,521 1,521 9.202 34.200 No

Straight Flange on BOTTOM HEAD 135,518 1,518 7.657 34.200 No

BOTTOM HEAD 135,518 1,518 10.044 34.200 No

ALIVIO (N3) 135,749 1,749 12.733 51.300 No

DRENAJE (N5) 134,813 0,813 11.404 51.300 No

ENTRADA (N1) 134,87 0,87 19.812 51.300 No

LG (N9A) 135,537 1,537 9.619 51.300 No

LG (N9B) 135,537 1,537 9.619 51.300 No

LIT (N8A) 135,631 1,631 9.625 51.300 No

LIT (N8B) 135,631 1,631 9.625 51.300 No

MANHOLE (M1) 135,11 1,11 24.766 51.300 No

PDIT (N4A) 135,537 1,537 9.619 51.300 No

PDIT (N4B) 135,537 1,537 9.619 51.300 No

PG (N11) 135,749 1,749 9.634 51.300 NoSALIDA DE CONDENSADOS (N7) 135,749 1,749 9.149 51.300 No

SALIDA DE GAS (N2) 134,904 0,904 9.773 51.300 No

TIT (N6) 135,352 1,352 9.606 51.300 No

Notes:(1) P L stresses at nozzle openings have been estimated using the method described in PVP-Vol. 399, pages 77-82.(2) 1,5*0,9*S y used as the basis for the maximum local primary membrane stress at the nozzle intersection P L.(3) The zero degree angular position is assumed to be up, and the test liquid height is assumed to the top-mostflange.

The field test condition has not been investigated for the Chamber bounded by BOTTOM HEAD and TOP HEAD.

The test temperature of 50 F is warmer than the minimum recommended temperature of -15,1 F so the brittlefracture provision of UG-99(h) has been met.

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TOP HEAD

ASME Section VIII, Division 1, 2010 Edition, A11 Addenda

Component: Ellipsoidal HeadMaterial Specification: SA-516 70 (II-D p.18, ln. 19)Straight Flange governs MDMT

Internal design pressure: P = 100 psi @ 150 F

Static liquid head:

P s= 0 psi (SG=0,8, H s=0" Operating head)P th= 1,52 psi (SG=1, H s=42,0625" Horizontal test head)

Corrosion allowance: Inner C = 0,125" Outer C = 0"

Design MDMT = -20F No impact test performedRated MDMT = -55F Material is not normalized

Material is produced to fine grain practicePWHT is not performedDo not Optimize MDMT / Find MAWP

Radiography: Category A joints - Seamless No RTHead to shell seam - Spot UW-11(b) Type 1

Estimated weight*: new = 172,9 lb corr = 93,2 lbCapacity*: new = 54 US gal corr = 55,1 US gal* includes straight flange

Inner diameter = 42"Minimum head thickness = 0,255"Head ratio D/2h = 2 (new)Head ratio D/2h = 1,9882 (corroded)Straight flange length L sf = 2"Nominal straight flange thickness t sf = 0,375"Results Summary

The governing condition is internal pressure.Minimum thickness per UG-16 = 0,0625" + 0, 125" = 0,1875"Design thickness due to internal pressure (t) = 0,2484 "Maximum allowable working pressure (MAWP) = 105,37 psiMaximum allowable pressure (MAP) = 206,18 psi

K (Corroded)K=(1/6)*[2 + (D / (2*h)) 2]=(1/6)*[2 + (42,25 / (2*10,625)) 2]=0,99218

K (New)

K=(1/6)*[2 + (D / (2*h)) 2]=(1/6)*[2 + (42 / (2*10,5)) 2]=1

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Design thickness for internal pressure, (Corroded at 150 F) Appendix 1-4(c)

t = P*D*K / (2*S*E - 0,2*P) + Corrosion= 100*42,25*0,99218 / (2*20.000*0,85 - 0,2*100) + 0,125= 0,2484"

The head internal pressure design thickness is 0,2484 ".

Maximum allowable working pressure, (Corroded at 150 F) Appendix 1-4(c)

P = 2*S*E*t / (K*D + 0,2*t) - P s= 2*20.000*0,85*0,13 / (0,99218*42,25 +0,2*0,13) - 0= 105,37 psi

The maximum allowable working pressure (MAWP) is 105,37 psi.

Maximum allowable pressure, (New at 50 F) Appendix 1-4(c)

P = 2*S*E*t / (K*D + 0,2*t) - P s= 2*20.000*0,85*0,255 / (1*42 +0,2*0,255) - 0= 206,18 psi

The maximum allowable pressure (MAP) is 206,18 psi.

% Extreme fiber elongation - UCS-79(d)

EFE = (75*t / R f)*(1 - R f / R o)= (75*0,375 / 7,3275)*(1 - 7,3275 / infinity)= 3,8383%

The extreme fiber elongation does not exceed 5%.

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Straight Flange on TOP HEAD


Component: Straight FlangeMaterial specification: SA-516 70 (II-D p. 18, ln. 19)Material impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 79,9 F, (coincident ratio = 0,424)Rated MDMT of -99,9F is limited to -55F by UCS-66(b)(2)



Static liquid head:

P s = 0 psi (SG = 0,8, H s = 0",Operatinghead)

P th = 1,52 psi (SG = 1, H s = 42,0625",Horizontal test head)

Corrosion allowance Inner C = 0,125" Outer C = 0"

Design MDMT = -20 F No impact test performedRated MDMT = -55 F Material is not normalized

Material is produced to Fine Grain PracticePWHT is not performed

Radiography: Longitudinal joint - Seamless No RTCircumferential joint - Spot UW-11(b) Type 1

Estimated weight New = 28,3 lb corr = 18,9 lbCapacity New = 12 US gal corr = 12,14 US gal

ID = 42"

LengthLc= 2"

t = 0,375"

Design thickness, (at 150 F) UG-27(c)(1)

t = P*R / (S*E - 0,60*P) + Corrosion= 100*21,125 / (20.000*0,85 - 0,60*100) + 0,125= 0,2498"

Maximum allowable working pressure, (at 150 F) UG-27(c)(1)

P = S*E*t / (R + 0,60*t) - P s= 20.000*0,85*0,25 / (21,125 + 0,60*0,25) - 0= 199,76 psi

Maximum allowable pressure, (at 50 F) UG-27(c)(1)

P = S*E*t / (R + 0,60*t)= 20.000*0,85*0,375 / (21 + 0,60*0,375)= 300,35 psi

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S cHN = min(B, S) = 15.265 psi

Allowable Compressive Stress, Cold and New- S cCN , (table CS-2)A = 0,125 / (R o / t)

= 0,125 / (21,375 / 0,375)= 0,002193

B = 15.265 psi

S = 20.000 / 1,00 = 20.000 psiS cCN = min(B, S) = 15.265 psi

Allowable Compressive Stress, Cold and Corroded- S cCC , (table CS-2)A = 0,125 / (R o / t)

= 0,125 / (21,375 / 0,25)= 0,001462

B = 13.713 psi

S = 20.000 / 1,00 = 20.000 psi

S cCC = min(B, S) = 13.713 psi

Allowable Compressive Stress, Vacuum and Corroded- S cVC , (tableCS-2)A = 0,125 / (R o / t)

= 0,125 / (21,375 / 0,25)= 0,001462

B = 13.713 psi

S = 20.000 / 1,00 = 20.000 psi

S cVC = min(B, S) = 13.713 psi

Operating, Hot & Corroded, Wind, Bottom Seam

tp = P*R / (2*S t*Ks*Ec + 0,40*|P|) (Pressure)= 100*21,125 / (2*20.000*1,20*0,85 + 0,40*|100|)= 0,0517"

tm = M / ( *Rm2*St*Ks*Ec) (bending)= 169 / ( *21,25 2*20.000*1,20*0,85)= 0"

tw = W / (2* *Rm*St*Ks*Ec) (Weight)= 141,2 / (2* *21,25*20.000*1,20*0,85)= 0,0001"

tt = tp + t m - tw(total required,tensile)

= 0,0517 + 0 - (0,0001)= 0,0517"

tc = |t mc + t wc - tpc |(total, nettensile)

= |0 + (0,0001) - (0,0517)|= 0,0517"

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Maximum allowable working pressure, Longitudinal Stress

P = 2*S t*Ks*Ec*(t - tm + t w) / (R - 0,40*(t - t m + t w))= 2*20.00 0*1,20*0,85*(0,25 - 0 + (0,0001)) / (21,125 - 0 ,40*(0,25 - 0 + (0,0001)))= 485,23 psi

Operating, Hot & New, Wind, Bottom Seam

tp = P*R / (2*S t*Ks*Ec + 0,40*|P|) (Pressure)= 100*21 / (2*20.000*1,20*0,85 + 0,40*|100|)= 0,0514"




= 0,0514 + 0 - (0,0001)= 0,0513"


= |0 + (0,0001) - (0,0514)|= 0,0513"


P = 2*S t*Ks*Ec*(t - tm + t w) / (R - 0,40*(t - t m + t w))= 2*20.00 0*1,20*0,85*(0,375 - 0 + (0,0001)) / (21 - 0,40*(0,3 75 - 0 + (0,0001)))= 733,96 psi

Hot Shut Down, Corroded, Wind, Bottom Seam

tp = 0" (Pressure)tm = M / ( *Rm2*Sc*Ks) (bending)

= 169 / ( *21,25 2*13.712,9*1,20)= 0"

tw = W / (2**Rm*Sc*Ks) (Weight)= 141,2 / (2* *21,25*13.712,9*1,20)

= 0,0001"tt = |t p + t m - tw| (total, net compressive)

= |0 + 0 - (0,0001)|= 0,0001"

tc = tmc + t wc - tpc (total required, compressive)= 0 + (0,0001) - (0)= 0,0001"

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Hot Shut Down, New, Wind, Bottom Seam


= 169 / ( *21,1875 2*15.264,57*1,20)= 0"

tw = W / (2**Rm*Sc*Ks) (Weight)= 223,2 / (2* *21,1875*15.264,57*1,20)= 0,0001"

tt = |t p + t m - tw| (total, net compressive)= |0 + 0 - (0,0001)|= 0,0001"

tc = tmc + t wc - tpc (total required, compressive)= 0 + (0, 0001) - (0)= 0,0001"

Empty, Corroded, Wind, Bottom Seam


= 169 / ( *21,25 2*13.712,9*1,20)= 0"




Empty, New, Wind, Bottom Seam


= 169 / ( *21,1875 2*15.264,57*1,20)= 0"

tw = W / (2**Rm*Sc*Ks) (Weight)

= 223,2 / (2* *21,1875*15.264,57*1,20)= 0,0001"



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Hot Shut Down, Corroded, Weight & Eccentric Moments Only, Bottom Seam


= 0 / ( *21,25 2*13.712,9*1,00)= 0"




Operating, Hot & Corroded, Seismic, Bottom Seam




tt = tp + t m - tw(total required,

tensile)= 0,0517 + 0 - (0,0001)= 0,0517"

twc = (1 + VAccel)*W / (2* *Rm*St*Ks*Ec) (Weight)= 1,20*141,2 / (2* *21,25*20.000*1,20*0,85)= 0,0001"


= |0 + (0,0001) - (0,0517)|= 0,0516"


P = 2*S t*Ks*Ec*(t - tm + t w) / (R - 0,40*(t - t m + t w))= 2*20.000*1,20*0,85*(0,25 - 0 + (0,0001)) / (21,125 - 0,40*(0,25 - 0 + (0,0001)))= 485,19 psi

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Operating, Hot & New, Seismic, Bottom Seam





= 0,0514 + 0 - (0,0001)= 0,0514"

twc = (1 + VAccel)*W / (2* *Rm*St*Ks*Ec) (Weight)= 1,20*223,2 / (2* *21,1875*20.000*1,20*0,85)= 0,0001"


= |0 + (0,0001) - (0,0514)|= 0,0513"


P = 2*S t*Ks*Ec*(t - tm + t w) / (R - 0,40*(t - t m + t w))= 2*20.00 0*1,20*0,85*(0,375 - 0 + (0,0001)) / (21 - 0,40*(0,375 - 0 + (0,0001)))= 733,92 psi

Hot Shut Down, Corroded, Seismic, Bottom Seam


= 692 / ( *21,25 2*13.712,9*1,20)= 0"


tt = |t p + t m - tw| (total, net compressive)

= |0 + 0 - (0,0001)|= 0"

twc = (1 + VAccel)*W / (2* *Rm*Sc*Ks) (Weight)= 1,20*141,2 / (2* *21,25*13.712,9*1,20)= 0,0001"


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Hot Shut Down, New, Seismic, Bottom Seam


= 791 / ( *21,1875 2*15.264,57*1,20)= 0"





Empty, Corroded, Seismic, Bottom Seam


= 602 / ( *21,25 2*13.712,9*1,20)= 0"


tt = |t p + t m - tw| (total, net compressive)= |0 + 0 - (0,0001)|= 0"



Empty, New, Seismic, Bottom Seam


= 697 / ( *21,1875 2*15.264,57*1,20)= 0"


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tc = tmc + t wc - tpc (total required, compressive)

= 0 + (0,0001) - (0)= 0,0001"

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BOTTOM HEAD

ASME Section VIII, Division 1, 2010 Edition, A11 Addenda

Component: Ellipsoidal HeadMaterial Specification: SA-516 70 (II-D p.18, ln. 19)Straight Flange governs MDMT


Static liquid head:

P s= 2,75 psi (SG=0,8, H s=95,25" Operating head)P th= 1,52 psi (SG=1, H s=42,0625" Horizontal test head)

Corrosion allowance: Inner C = 0,125" Outer C = 0"

Design MDMT = -20F No impact test performedRated MDMT = -55F Material is not normalized

Material is produced to fine grain practicePWHT is not performedDo not Optimize MDMT / Find MAWP

Radiography: Category A joints - Seamless No RTHead to shell seam - Spot UW-11(b) Type 1

Estimated weight*: new = 176,4 lb corr = 95 lbCapacity*: new = 54 US gal corr = 55,1 US gal* includes straight flange

Inner diameter = 42"Minimum head thickness = 0,255"Head ratio D/2h = 2 (new)Head ratio D/2h = 1,9882 (corroded)Straight flange length L sf = 2"Nominal straight flange thickness t sf = 0,375"Results Summary

The governing condition is internal pressure.Minimum thickness per UG-16 = 0,0625" + 0, 125" = 0,1875"Design thickness due to internal pressure (t) = 0,2518 "Maximum allowable working pressure (MAWP) = 102,62 psiMaximum allowable pressure (MAP) = 206,18 psi

K (Corroded)K=(1/6)*[2 + (D / (2*h)) 2]=(1/6)*[2 + (42,25 / (2*10,625)) 2]=0,99218

K (New)

K=(1/6)*[2 + (D / (2*h)) 2]=(1/6)*[2 + (42 / (2*10,5)) 2]=1

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26/137

Design thickness for internal pressure, (Corroded at 150 F) Appendix 1-4(c)

t = P*D*K / (2*S*E - 0,2*P) + Corrosion= 102,75*42,25*0,99218 / (2*20.000*0,85 - 0,2*102 ,75) + 0 ,125= 0,2518"

The head internal pressure design thickness is 0,2518 ".

Maximum allowable working pressure, (Corroded at 150 F) Appendix 1-4(c)

P = 2*S*E*t / (K*D + 0,2*t) - P s= 2*20.000*0,85*0,13 / (0,99218*42,25 +0,2*0,13) - 2,75= 102,62 psi

The maximum allowable working pressure (MAWP) is 102,62 psi.

Maximum allowable pressure, (New at 50 F) Appendix 1-4(c)

P = 2*S*E*t / (K*D + 0,2*t) - P s= 2*20.000*0,85*0,255 / (1*42 +0,2*0,255) - 0= 206,18 psi

The maximum allowable pressure (MAP) is 206,18 psi.




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27/137

Straight Flange on BOTTOM HEAD


Component: Straight FlangeMaterial specification: SA-516 70 (II-D p. 18, ln. 19)Material impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 75,6 F, (coincident ratio = 0,4344)Rated MDMT of -95,6F is limited to -55F by UCS-66(b)(2)



Static liquid head:

P s = 2,44 psi (SG = 0,8, H s =84,625",Operating head)

P th = 1,52 psi (SG = 1, H s = 42,0625",Horizontal test head)




Radiography: Longitudinal joint - Seamless No RTCircumferential joint - Spot UW-11(b) Type 1

Estimated weight New = 28,3 lb corr = 18,9 lbCapacity New = 12 US gal corr = 12,14 US gal

ID = 42"

LengthLc= 2"

t = 0,375"


t = P*R / (S*E - 0,60*P) + Corrosion= 102,44*21,125 / (20.000*0,85 - 0,60*102,44) + 0,125= 0,2528"


P = S*E*t / (R + 0,60*t) - P s= 20.000*0,85*0,25 / (21,125 + 0,60*0,25) - 2,44= 197,32 psi


P = S*E*t / (R + 0,60*t)= 20.000*0,85*0,375 / (21 + 0,60*0,375)= 300,35 psi

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28/137




Design thickness = 0,2528"

The governing condition is due to internal pressure.

The cylinder thickness of 0,375" is adequate.

Thickness Required Due to Pressure + External Loads

Con dition Pressure P (psi)

AllowableStress BeforeUG-23 StressIncrease ( psi)

Temperature ( F)

Corrosion C(in) Load

Req'd Thk Due toTension (in)

Req'd Thk D ue toCompressio n (in)

S t S c

Operating, Hot & Corroded 100 20.000 13.713 150 0,125Wind 0,0552 0,0458

Seismic 0,0536 0,0473

Operating, Hot & New 100 20.000 15.265 150 0 Wind 0,0547 0,0452

Seismic 0,0533 0,0462

Hot Shut Down, Corroded 0 20.000 13.713 150 0,125 Wind 0,0035 0,0073

Seismic 0,0018 0,0055

Hot Shut Down, New 0 20.000 15.265 150 0 Wind 0,0033 0,007

Seismic 0,0019 0,0058

Empty, Corroded 0 20.000 13.713 70 0,125 Wind 0,0035 0,0073

Seismic 0,001 0,0046

Empty, New 0 20.000 15.265 70 0 Wind 0,0033 0,007

Seismic 0,0011 0,0049

Hot Shut Down, Corroded, Weight& Eccentric Moments Only 0 20.000 13.713 150 0,125 Weight 0,0009 0,0027

Allowable Compressive Stress, Hot and Corroded- S cHC , (table CS-2)A = 0,125 / (R o / t)

= 0,125 / (21,375 / 0,25)= 0,001462

B = 13.713 psi

S = 20.000 / 1,00 = 20.000 psi

S cHC = min(B, S) = 13.713 psi

Allowable Compressive Stress, Hot and New- S cHN , (table CS-2)A = 0,125 / (R o / t)

= 0,125 / (21,375 / 0,375)= 0,002193

B = 15.265 psi

S = 20.000 / 1,00 = 20.000 psi

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= 0,125 / (21,375 / 0,375)= 0,002193

B = 15.265 psi



= 0,125 / (21,375 / 0,25)= 0,001462

B = 13.713 psi

S = 20.000 / 1,00 = 20.000 psi



= 0,125 / (21,375 / 0,25)= 0,001462

B = 13.713 psi

S = 20.000 / 1,00 = 20.000 psi




tm = M / ( *Rm2*St*Ks*Ec) (bending)= 136.397 / ( *21,25 2*20.000*1,20*0,85)= 0,0047"

tw = W / (2* *Rm*St*Ks*Ec) (Weight)= 3.255,6 / (2* *21,25*20.000*1,20*0,85)= 0,0012"


= 0,0517 + 0,0047 - (0,0012)= 0,0552"


= |0,0047 + (0,0012) - (0,0517)|= 0,0458"

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30/137


31/137

= 3.255,6 / (2* *21,25*13.712,9*1,20)= 0,0015"

tc = tmc + t wc - tpc (total required, compressive)= 0,005 8 + (0,0015) - (0)= 0,0073"


tp = 0" (Pressure)tm = M / ( *Rm2*St*Ks*Ec) (bending)

= 136.965 / ( *21,1875 2*20.000*1,20*0,85)= 0,0048"


tt = tp + t m - tw (total required, tensile)= 0 + 0,0048 - (0,0015)= 0,0033"

tmc = M / ( *Rm2*Sc*Ks) (bending)= 136.965 / ( *21,1875 2*15.264,57*1,20)= 0,0053"

twc = W / (2* *Rm*Sc*Ks) (Weight)= 4.069,2 / (2* *21,1875*15.264,57*1,20)= 0,0017"




= 136.397 / ( *21,25 2*20.000*1,20*0,85)= 0,0047"





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32/137




= 136.965 / ( *21,1875 2*20.000*1,20*0,85)= 0,0048"







tp = 0" (Pressure)tm = M / ( *Rm2*Sc*Ks) (bending)= 17.337 / ( *21,25 2*13.712,9*1,00)= 0,0009"

tw = W / (2**Rm*Sc*Ks) (Weight)= 3.255,6 / (2* *21,25*13.712,9*1,00)= 0,0018"

tt = |t p + t m - tw| (total, net compressive)= |0 + 0,0009 - (0,0018)|= 0,0009"

tc = tmc + t wc - tpc (total required, compressive)= 0,0009 + (0,0018) - (0)= 0,0027"



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tt

= tp + t

m - t

w

(total required,

tensile)= 0,0517 + 0,003 - (0,0012)= 0,0536"

twc = (1 + VAccel)*W / (2* *Rm*St*Ks*Ec) (Weight)= 1,20*3.255,6 / (2* *21,25*20.000*1,20*0,85)= 0,0014"


= |0,003 + (0,0014) - (0,0517)|= 0,0473"


P = 2*S t*Ks*Ec*(t - tm + t w) / (R - 0,40*(t - t m + t w))= 2*20.00 0*1,20*0,85*(0,25 - 0,003 + (0,0012)) / (21,125 - 0,40*(0,25 - 0,003 + (0,0012)))= 481,57 psi




tw = W / (2**Rm*St*Ks*Ec) (Weight)= 4.069,2 / (2* *21,1875*20.000*1,20*0,85)= 0,0015"

tt = tp + t m - tw (total required, tensile)= 0,0514 + 0,0034 - (0,0015)= 0,0533"


tc = |t mc + t wc - tpc | (total, net tensile)= |0,0034 + (0,0018) - (0,0514)|= 0,0462"

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34/137


P = 2*S t*Ks*Ec*(t - tm + t w) / (R - 0,40*(t - t m + t w))= 2*20.00 0*1,20*0,85*(0,375 - 0,0034 + (0,0015)) / (21 - 0,40*( 0,375 - 0,0034 + (0,0015)))= 730,07 psi


tp = 0" (Pressure)tm = M / ( *Rm2*St*Ks*Ec) (bending)= 87.555 / ( *21,25 2*20.000*1,20*0,85)= 0,003"



tmc = M / ( *Rm2

*Sc*Ks) (bending)= 87.555 / ( *21,25 2*13.712,9*1,20)= 0,0038"

twc = (1 + VAccel)*W / (2* *Rm*Sc*Ks) (Weight)= 1,20*3.255,6 / (2* *21,25*13.712,9*1,20)= 0,0018"




= 97.684 / ( *21,1875 2*20.000*1,20*0,85)= 0,0034"


tt = tp + t m - tw (total required, tensile)= 0 + 0,0034 - (0,0015)

= 0,0019"tmc = M / ( *Rm2*Sc*Ks) (bending)

= 97.684 / ( *21,1875 2*15.264,57*1,20)= 0,0038"



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35/137

= 0,003 8 + (0,002) - (0)= 0,0058"



= 64.918 / ( *21,25 2*20.000*1,20*0,85)

= 0,0022"tw = W / (2* *Rm*St*Ks*Ec) (Weight)

= 3.255,6 / (2* *21,25*20.000*1,20*0,85)= 0,0012"







= 74.968 / ( *21,1875 2*20.000*1,20*0,85)= 0,0026"






34/136


36/137

Cylinder #1


Component: CylinderMaterial specification: SA-516 70 (II-D p. 18, ln. 19)Material impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 45,6 F, (coincident ratio = 0,5717)Rated MDMT of -65,6F is limited to -55F by UCS-66(b)(2)



Static liquid head:

P s = 0,83 psi (SG = 0,8, H s = 28,625",Operating head)

P th = 1,52 psi (SG = 1, H s = 42,125", Horizontal testhead)




Radiography: Longitudinal joint - Spot UW-11(b) Type 1Top circumferential joint - Spot UW-11(b) Type 1Bottom circumferential joint - Spot UW-11(b) Type 1

Estimated weight New = 1.097,9 lb corr = 660,7 lbCapacity New = 579,2 US gal corr = 586,1 US gal

ID = 42,125"

LengthLc= 96"

t = 0,3125"




P = S*E*t / (R + 0,60*t) - P s= 20.000*0,85*0,1875 / (21,1875 + 0,60*0,1875) - 0,83= 148,82 psi


P = S*E*t / (R + 0,60*t)= 20.000*0,85*0,3125 / (21,0625 + 0,60*0,3125)= 250 psi

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Temperature ( F)




S t S c


Seismic 0,0525 0,049


Seismic 0,0522 0,0482


Seismic 0,0006 0,0039


Seismic 0,0006 0,0039


Seismic 0,0004 0,0036

Empty, New 0 20.000 14.618 70 0 Wind 0,0014 0,0045

Seismic 0,0004 0,0037



= 0,125 / (21,375 / 0,1875)= 0,001096

B = 12.629 psi

S = 20.000 / 1,00 = 20.000 psi



= 0,125 / (21,375 / 0,3125)= 0,001827

B = 14.618 psi

S = 20.000 / 1,00 = 20.000 psi

36/136


38/137



= 0,125 / (21,375 / 0,3125)= 0,001827

B = 14.618 psi



= 0,125 / (21,375 / 0,1875)= 0,001096

B = 12.629 psi

S = 20.000 / 1,00 = 20.000 psi



= 0,125 / (21,375 / 0,1875)= 0,001096

B = 12.629 psi

S = 20.000 / 1,00 = 20.000 psi







= 0,0519 + 0,0026 - (0,001)= 0,0534"


= |0,0026 + (0,001) - (0,0519)|= 0,0482"

37/136


39/137


P = 2*S t*Ks*Ec*(t - tm + t w) / (R - 0,40*(t - t m + t w))= 2*20.00 0*1,20*0,85*(0,1875 - 0,0026 + (0,001)) / (21, 1875 - 0,40*(0,1875 - 0,0026 + (0,001)))= 359,3 psi






= 0,0516 + 0,0026 - (0,0012)= 0,053"


= |0,0026 + (0,0012) - (0,0516)|= 0,0477"


P = 2*S t*Ks*Ec*(t - tm + t w) / (R - 0,40*(t - t m + t w))= 2*20.00 0*1,20*0,85*(0,3125 - 0,0026 + (0,0012)) / (21,062 5 - 0,40*(0,3125 - 0,0026 + (0,0012)))= 606,21 psi



= 75.629 / ( *21,2813 2*20.000*1,20*0,85)= 0,0026"

tw = W / (2* *Rm*St*Ks*Ec) (Weight)= 2.827,1 / (2* *21,2813*20.000*1,20*0,85)

= 0,001"tt = tp + t m - tw (total required, tensile)

= 0 + 0,0026 - (0,001)= 0,0016"


twc = W / (2* *Rm*Sc*Ks) (Weight)

38/136


40/137

= 2.827,1 / (2* *21,2813*12.628,7*1,20)= 0,0014"




= 76.153 / ( *21,2188 2*20.000*1,20*0,85)= 0,0026"








= 75.629 / ( *21,2813 2*20.000*1,20*0,85)= 0,0026"





39/136


41/137




= 76.153 / ( *21,2188 2*20.000*1,20*0,85)= 0,0026"













40/136


42/137



tt

= tp + t

m - t

w

(total required,

tensile)= 0,0519 + 0,0017 - (0,001)= 0,0525"



= |0,0017 + (0,0012) - (0,0519)|= 0,049"








= 0,0516 + 0,0019 - (0,0012)= 0,0522"



= |0,0019 + (0,0015) - (0,0516)|= 0,0482"

41/136


43/137







tmc = M / ( *Rm2

*Sc*Ks) (bending)= 48.485 / ( *21,2813 2*12.628,7*1,20)= 0,0022"





= 54.053 / ( *21,2188 2*20.000*1,20*0,85)= 0,0019"




= 54.053 / ( *21,2188 2*14.617,56*1,20)= 0,0022"



42/136


44/137

= 0,002 2 + (0,0017) - (0)= 0,0039"



= 42.492 / ( *21,2813 2*20.000*1,20*0,85)


= 2.827,1 / (2* *21,2813*20.000*1,20*0,85)= 0,001"







= 47.837 / ( *21,2188 2*20.000*1,20*0,85)= 0,0017"






43/136


45/137

Cylinder #2


Component: CylinderMaterial specification: SA-516 70 (II-D p. 18, ln. 19)Material impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 44,6 F, (coincident ratio = 0,5806)Rated MDMT of -64,6F is limited to -55F by UCS-66(b)(2)



Static liquid head:

P s = 2,39 psi (SG = 0,8, H s = 82,625",Operating head)

P th = 1,52 psi (SG = 1, H s = 42,125", Horizontal testhead)




Radiography: Longitudinal joint - Spot UW-11(b) Type 1Top circumferential joint - Spot UW-11(b) Type 1Bottom circumferential joint - Spot UW-11(b) Type 1

Estimated weight New = 635,1 lb corr = 382,2 lbCapacity New = 325,8 US gal corr = 329,68 US gal

ID = 42,125"

LengthLc= 54"

t = 0,3125"




P = S*E*t / (R + 0,60*t) - P s= 20.000*0,85*0,1875 / (21,1875 + 0,60*0,1875) - 2,39= 147,26 psi


P = S*E*t / (R + 0,60*t)= 20.000*0,85*0,3125 / (21,0625 + 0,60*0,3125)= 250 psi

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46/137










Temperature ( F)




S t S c


Seismic 0,0537 0,0474


Seismic 0,0535 0,0464


Seismic 0,0018 0,006


Seismic 0,0019 0,006


Seismic 0,0011 0,0049

Empty, New 0 20.000 14.618 70 0 Wind 0,0033 0,0072

Seismic 0,0011 0,0051



= 0,125 / (21,375 / 0,1875)= 0,001096

B = 12.629 psi

S = 20.000 / 1,00 = 20.000 psi



= 0,125 / (21,375 / 0,3125)= 0,001827

B = 14.618 psi

S = 20.000 / 1,00 = 20.000 psi

45/136


47/137



= 0,125 / (21,375 / 0,3125)= 0,001827

B = 14.618 psi



= 0,125 / (21,375 / 0,1875)= 0,001096

B = 12.629 psi

S = 20.000 / 1,00 = 20.000 psi



= 0,125 / (21,375 / 0,1875)= 0,001096

B = 12.629 psi

S = 20.000 / 1,00 = 20.000 psi







= 0,0519 + 0,0047 - (0,0012)= 0,0554"


= |0,0047 + (0,0012) - (0,0519)|= 0,046"

46/136


48/137


P = 2*S t*Ks*Ec*(t - tm + t w) / (R - 0,40*(t - t m + t w))= 2*20.00 0*1,20*0,85*(0,1875 - 0,0047 + (0,0012)) / (2 1,1875 - 0,40*(0,1875 - 0,0047 + (0,0012)))= 355,53 psi






= 0,0516 + 0,0047 - (0,0015)= 0,0548"


= |0,0047 + (0,0015) - (0,0516)|= 0,0453"





= 136.397 / ( *21,2813 2*20.000*1,20*0,85)= 0,0047"

tw = W / (2* *Rm*St*Ks*Ec) (Weight)= 3.236,7 / (2* *21,2813*20.000*1,20*0,85)

= 0,0012"tt = tp + t m - tw (total required, tensile)

= 0 + 0,0047 - (0,0012)= 0,0035"


twc = W / (2* *Rm*Sc*Ks) (Weight)

47/136


49/137

= 3.236,7 / (2* *21,2813*12.628,7*1,20)= 0,0016"




= 136.965 / ( *21,2188 2*20.000*1,20*0,85)= 0,0047"








= 136.397 / ( *21,2813 2*20.000*1,20*0,85)= 0,0047"





48/136


50/137




= 136.965 / ( *21,2188 2*20.000*1,20*0,85)= 0,0047"













49/136


51/137



tt

= tp + t

m - t

w

(total required,

tensile)= 0,0519 + 0,003 - (0,0012)= 0,0537"



= |0,003 + (0,0014) - (0,0519)|= 0,0474"








= 0,0516 + 0,0034 - (0,0015)= 0,0535"



= |0,0034 + (0,0018) - (0,0516)|= 0,0464"

50/136


52/137







tmc = M / ( *Rm2

*Sc*Ks) (bending)= 87.555 / ( *21,2813 2*12.628,7*1,20)= 0,0041"





= 97.684 / ( *21,2188 2*20.000*1,20*0,85)= 0,0034"




= 97.684 / ( *21,2188 2*14.617,56*1,20)= 0,0039"



51/136


53/137

= 0,003 9 + (0,0021) - (0)= 0,006"



= 64.918 / ( *21,2813 2*20.000*1,20*0,85)


= 3.236,7 / (2* *21,2813*20.000*1,20*0,85)= 0,0012"







= 74.968 / ( *21,2188 2*20.000*1,20*0,85)= 0,0026"






52/136


54/137

ENTRADA (N1)


tw(lower) = 0,3125 inLeg 41 = 0,375 in

Note: round inside edges per UG-76(c)

Location and OrientationLocated on: Cylinder #1Orientation: 270Nozzle center line offset to datum line: 80 inEnd of nozzle to shell center: 27,375 inPasses through a Category A joint: No

NozzleMaterial specification: SA-106 B Smls pipe (II-D p. 10, ln. 40)Description: NPS 6 Sch 40 (Std)Inside diameter, new: 6,065 in

Nominal wall thickness: 0,28 inCorrosion allowance: 0,125 inProjection available outside vessel, Lpr: 2,5 inProjection available outside vessel to flange face, Lf: 6 inLocal vessel minimum thickness: 0,3125 inLiquid static head included: 0,1634 psiLongitudinal joint efficiency: 1

ASME B16.5-2009 FlangeDescription: NPS 6 Class 150 WN A105

Bolt Material: SA-193 B7 Bolt


55/137

Reinforcement Calculations for Internal Pressure

UG-37 Area Calculation Summary (in 2)For P = 100,16 psi @ 150 F

The opening is adequately reinforced

UG-45 NozzleWall

ThicknessSummary (in)The nozzle passes

UG-45

Arequired

Aavailable A1 A2 A3 A5

Awelds treq tmin

0,6769 0,7189 0,5083 0,0904 -- -- 0,1202 0,2314 0,245

UG-41 Weld Failure Path Analysis Summary

The nozzle is exempt from weld strength calculationsper UW-15(b)(1)

UW-16 Weld Sizi ng Sum mary

Weld description Required weld

throat size (in)

Actual weld

throat size (in)Status

Nozzle to shell fillet (Leg 41 ) 0,1085 0,2625 weld size is adequate

Calculations for internal pressure 100,16 psi @ 150 F

Fig UCS-66.2 general note (1) applies.

Nozzle is impact test exempt to -155 F per UCS-66(b)(3) (coincident ratio = 0,1547).

Nozzle UCS-66 governing thk: 0,245 inNozzle rated MDMT: -155 FParallel Limit of reinforcement per UG-40

LR = MAX(d, R n + (t n - C n) + (t - C))= MAX(6,315, 3,1575 + (0,28 - 0,125) + (0,3125 - 0,125))= 6,315 in

Outer Normal Limit of reinforcement per UG-40

LH = MIN(2,5*(t - C), 2,5*(t n - C n) + t e)= MIN(2,5*(0,3125 - 0,125), 2,5*(0,28 - 0,125) + 0)= 0,3875 in

Nozzle required thickness per UG-27(c)(1)

trn = P*R n / (S n*E - 0,6*P)= 100,1634*3,1575 / (17.100*1 - 0,6*100,1634)= 0,0186 in

Required thickness t r from UG-37(a)

tr = P*R / (S*E - 0,6*P)

54/136


56/137

= 100,1634*21,1875 / (20.000*1 - 0,6*100,1634)= 0,1064 in

Area required per UG-37(c)

Allowable stresses: S n = 17.100, S v = 20.000 psi

fr1 = lesser of 1 or S n / S v = 0,855


A = d*tr*F + 2*tn*tr*F*(1 - fr1)= 6,315*0,1064*1 + 2*0,155*0,1064*1*(1 - 0,855)= 0,6769 in2

Area available from FIG. UG-37.1

A1 = larger of the following= 0,5083 in2

= d*(E 1*t - F*tr) - 2*tn*(E1*t - F*tr)*(1 - f r1)= 6,315*(1*0,1875 - 1*0,1064) - 2*0,155*(1*0,1875 - 1*0,1064)*(1 - 0,855)= 0,5083 in 2

= 2*(t + t n)*(E1*t - F*tr) - 2*tn*(E1*t - F*tr)*(1 - fr1)= 2*(0,1875 + 0,155)*(1*0,1875 - 1 *0,106 4) - 2*0,155*(1*0,1875 - 1*0,1064)*(1 - 0,855)= 0,0519 in 2

A2 = smaller of the following= 0,0904 in2

= 5*(tn - t rn)*fr2*t= 5*(0,155 - 0,0186)*0,855*0,1875= 0,1093 in 2

= 5*(tn - t rn)*fr2*tn= 5*(0,155 - 0,0186)*0,855*0,155= 0,0904 in 2

A41 = Leg 2*fr2

= 0,3752

*0,855= 0,1202 in2

Area = A 1 + A2 + A41= 0,5083 + 0,0904 + 0,1202= 0,7189 in2

As Area >= A the reinforcement is adequate.

55/136


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UW-16(c) Weld Check

Fillet weld: t min = lesser of 0,75 or t n or t = 0,155 intc(min) = lesser of 0,25 or 0,7*t min = 0,1085 intc(actual) = 0,7*Leg = 0.7*0,375 = 0,2625 in

The fillet weld size is satisfactory.

Weld strength calculations are not required for this detail which conforms to Fig. UW-16.1, sketch (c-e).

UG-45 Nozzle Neck Thickness Check

ta UG-27 = P*R / (S*E - 0,6*P) + Corrosion= 100,1634*3,1575 / (17.100*1 - 0,6*100,1634) + 0,125= 0,1436 in

ta = max[ t a UG-27 , t a UG-22 ]

= max[ 0,1436 , 0 ]= 0,1436 in

tb1 = P*R / (S*E - 0,6*P) + Corrosion= 100,1634*21,1875 / (20.000*1 - 0,6*100,1634) + 0,125= 0,2314 in

tb1 = max[ t b1 , t b UG16 ]= max[ 0,2314 , 0,1875 ]= 0,2314 in

tb = min[ t b3 , t b1 ]= min[ 0,37 , 0,2314 ]= 0,2314 in

tUG-45 = max[ t a , t b ]= max[ 0,1436 , 0,2314 ]= 0,2314 in

Available nozzle wall thickness new, t n = 0,875*0,28 = 0,245 in

The nozzle neck thickness is adequate.

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SALIDA DE GAS (N2)


tw(lower) = 0,255 inLeg 41 = 0,3125 intw(upper) = 0,3125 inLeg 42 = 0,25 in

Dp = 12,625 inte = 0,3125 in


Location and OrientationLocated on: TOP HEADOrientation: 0End of nozzle to datum line: 168,5313 inCalculated as hillside: NoDistance to head center, R: 0 inPasses through a Category A joint: No

NozzleMaterial specification: SA-106 B Smls pipe (II-D p. 10, ln. 40)Description: NPS 8 Sch 40 (Std)

Inside diameter, new: 7,981 inNominal wall thickness: 0,322 inCorrosion allowance: 0,125 inProjection available outside vessel, Lpr: 2 inProjection available outside vessel to flange face, Lf: 6 inLocal vessel minimum thickness: 0,255 inLiquid static head included: 0 psiLongitudinal joint efficiency: 1

Reinforcing Pad

Material specification: SA-516 70 (II-D p. 18, ln. 19)Diameter: 12,625 inIs split: No

ASME B16.5-2009 FlangeDescription: NPS 8 Class 150 WN A105Bolt Material: SA-193 B7 Bolt


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Liquid static head: 0 psiMAWP rating: 272,5 psi @ 150FMAP rating: 285 psi @ 50FHydrotest rating: 450 psi @ 50FPWHT performed: NoCircumferential joint radiography: Spot UW-11(b) Type 1

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UG-37 Area Calculation Summary (in 2)For P = 100 psi @ 150 F

The opening is adequately reinforced

UG-45 NozzleWall


UG-45

Arequired


Awelds treq tmin

0,7836 1,7048 0,2898 0,096 -- 1,25 0,069 0,2299 0,2818

UG-41 Weld Failure Path Analysis Summary (lb f)All failu re paths ar e st ronger than th e applicable w eld loads

Weld loadW

Weld loadW1-1

Path 1-1strength

Weld loadW2-2

Path 2-2strength

Weld loadW3-3

Path 3-3strength

10.115,69 28.300 79.804,67 2.925,86 124.201,53 29.175,86 74.653,27

UW-16 Weld Sizin g Sum mary

Weld description Required weldsize (in)Actual weld

size (in) Status

Nozzle to pad fillet (Leg 41 ) 0,1379 0,2188 weld size is adequate

Pad to shell fillet (Leg 42 ) 0,065 0,175 weld size is adequate

Nozzle to pad groove (Upper) 0,1379 0,3125 weld size is adequate

Calculations for internal pressure 100 psi @ 150 F


Nozzle impact test exemption temperature from Fig UCS-66 Curve B = -20 F

Fig UCS-66.1 MDMT reduction = 27,3 F, (coincident ratio = 0,7273).Pad impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 27,3 F, (coincident ratio = 0,7273).

Nozzle UCS-66 governing thk: 0,2818 inNozzle rated MDMT: -47,3 FPad UCS-66 governing thickness: 0,2818 inPad rated MDMT: -47,3 FParallel Limit of reinforcement per UG-40



LH = MIN(2,5*(t - C), 2,5*(t n - C n) + t e)= MIN(2,5*(0,255 - 0,125), 2,5*(0,322 - 0,125) + 0,3125)= 0,325 in

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trn = P*R n / (S n*E - 0,6*P)= 100*4,1155 / (17.100*1 - 0,6*100)= 0,0242 in

Required thickness t r from UG-37(a)(c)

tr = P*K1*D / (2*S*E - 0,2*P)= 100*0,8947*42,25 / (2*20.000*1 - 0,2*100)= 0,0946 in

Area required per UG-37(c)

Allowable stresses: S n = 17.100, S v = 20.000, S p = 20.000 psi


fr2

= lesser of 1 or Sn / S

v = 0,855

fr3 = lesser of f r2 or S p / S v = 0,855

fr4 = lesser of 1 or S p / S v = 1

A = d*tr*F + 2*tn*tr*F*(1 - fr1)= 8,231*0,0946*1 + 2*0,197*0,0946*1*(1 - 0,855)= 0,7836 in2

Area available from FIG. UG-37.1

A1 = larger of the following= 0,2898 in2

= d*(E 1*t - F*tr) - 2*tn*(E1*t - F*tr)*(1 - f r1)= 8,231*(1*0,13 - 1*0,0946) - 2*0,197*(1*0,13 - 1*0,0946)*(1 - 0,855)= 0,2898 in 2

= 2*(t + t n)*(E1*t - F*tr) - 2*tn*(E1*t - F*tr)*(1 - fr1)= 2*(0,13 + 0,197)*(1*0,13 - 1*0,09 46) - 2*0,197*(1*0,13 - 1*0,0946)*(1 - 0,855)= 0,0212 in 2

A2 = smaller of the following= 0,096 in2

= 5*(tn - t rn)*fr2*t= 5*(0,197 - 0,0242)*0,855*0,13= 0,096 in 2

= 2*(tn - t rn)*(2,5*tn + t e )*fr2= 2*(0,197 - 0,0242)*(2,5*0,197 + 0,3125)*0,855

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= 0,2379 in 2

A41 = Leg 2*fr3= 0,0875 2*0,855= 0,0065 in2

(Part of the weld is outside of the limits)

A42 = Leg 2*fr4= 0,25 2*1= 0,0625 in2

A5 = (Dp - d - 2*t n)*te*fr4= (12,625 - 8,231 - 2*0,197)*0,3125*1= 1,25 in2

Area = A1 + A

2 + A

41 + A

42 + A

5= 0,2898 + 0,096 + 0,0065 + 0,0625 + 1,25= 1,7048 in2

As Area >= A the reinforcement is adequate.

UW-16(c)(2) Weld Check

Inner fillet: t min = lesser of 0,75 or t n or t e = 0,197 intc(min) = lesser of 0,25 or 0,7*t min = 0,1379 intc(actual) = 0,7*Leg = 0.7*0,3125 = 0,21 88 in

Outer fillet: t min = lesser of 0,75 or t e or t = 0,13 intw(min) = 0,5*t min = 0,065 intw(actual) = 0,7*Leg = 0.7*0,25 = 0,175 in


Interpretation VIII-1-83-66 has been applied.

ta UG-27 = P*R / (S*E - 0,6*P) + Corrosion= 100*4,1155 / (17.100*1 - 0,6*100) + 0,125= 0,1492 in

ta = max[ t a UG-27 , t a UG-22 ]= max[ 0,1492 , 0 ]= 0,1492 in

tb1 = 0,2299 in

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tb = min[ t b3 , t b1 ]= min[ 0,4068 , 0,2299 ]= 0,2299 in




Allowable stresses in joints UG-45 and UW-15(c)

Groove weld in tension: 0,74*20.000 = 14.800 psiNozzle wall in shear: 0,7*17.100 = 11.970 psiInner fil let weld in shear: 0,49*17.100 = 8.379 psiOuter fi llet weld in shear: 0,49*20.000 = 9.800 psiUpper groove weld in tension: 0,74*20.000 = 14.800 psiStrength of welded joints:

(1) Inner fillet weld in shear( / 2)*Nozzle OD*Leg*S i = ( / 2)*8,625*0,3125*8.379 = 35.474,9 lb f

(2) Outer fillet weld in shear( / 2)*Pad OD*Leg*S o = ( / 2)*12,625*0,25*9.800 = 48.586,69 lb f

(3) Nozzle wall in shear( / 2)*Mean nozzle dia*t n*Sn = ( / 2)*8,428*0,197*11.970 = 31.217,98 lb f

(4) Groove weld in tension( / 2)*Nozzle OD*t w*Sg = ( / 2)*8,625*0,13*14.800 = 26.066,58 lb f

(6) Upper groove weld in tension( / 2)*Nozzle OD*t w*Sg = ( / 2)*8,625*0,3125*14.800 = 62.660,05 lb f

Loading on welds per UG-41(b)(1)

W = (A - A 1 + 2*t n*fr1*(E1*t - F*tr))*Sv= (0,7836 - 0,2898 + 2*0,197*0,855*(1*0,13 - 1*0,0946))*20.000= 10.115,69 lbf

W1-1 = (A2 + A5 + A41 + A42 )*Sv= (0,096 + 1,25 + 0,0065 + 0,0625)*20.000= 28.300 lbf

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W2-2 = (A2 + A3 + A41 + A43 + 2*t n*t*fr1)*Sv= (0,096 + 0 + 0,0065 + 0 + 2*0,197*0,13*0,855)*20.000= 2.925,86 lbf

W3-3 = (A2 + A3 + A5 + A41 + A42 + A43 + 2*t n*t*fr1)*Sv

= (0,096 + 0 + 1,25 + 0,0065 + 0,0625 + 0 + 2*0,197*0,13*0,855)*20.000= 29.175,86 lbf

Load for path 1-1 lesser of W or W 1-1 = 10.115,69 lb fPath 1-1 through (2) & (3) = 48.586,69 + 31.217,98 = 79.804,67 lbfPath 1-1 is stronger than W so it is acceptable per UG-41(b)(2).

Load for path 2-2 lesser of W or W 2-2 = 2.925,86 lb fPath 2-2 through (1), (4), (6) = 35.474,9 + 26.066,58 + 62.660,05 = 124.201,53 lbfPath 2-2 is stronger than W 2-2 so it is acceptable per UG-41(b)(1 ).

Load for path 3-3 lesser of W or W3-3

= 10.115,69 lbfPath 3-3 through (2), (4) = 48.586,69 + 26.066,58 = 74.653,27 lbf

Path 3-3 is stronger than W so it is acceptable per UG-41(b)(2).

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ALIVIO (N3)


tw(lower) = 0,3125 inLeg 41 = 0,375 in



NozzleMaterial specification: SA-106 B Smls pipe (II-D p. 10, ln. 40)Description: NPS 3 Sch 80 (XS)Inside diameter, new: 2,9 in

Nominal wall thickness: 0,3 inCorrosion allowance: 0,125 inProjection available outside vessel, Lpr: 3,25 inProjection available outside vessel to flange face, Lf: 6 inLocal vessel minimum thickness: 0,3125 inLiquid static head included: 0 psiLongitudinal joint efficiency: 1




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UG-37 Area Calculation Summary(in 2)

For P = 100 psi @ 150 F

UG-45 NozzleWall


UG-45

Arequired


Awelds treq tmin

This nozzle is exempt from areacalculations per UG-36(c)(3)(a) 0,2313 0,2625




Weld description Required weldthroat size (in)Actual weld

throat size (in) Status





Nozzle UCS-66 governing thk: 0,2625 in

Nozzle rated MDMT: -155 FParallel Limit of reinforcement per UG-40





trn = P*R n / (S n*E - 0,6*P)= 100*1,575 / (17.100*1 - 0,6*100)= 0,0092 in

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tr = P*R / (S*E - 0,6*P)= 100*21,1875 / (20.000*1 - 0,6*100)= 0,1063 in

This opening does not require reinforcement per UG-36(c)(3)(a)

UW-16(c) Weld Check







tb1

= P*R / (S*E - 0,6*P) + Corrosion= 100*21,1875 / (20.000*1 - 0,6*100) + 0,125= 0,2313 in


tb = min[ t b3 , t b1 ]= min[ 0,314 , 0,2313 ]= 0,2313 in




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PDIT (N4A)


tw(lower) = 0,3125 inLeg 41 = 0,375 in



NozzleMaterial specification: SA-106 B Smls pipe (II-D p. 10, ln. 40)Description: NPS 2 Sch 160Inside diameter, new: 1,687 in

Nominal wall thickness: 0,344 inCorrosion allowance: 0,125 inProjection available outside vessel, Lpr: 3,5 inProjection available outside vessel to flange face, Lf: 6 inLocal vessel minimum thickness: 0,3125 inLiquid static head included: 0 psiLongitudinal joint efficiency: 1




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UG-37 Area Calculation Summary(in 2)

For P = 100 psi @ 150 F

UG-45 NozzleWall


UG-45

Arequired


Awelds treq tmin

This nozzle is exempt from areacalculations per UG-36(c)(3)(a) 0,2313 0,301




Weld description Required weldthroat size (in)Actual weld

throat size (in) Status





Nozzle UCS-66 governing thk: 0,301 in

Nozzle rated MDMT: -155 FParallel Limit of reinforcement per UG-40





trn = P*R n / (S n*E - 0,6*P)= 100*0,9685 / (17.100*1 - 0,6*100)= 0,0057 in

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tr = P*R / (S*E - 0,6*P)= 100*21,1875 / (20.000*1 - 0,6*100)= 0,1063 in

This opening does not require reinforcement per UG-36(c)(3)(a)

UW-16(c) Weld Check







tb1

= P*R / (S*E - 0,6*P) + Corrosion= 100*21,1875 / (20.000*1 - 0,6*100) + 0,125= 0,2313 in

tb1

calculos scrubber

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