Memoria de Calculo Recipiente a Presion

8/13/2019 Memoria de Calculo Recipiente a Presion

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CFE AGUA PRIETA SENER

Agua Prieta Sonora Mexico

MEMORIA DE CALCULO PARA TANQUE DE 36" DIAMETRO

Item: TANQUE LECHOS MIXTOS 36"Vessel No: LM-AGT-06

Customer: CFE SENER

Contract: XXXXX

Designer: Armando Iracheta Puente

Date: junio 2012

TANQUE AZ001 LECHOS MIXTOS


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Deficiencies Summary

Deficiencies for AIRE (B5)Physical interference between nozzles B5 and R1 (pad) detected.

Deficiencies for REGISTRO HOMBRE (R1)Physical interference between nozzles R1 (pad) and B5 detected.

Deficiencies for REGISTRO HOMBRE (R3)

Physical interference between nozzles R3 (pad) and B6 detected.

Deficiencies for SALIDA DE PRODUCTO (B6)Physical interference between nozzles B6 and R3 (pad) detected.

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Nozzle Schedule

Nozzle

markService Size

Materials

Nozzle Impact NormFineGrain

Pad Impact NormFineGrain

Flange

B1 ALIMENTACIONNPS 2 Sch 40

(Std)

SA-106 B Smls

pipeNo No No N/A N/A N/A N/A

WNA105

Class150

B2 SOSANPS 2 Sch 40

(Std)

SA-106 B Smls


WNA105

Class150

B3 ACIDONPS 2 Sch 40(Std)

SA-106 B Smlspipe

No No No N/A N/A N/A N/A

WN

A105Class150

B4 INTERMEDIONPS 2.5 Sch 40(Std)

SA-106 B Smlspipe


WN

A105Class

150

B5 AIRENPS 2 Sch 40(Std)

SA-106 B Smlspipe


WN

A105Class

150

B6SALIDA DE

PRODUCTO

NPS 2 Sch 40

(Std)

SA-106 B Smls


WNA105

Class150

B7 RESINAS 3.00 IDx2.25 SA-105 No No No N/A N/A N/A N/A N/A

M1 MIRILLASUPERIOR 3.00 IDx2.25 SA-105 No No No N/A N/A N/A N/A N/A

M2 MIRILLA INFERIOR 3.00 IDx2.25 SA-105 No No No N/A N/A N/A N/A N/A

MIRILLAINFERIOR

Nozzle #15 3.00 IDx2.25 SA-105 No No No N/A N/A N/A N/A N/A

R1 REGISTRO HOMBRENPS 24 Sch 20(Std)

SA-53 E/B Wldpipe

No No NoSA-285C

No No No

SO

A105Class150


SA-53 E/B Wldpipe

No No NoSA-285C

No No No

SO

A105Class

150


SA-53 E/B Wldpipe

No No NoSA-285C

No No No

SOA105Class

150

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Nozzle Summary

Nozzle

mark

OD

(in)

tn

(in)

Req tn

(in)A1? A2?

ShellReinforcement

Pad Corr

(in)

Aa/A

r(%)

Nom t

(in)

Design t

(in)

User t

(in)

Width

(in)

tpad(in)

B1 2.375 0.154 0.154 Yes Yes 0.235 N/A N/A N/A 0 Exempt

B2 2.375 0.154 0.154 Yes Yes 0.235 N/A 0.375 N/A N/A 0 Exempt



B5 2.375 0.154 0.154 No Yes 0.235* N/A N/A N/A 0 Exempt

B6 2.375 0.154 0.154 Yes Yes 0.235* 0.1517 N/A N/A 0 100.0

B7 7.5 2.25 0.235 Yes Yes 0.235 0.0915 N/A N/A 0 176.6

M1 7.5 2.25 0.235 Yes Yes 0.235 0.0915 N/A N/A 0 176.6

M2 7.5 2.25 0.235 Yes Yes 0.235 0.0915 N/A N/A 0 176.6

MIRILLA INFERIOR 7.5 2.25 0.235 Yes Yes 0.235 0.0915 N/A N/A 0 176.6

R1 24 0.375 0.2423 Yes Yes 0.235* 0.212 4 0.5 0 100.0

R2 20 0.375 0.1153 Yes Yes 0.235 0.1737 1.5 0.625 0 100.0

R3 20 0.375 0.2643 Yes Yes 0.235* 0.2313 4 0.5 0 100.0

tn: Nozzle thickness

Req tn: Nozzle thickness required per UG-45/UG-16

Nom t: Vessel wall thickness

Design t: Required vessel wall thickness due to pressure + corrosion allowance per UG-37

User t: Local vessel wall thickness (near opening)

Aa: Area available per UG-37, governing condition

Ar: Area required per UG-37, governing condition

Corr: Corrosion allowance on nozzle wall

* Head minimum thickness after forming

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Pressure Summary

Pressure Summary for Chamber bounded by F&D Head #2 and F&D Head #1

Identifier

P

Design

( psi)

T

Design

( F)

MAWP

( psi)

MAP

( psi)

MDMT

( F)

MDMT

Exemption

Impact

Tested

F&D Head #1 80 100 149.3 149.3 -55 Note 1 No

Straight Flange on F&D Head #1 80 100 186.38 186.38 -55 Note 2 No

Cylinder #1 80 150 175.14 175.14 -55 Note 3 No

Cylinder #2 80 100 175.14 175.14 -55 Note 3 No

Straight Flange on F&D Head #2 80 100 186.31 186.38 -55 Note 5 No

F&D Head #2 80 100 148.94 149.3 -55 Note 4 No

Legs #1 80 100 80 N/A N/A N/A N/A

ALIMENTACION (B1) 80 150 206.05 206.05 -55 Note 6 No

SOSA (B2) 80 100 285 285 -55 Note 6 No

ACIDO (B3) 80 100 285 285 -55 Note 6 No

INTERMEDIO (B4) 80 100 285 285 -55 Note 6 No

AIRE (B5) 80 100 255.79 255.79 -55 Note 6 No

SALIDA DE PRODUCTO (B6) 80 100 163.88 164.74 -55 Note 7 No

RESINAS (B7) 80 100 206.05 206.05 -55Nozzle N/A No

Pad Note 8 No

MIRILLA SUPERIOR (M1) 80 100 206.05 206.05 -55Nozzle N/A No

Pad Note 8 No

MIRILLA INFERIOR (M2) 80 100 206.05 206.05 -55Nozzle N/A No

Pad Note 8 No

Nozzle #15 (MIRILLA INFERIOR) 80 100 206.05 206.05 -55Nozzle N/A No

Pad Note 8 No

REGISTRO HOMBRE (R1) 80 100 158.36 158.36 -55Nozzle Note 9 No

Pad Note 10 No

REGISTRO HOMBRE (R2) 80 100 152.09 152.09 -55Nozzle Note 11 No

Pad Note 12 No

REGISTRO HOMBRE (R3) 80 100 172.21 172.83 -53.9Nozzle Note 13 No

Pad Note 14 No

Chamber design MDMT is -20 FChamber rated MDMT is -53.9 F @ 80 psi

Chamber MAWP hot & corroded is 80 psi @ 100 F

Chamber MAP cold & new is 149.3 psi @ 70 F

This pressure chamber is not designed for external pressure.

Notes for MDMT Rating:

Note # Exemption Details

1. Straight Flangegoverns MDMT

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2.

Material impact test exemption temperature from Fig UCS-66 Curve A = 18 F

Fig UCS-66.1 MDMT reduction = 125.9 F, (coincident ratio = 0.3660014)Rated MDMT is governed by UCS-66(b)(2)

UCS-66 governing thickness = 0.235 in

3.

Material impact test exemption temperature from Fig UCS-66 Curve A = 18 F



4. Straight Flangegoverns MDMT

5.Material impact test exemption temperature from Fig UCS-66 Curve A = 18 FFig UCS-66.1 MDMT reduction = 125.7 F, (coincident ratio = 0.3663309)

Rated MDMT is governed by UCS-66(b)(2)


6.Flange rating governs:Flange rated MDMT = -155 F

Bolts rated MDMT per Fig UCS-66 note (c) = -55 F

UCS-66(b)(3): Coincident ratio = 0.2807018

7.Flange rating governs:Flange rated MDMT = -155 FBolts rated MDMT per Fig UCS-66 note (c) = -55 F

UCS-66(b)(3): Coincident ratio = 0.2837414

8.

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


UCS-66 governing thickness = 0.235 in.

9.

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



10.Pad impact test exemption temperature from Fig UCS-66 Curve A = 18 FFig UCS-66.1 MDMT reduction = 73.6 F, (coincident ratio = 0.45719)



11.Nozzle impact test exemption temperature from Fig UCS-66 Curve B = -20 FFig UCS-66.1 MDMT reduction = 110.2 F, (coincident ratio = 0.38949)



12.Pad impact test exemption temperature from Fig UCS-66 Curve A = 18 FFig UCS-66.1 MDMT reduction = 110.2 F, (coincident ratio = 0.38949)



13.

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



14.Pad impact test exemption temperature from Fig UCS-66 Curve A = 18 F

Fig UCS-66.1 MDMT reduction = 71.9 F, (coincident ratio = 0.46072)UCS-66 governing thickness = 0.3281 in.

Design notes are available on the Settings Summarypage.

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Revision History

No. Date Operator Notes

0 6/ 1/2012 DIBUJO-7 New vessel created ASME Section VIII Division 1 [COMPRESS Build 7110]

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Settings Summary

COMPRESS Build 7110

Units: U.S. Customary

Datum Line Location: 0.00" from bottom seam

Design

ASME Section VIII Division 1, 2010 Edition

Design or Rating: Get Thickness from Pressure

Minimum thickness: 0.0625" per UG-16(b)

Design for cold shut down only: No

Design for lethal service (full radiography required): No

Design nozzles for: Design P, find nozzle MAWP and MAP

Corrosion weight loss: 100% of theoretical loss

UG-23 Stress Increase: 1.20

Skirt/legs stress increase: 1.0

Minimum nozzle projection: 6"

Juncture calculations for > 30 only: Yes

Preheat P-No 1 Materials > 1.25" and


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UG-22 Loadings

UG-22(a) Internal or External Design Pressure : Yes

UG-22(b) Weight of the vessel and normal contents under operating or test conditions: Yes

UG-22(c) Superimposed static reactions from weight of attached equipment (external loads): Yes

UG-22(d)(2) Vessel supports such as lugs, rings, skirts, saddles and legs: Yes

UG-22(f) Wind reactions: Yes

UG-22(f) Seismic reactions: Yes

UG-22(j) Test pressure and coincident static head acting during the test: Yes

Note: UG-22(b),(c) and (f) loads only considered when supports are present.

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Thickness Summary

Component

IdentifierMaterial Diameter

(in)

Length

(in)

Nominal t

(in)

Design t

(in)

Total Corrosion

(in)

Joint

ELoad

F&D Head #1 SA-285 C 36 OD 8.1929 0.235* 0.1264 0 0.85 Internal

Straight Flange on F&D Head #1 SA-285 C 36 OD 2 0.25 0.1077 0 0.85 Internal

Cylinder #1 SA-285 C 36 OD 47.375 0.235 0.1077 0 0.85 Internal

Cylinder #2 SA-285 C 36 OD 72 0.235 0.1077 0 0.85 Internal

Straight Flange on F&D Head #2 SA-285 C 36 OD 2 0.25 0.1078 0 0.85 Internal

F&D Head #2 SA-285 C 36 OD 8.1929 0.235* 0.1269 0 0.85 Internal

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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Weight Summary

Component

Weight ( lb) Contributed by Vessel Elements SurfaceAreaft2Metal

New*

Metal

Corroded*Insulation &

SupportsLining

Piping+ Liquid

OperatingLiquid

TestLiquid

F&D Head #1 72.1 72.1 0 0 0 0 329.7 8

Cylinder #1 353.7 353.7 0 0 0 0 1,695.9 37

Cylinder #2 504.4 504.4 0 0 0 0 2,642.5 53

F&D Head #2 81.3 81.3 0 0 0 321 320.9 9

Legs #1 455.3 455.3 0 0 0 0 0 36

TOTAL: 1,466.8 1,466.8 0 0 0 321 4,989 143

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

Component

Weight ( lb) Contributed by AttachmentsSurface Area

ft2Body FlangesNozzles &Flanges

PackedBeds

Ladders&Platforms

Trays &Supports

Rings &Clips

VerticalLoads

New Corroded New Corroded

F&D Head #1 0 0 822.6 822.6 0 0 0 0 0 13

Cylinder #1 0 0 7.5 7.5 0 0 0 52.4 0 4

Cylinder #2 0 0 657.4 657.4 0 0 0 20.7 0 14

F&D Head #2 0 0 595.6 595.6 0 0 0 0 0 11

Legs #1 0 0 0 0 0 0 0 0 0 0

TOTAL: 0 0 2,083 2,083 0 0 0 73.1 0 42

Vessel operating weight, Corroded: 3,944 lb

Vessel operating weight, New: 3,944 lb

Vessel empty weight, Corroded: 3,623 lb

Vessel empty weight, New: 3,623 lb

Vessel test weight, New: 8,612 lb

Vessel surface area: 186 ft2

Vessel center of gravity location - from datum - lift condition

Vessel Lift Weight, New: 3,623 lb

Center of Gravity: 51.2442"

Vessel Capacity

Vessel Capacity** (New): 572 US gal

Vessel Capacity** (Corroded): 572 US gal

**The vessel capacity does not include volume of nozzle, piping or other attachments.

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Long Seam Summary

Shell Long SeamAngles

Component Seam 1

Cylinder #1 15

Cylinder #2 45

Shell Plate Lengths

ComponentStartingAngle

Plate 1

Cylinder #1 15 112.3591"

Cylinder #2 45 112.3591"

*North is located at 180*Plate Lengths use the circumfrence of the vessel based on the mid diameter of the components

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Shell Rollout

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Hydrostatic Test

Shop test pressure determination for Chamber bounded by F&D Head #2 and F&D Head #1 based on MAWPper UG-99(b)

Shop hydrostatic test gauge pressure is 104 psi at 70 F (the chamber MAWP = 80 psi)

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

IdentifierLocal testpressure

psi

Test liquidstatic head

psi

UG-99stressratio

UG-99pressure

factor

Stressduring test

psi

Allowabletest stress

psi

Stressexcessive?

F&D Head #1 (1) 104.83 0.83 1 1.30 6,424 27,000 No

Straight Flange on F&D Head #1 104.83 0.83 1 1.30 7,495 27,000 No

Cylinder #1 106.54 2.54 1 1.30 8,107 27,000 No

Cylinder #2 109.139 5.139 1 1.30 8,305 27,000 No

Straight Flange on F&D Head #2 109.212 5.212 1 1.30 7,809 27,000 No

F&D Head #2 109.499 5.499 1 1.30 6,710 27,000 No

ACIDO (B3) 108.96 4.96 1 1.30 7,277 40,500 No

AIRE (B5) 104.514 0.514 1 1.30 7,292 40,500 No

ALIMENTACION (B1) 105.295 1.295 1 1.30 9,186 40,500 No

INTERMEDIO (B4) 108.189 4.189 1 1.30 7,016 40,500 No

MIRILLA INFERIOR (M2) 107.569 3.569 1 1.30 1,341 40,500 No

MIRILLA SUPERIOR (M1) 107.389 3.389 1 1.30 1,339 40,500 No

Nozzle #15 (MIRILLA INFERIOR) 108.454 4.454 1 1.30 1,352 40,500 No

REGISTRO HOMBRE (R1) 104.462 0.462 1 1.30 7,244 40,500 No



RESINAS (B7) 108.941 4.941 1 1.30 1,358 40,500 No

SALIDA DE PRODUCTO (B6) 110.006 6.006 1 1.30 9,460 40,500 No

SOSA (B2) 107.011 3.011 1 1.30 7,147 40,500 No

Notes:

(1) F&D Head #1 limits the UG-99 stress ratio.(2) PLstresses at nozzle openings have been estimated using the method described in PVP-Vol. 399, pages 77-82.

(3) 1.5*0.9*Syused as the basis for the maximum local primary membrane stress at the nozzle intersection PL.

The field test condition has not been investigated for the Chamber bounded by F&D Head #2 and F&D Head #1.

The test temperature of 70 F is warmer than the minimum recommended temperature of -23.9 F so the brittlefracture provision of UG-99(h) has been met.

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Cylinder #1


Component: Cylinder

Material specification: SA-285 C (II-D p. 6, ln. 42)Material impact test exemption temperature from Fig UCS-66 Curve A = 18 F



Internal design pressure: P = 80 psi @ 150 F

Static liquid head:

Ps = 0 psi (SG = 1, Hs= 0",Operating

head)

Ptv = 2.54 psi (SG = 1, Hs= 70.375",Vertical test head)

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

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

Material is not produced to Fine Grain Practice

PWHT is not performed

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

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

Estimated weight New = 353.7 lb corr = 353.7 lb

Capacity New = 203.34 US gal corr = 203.34 US gal

OD = 36"Length

Lc= 47.375"

t = 0.235"

Design thickness, (at 150 F) Appendix 1-1

t = P*Ro/ (S*E + 0.40*P) + Corrosion= 80*18 / (15,700*0.85 + 0.40*80) + 0

= 0.1077"

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

P = S*E*t / (Ro- 0.40*t) - Ps= 15,700*0.85*0.235 / (18 - 0.40*0.235) - 0= 175.14 psi

Maximum allowable pressure, (at 70 F) Appendix 1-1

P = S*E*t / (Ro- 0.40*t)= 15,700*0.85*0.235 / (18 - 0.40*0.235)

= 175.14 psi

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% Extreme fiber elongation - UCS-79(d)

EFE = (50*t / Rf)*(1 - Rf/ Ro)

= (50*0.235 / 17.8825)*(1 - 17.8825 / )

= 0.6571%

The extreme fiber elongation does not exceed 5%.

Design thickness = 0.1077"

The governing condition is due to internal pressure.

The cylinder thickness of 0.235" is adequate.

Thickness Required Due to Pressure + External Loads

ConditionPressure P (

psi)

Allowable StressBefore UG-23

Stress Increase (psi)

Temperature (F)

Corrosion C(in)

LoadReq'd Thk Due to

Tension (in)

Req'd Thk Dueto

Compression(in)

St Sc

Operating, Hot & Corroded 80 15,700 14,152 150 0 Wind 0.0441 0.0433

Seismic 0.0448 0.0422

Operating, Hot & New 80 15,700 14,152 150 0Wind 0.0441 0.0433

Seismic 0.0448 0.0422

Hot Shut Down, Corroded 0 15,700 14,152 150 0Wind 0.0002 0.0009

Seismic 0.0005 0.002

Hot Shut Down, New 0 15,700 14,152 150 0Wind 0.0002 0.0009

Seismic 0.0005 0.002

Empty, Corroded 0 15,700 14,152 70 0Wind 0.0002 0.0009

Seismic 0.0005 0.0019

Empty, New 0 15,700 14,152 70 0Wind 0.0002 0.0009

Seismic 0.0005 0.0019

Hot Shut Down, Corroded, Weight

& Eccentric Moments Only0 15,700 14,152 150 0 Weight 0.0008 0.0008

Allowable Compressive Stress, Hot and Corroded- ScHC, (table CS-2)

A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.235)

= 0.001632

B = 14,152 psi

S = 15,700 / 1.00 = 15,700 psi

ScHC = min(B, S) = 14,152 psi

Allowable Compressive Stress, Hot and New- ScHNScHN = ScHC

= 14,152 psi

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Allowable Compressive Stress, Cold and New- ScCN, (table CS-2)

A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.235)

= 0.001632

B = 14,152 psi

S = 15,700 / 1.00 = 15,700 psi

ScCN = min(B, S) = 14,152 psi

Allowable Compressive Stress, Cold and Corroded- ScCCScCC = ScCN

= 14,152 psi

Allowable Compressive Stress, Vacuum and Corroded- ScVC, (table CS-2)

A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.235)

= 0.001632

B = 14,152 psi

S = 15,700 / 1.00 = 15,700 psi

ScVC = min(B, S) = 14,152 psi

Operating, Hot & Corroded, Wind, Bottom Seam

tp = P*R / (2*St*Ks*Ec+ 0.40*|P|) (Pressure)

= 80*17.765 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"

tm = M / (*Rm2*St*Ks*Ec) (bending)

= 4,061 / (*17.88252*15,700*1.20*0.85)

= 0.0003"

tw = 0.6*W / (2**Rm*St*Ks*Ec) (Weight)

= 0.60*1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0004"

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

= 0.0443 + 0.0003 - (0.0004)

= 0.0441"

twc = W / (2**Rm*St*Ks*Ec) (Weight)

= 1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0007"

tc = |tmc+ twc- tpc| (total, net tensile)

= |0.0003 + (0.0007) - (0.0443)|

= 0.0433"

Maximum allowable working pressure, Longitudinal Stress

P = 2*St*Ks*Ec*(t - tm+ tw) / (R - 0.40*(t - tm+ tw))

= 2*15,700*1.20*0.85*(0.235 - 0.0003 + (0.0004)) / (17.765 - 0.40*(0.235 - 0.0003 + (0.0004)))

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= 426.26 psi

Operating, Hot & New, Wind, Bottom Seam


= 80*17.765 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"


= 4,061 / (*17.88252*15,700*1.20*0.85)

= 0.0003"


= 0.60*1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0004"


= 0.0443 + 0.0003 - (0.0004)

= 0.0441"


= 1,308.3 / (2**17.8825*15,700*1.20*0.85)= 0.0007"


= |0.0003 + (0.0007) - (0.0443)|

= 0.0433"



= 2*15,700*1.20*0.85*(0.235 - 0.0003 + (0.0004)) / (17.765 - 0.40*(0.235 - 0.0003 + (0.0004)))

= 426.26 psi

Hot Shut Down, Corroded, Wind, Bottom Seam

tp = 0" (Pressure)

tm = M / (*Rm2*Sc*Ks) (bending)

= 4,061 / (*17.88252*14,151.54*1.20)

= 0.0002"

tw = 0.6*W / (2**Rm*Sc*Ks) (Weight)

= 0.60*1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0004"

tt = |tp+ tm- tw| (total, net compressive)= |0 + 0.0002 - (0.0004)|

= 0.0002"

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

= 1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0007"

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

= 0.0002 + (0.0007) - (0)

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= 0.0009"

Hot Shut Down, New, Wind, Bottom Seam

tp = 0" (Pressure)


= 4,061 / (*17.88252*14,151.54*1.20)

= 0.0002"


= 0.60*1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0004"

tt = |tp+ tm- tw| (total, net compressive)

= |0 + 0.0002 - (0.0004)|

= 0.0002"


= 1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0007"

tc = tmc+ twc- tpc (total required, compressive)= 0.0002 + (0.0007) - (0)

= 0.0009"

Empty, Corroded, Wind, Bottom Seam

tp = 0" (Pressure)


= 4,061 / (*17.88252*14,151.54*1.20)

= 0.0002"


= 0.60*1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0004"


= |0 + 0.0002 - (0.0004)|

= 0.0002"


= 1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0007"


= 0.0002 + (0.0007) - (0)= 0.0009"

Empty, New, Wind, Bottom Seam

tp = 0" (Pressure)


= 4,061 / (*17.88252*14,151.54*1.20)

= 0.0002"

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= 0.60*1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0004"


= |0 + 0.0002 - (0.0004)|

= 0.0002"


= 1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0007"


= 0.0002 + (0.0007) - (0)

= 0.0009"

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

tp = 0" (Pressure)


= 199 / (*17.88252

*14,151.54*1.00)= 0"

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

= 1,308.3 / (2**17.8825*14,151.54*1.00)

= 0.0008"


= |0 + 0 - (0.0008)|

= 0.0008"


= 0 + (0.0008) - (0)

= 0.0008"

Operating, Hot & Corroded, Seismic, Bottom Seam


= 80*17.765 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"


= 19,659 / (*17.88252*15,700*1.20*0.85)

= 0.0012"

tw = W / (2**Rm*St*Ks*Ec) (Weight)= 1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0007"


= 0.0443 + 0.0012 - (0.0007)

= 0.0448"

twc = (1 + VAccel)*W / (2**Rm*St*Ks*Ec) (Weight)

= 1.20*1,308.3 / (2**17.8825*15,700*1.20*0.85)

20/240


22/241

= 0.0009"


= |0.0012 + (0.0009) - (0.0443)|

= 0.0422"



= 2*15,700*1.20*0.85*(0.235 - 0.0012 + (0.0007)) / (17.765 - 0.40*(0.235 - 0.0012 + (0.0007)))

= 425.03 psi

Operating, Hot & New, Seismic, Bottom Seam


= 80*17.765 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"


= 19,659 / (*17.88252*15,700*1.20*0.85)

= 0.0012"tw = W / (2**Rm*St*Ks*Ec) (Weight)

= 1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0007"


= 0.0443 + 0.0012 - (0.0007)

= 0.0448"


= 1.20*1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0009"


= |0.0012 + (0.0009) - (0.0443)|

= 0.0422"



= 2*15,700*1.20*0.85*(0.235 - 0.0012 + (0.0007)) / (17.765 - 0.40*(0.235 - 0.0012 + (0.0007)))

= 425.03 psi

Hot Shut Down, Corroded, Seismic, Bottom Seam

tp = 0" (Pressure)


= 19,659 / (*17.88252*15,700*1.20*0.85)

= 0.0012"

tw = W / (2**Rm*St*Ks*Ec) (Weight)

= 1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0007"

21/240


23/241


= 0 + 0.0012 - (0.0007)

= 0.0005"

tmc = M / (*Rm2*Sc*Ks) (bending)

= 19,659 / (*17.88252*14,151.54*1.20)

= 0.0012"

twc = (1 + VAccel)*W / (2**Rm*Sc*Ks) (Weight)

= 1.20*1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0008"


= 0.0012 + (0.0008) - (0)

= 0.002"

Hot Shut Down, New, Seismic, Bottom Seam

tp = 0" (Pressure)


= 19,659 / (*17.88252

*15,700*1.20*0.85)= 0.0012"


= 1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0007"


= 0 + 0.0012 - (0.0007)

= 0.0005"


= 19,659 / (*17.88252*14,151.54*1.20)

= 0.0012"


= 1.20*1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0008"


= 0.0012 + (0.0008) - (0)

= 0.002"

Empty, Corroded, Seismic, Bottom Seam

tp = 0" (Pressure)tm = M / (*Rm

2*St*Ks*Ec) (bending)

= 18,967 / (*17.88252*15,700*1.20*0.85)

= 0.0012"


= 1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0007"


22/240


24/241

= 0 + 0.0012 - (0.0007)

= 0.0005"


= 18,967 / (*17.88252*14,151.54*1.20)

= 0.0011"


= 1.20*1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0008"


= 0.0011 + (0.0008) - (0)

= 0.0019"

Empty, New, Seismic, Bottom Seam

tp = 0" (Pressure)


= 18,967 / (*17.88252*15,700*1.20*0.85)

= 0.0012"tw = W / (2**Rm*St*Ks*Ec) (Weight)

= 1,308.3 / (2**17.8825*15,700*1.20*0.85)

= 0.0007"


= 0 + 0.0012 - (0.0007)

= 0.0005"


= 18,967 / (*17.88252*14,151.54*1.20)

= 0.0011"


= 1.20*1,308.3 / (2**17.8825*14,151.54*1.20)

= 0.0008"


= 0.0011 + (0.0008) - (0)

= 0.0019"

23/240


25/241

Cylinder #2


Component: Cylinder





Static liquid head:

Ps = 0 psi (SG = 1, Hs= 0",Operating head)

Ptv = 5.14 psi (SG = 1, Hs= 142.375", Vertical testhead)


Design MDMT = -20 F No impact test performed

Rated MDMT = -55 F Material is not normalizedMaterial is not produced to Fine Grain PracticePWHT is not performed

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

Bottom circumferential joint - Spot UW-11(b) Type 1



OD = 36"

LengthLc

= 72"

t = 0.235"


t = P*Ro/ (S*E + 0.40*P) + Corrosion

= 80*18 / (15,700*0.85 + 0.40*80) + 0= 0.1077"


P = S*E*t / (Ro- 0.40*t) - Ps= 15,700*0.85*0.235 / (18 - 0.40*0.235) - 0= 175.14 psi


P = S*E*t / (Ro- 0.40*t)

= 15,700*0.85*0.235 / (18 - 0.40*0.235)= 175.14 psi

24/240


26/241


EFE = (50*t / Rf)*(1 - Rf/ Ro)

= (50*0.235 / 17.8825)*(1 - 17.8825 / )

= 0.6571%






ConditionPressure P

( psi)

AllowableStress BeforeUG-23 StressIncrease ( psi)

Temperature (F)

Corrosion C(in)

Location LoadReq'd Thk Dueto Tension (in)

Req'd Thk Due toCompression (in)

St Sc

Operating, Hot & Corroded 80 15,700 14,152 100 0Top Wind 0.0387 0.0348

Seismic 0.0401 0.0327

BottomWind 0.0381 0.0379

Seismic 0.0383 0.0381

Operating, Hot & New 80 15,700 14,152 100 0Top

Wind 0.0387 0.0348

Seismic 0.0401 0.0327


Seismic 0.0383 0.0381

Hot Shut Down, Corroded 0 15,700 14,152 100 0Top

Wind 0.001 0.0032

Seismic 0.0024 0.0056


Seismic 0.0006 0.0004

Hot Shut Down, New 0 15,700 14,152 100 0Top

Wind 0.001 0.0032

Seismic 0.0024 0.0056


Seismic 0.0006 0.0004

Empty, Corroded 0 15,700 14,152 70 0Top

Wind 0.001 0.0032

Seismic 0.0023 0.0054


Seismic 0.0004 0.0003

Empty, New 0 15,700 14,152 70 0Top

Wind 0.001 0.0032

Seismic 0.0023 0.0054


Seismic 0.0004 0.0003

Hot Shut Down, Corroded,Weight & Eccentric Moments

Only0 15,700 14,152 100 0

Top Weight 0.0006 0.0025

Bottom Weight 0.0005 0.0005

25/240


27/241


A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.235)

= 0.001632

B = 14,152 psi

S = 15,700 / 1.00 = 15,700 psi



= 14,152 psi


A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.235)

= 0.001632

B = 14,152 psi

S = 15,700 / 1.00 = 15,700 psi



= 14,152 psi


A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.235)

= 0.001632

B = 14,152 psi

S = 15,700 / 1.00 = 15,700 psi


Operating, Hot & Corroded, Wind, Above Support Point


= 80*17.765 / (2*15,700*1.20*1.00 + 0.40*|80|)

= 0.0377"


= 33,085 / (*17.88252*15,700*1.20*1.00)

= 0.0017"


= 0.60*2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0007"


26/240


28/241

= 0.0377 + 0.0017 - (0.0007)

= 0.0387"


= 2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0012"


= |0.0017 + (0.0012) - (0.0377)|

= 0.0348"



= 2*15,700*1.20*1.00*(0.235 - 0.0017 + (0.0007)) / (17.765 - 0.40*(0.235 - 0.0017 + (0.0007)))

= 498.85 psi

Operating, Hot & New, Wind, Above Support Point


= 80*17.765 / (2*15,700*1.20*1.00 + 0.40*|80|)= 0.0377"


= 33,085 / (*17.88252*15,700*1.20*1.00)

= 0.0017"


= 0.60*2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0007"


= 0.0377 + 0.0017 - (0.0007)

= 0.0387"


= 2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0012"


= |0.0017 + (0.0012) - (0.0377)|

= 0.0348"


P = 2*St*Ks*Ec*(t - tm+ tw) / (R - 0.40*(t - tm+ tw))= 2*15,700*1.20*1.00*(0.235 - 0.0017 + (0.0007)) / (17.765 - 0.40*(0.235 - 0.0017 + (0.0007)))

= 498.85 psi

Hot Shut Down, Corroded, Wind, Above Support Point

tp = 0" (Pressure)


= 33,085 / (*17.88252*15,700*1.20*1.00)

27/240


29/241

= 0.0017"


= 0.60*2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0007"


= 0 + 0.0017 - (0.0007)

= 0.001"


= 33,085 / (*17.88252*14,151.54*1.20)

= 0.0019"


= 2,483.2 / (2**17.8825*14,151.54*1.20)

= 0.0013"


= 0.0019 + (0.0013) - (0)

= 0.0032"

Hot Shut Down, New, Wind, Above Support Point

tp = 0" (Pressure)


= 33,085 / (*17.88252*15,700*1.20*1.00)

= 0.0017"


= 0.60*2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0007"


= 0 + 0.0017 - (0.0007)

= 0.001"


= 33,085 / (*17.88252*14,151.54*1.20)

= 0.0019"


= 2,483.2 / (2**17.8825*14,151.54*1.20)

= 0.0013"


= 0.0019 + (0.0013) - (0)= 0.0032"

Empty, Corroded, Wind, Above Support Point

tp = 0" (Pressure)


= 33,085 / (*17.88252*15,700*1.20*1.00)

= 0.0017"

28/240


30/241


= 0.60*2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0007"


= 0 + 0.0017 - (0.0007)

= 0.001"


= 33,085 / (*17.88252*14,151.54*1.20)

= 0.0019"


= 2,483.2 / (2**17.8825*14,151.54*1.20)

= 0.0013"


= 0.0019 + (0.0013) - (0)

= 0.0032"

Empty, New, Wind, Above Support Point

tp = 0" (Pressure)


= 33,085 / (*17.88252*15,700*1.20*1.00)

= 0.0017"


= 0.60*2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0007"


= 0 + 0.0017 - (0.0007)

= 0.001"


= 33,085 / (*17.88252*14,151.54*1.20)

= 0.0019"


= 2,483.2 / (2**17.8825*14,151.54*1.20)

= 0.0013"


= 0.0019 + (0.0013) - (0)

= 0.0032"

Hot Shut Down, Corroded, Weight & Eccentric Moments Only, Above Support Point

tp = 0" (Pressure)


= 13,062 / (*17.88252*14,151.54*1.00)

= 0.0009"


29/240


31/241

= 2,483.2 / (2**17.8825*14,151.54*1.00)

= 0.0016"


= |0 + 0.0009 - (0.0016)|

= 0.0006"


= 0.0009+ (0.0016) - (0)

= 0.0025"

Operating, Hot & Corroded, Wind, Below Support Point


= 80*17.765 / (2*15,700*1.20*1.00 + 0.40*|80|)

= 0.0377"


= 72 / (*17.88252*15,700*1.20*1.00)

= 0"

tw = W / (2**Rm*St*Ks*Ec) (Weight)= -933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0004"


= 0.0377 + 0 - (-0.0004)

= 0.0381"

twc = 0.6*W / (2**Rm*St*Ks*Ec) (Weight)

= 0.60*-933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0003"


= |0 + (-0.0003) - (0.0377)|

= 0.0379"



= 2*15,700*1.20*1.00*(0.235 - 0 + (-0.0004)) / (17.765 - 0.40*(0.235 - 0 + (-0.0004)))

= 500.14 psi

Operating, Hot & New, Wind, Below Support Point

tp = P*R / (2*St*Ks*Ec+ 0.40*|P|) (Pressure)= 80*17.765 / (2*15,700*1.20*1.00 + 0.40*|80|)

= 0.0377"


= 72 / (*17.88252*15,700*1.20*1.00)

= 0"


= -933.4 / (2**17.8825*15,700*1.20*1.00)

30/240


32/241

= -0.0004"


= 0.0377 + 0 - (-0.0004)

= 0.0381"


= 0.60*-933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0003"


= |0 + (-0.0003) - (0.0377)|

= 0.0379"



= 2*15,700*1.20*1.00*(0.235 - 0 + (-0.0004)) / (17.765 - 0.40*(0.235- 0 + (-0.0004)))

= 500.14 psi

Hot Shut Down, Corroded, Wind, Below Support Point

tp = 0" (Pressure)


= 72 / (*17.88252*15,700*1.20*1.00)

= 0"


= -933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0004"


= 0 + 0 - (-0.0004)

= 0.0004"


= 0.60*-933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0003"


= |0 + (-0.0003) - (0)|

= 0.0003"

Hot Shut Down, New, Wind, Below Support Point

tp = 0" (Pressure)tm = M / (*Rm

2*St*Ks*Ec) (bending)

= 72 / (*17.88252*15,700*1.20*1.00)

= 0"


= -933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0004"


31/240


33/241

= 0 + 0 - (-0.0004)

= 0.0004"


= 0.60*-933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0003"


= |0 + (-0.0003) - (0)|

= 0.0003"

Empty, Corroded, Wind, Below Support Point

tp = 0" (Pressure)


= 72 / (*17.88252*15,700*1.20*1.00)

= 0"


= -684.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0003"tt = tp+ tm- tw (total required, tensile)

= 0 + 0 - (-0.0003)

= 0.0003"


= 0.60*-684.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0002"


= |0 + (-0.0002) - (0)|

= 0.0002"

Empty, New, Wind, Below Support Point

tp = 0" (Pressure)


= 72 / (*17.88252*15,700*1.20*1.00)

= 0"


= -684.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0003"

tt = tp+ tm- tw (total required, tensile)= 0 + 0 - (-0.0003)

= 0.0003"


= 0.60*-684.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0002"


= |0 + (-0.0002) - (0)|

32/240


34/241

= 0.0002"

Hot Shut Down, Corroded, Weight & Eccentric Moments Only, Below Support Point

tp = 0" (Pressure)


= 72 / (*17.88252*15,700*1.00*1.00)

= 0"


= -933.4 / (2**17.8825*15,700*1.00*1.00)

= -0.0005"

tt = tp+ tm- tw(total required,

tensile)

= 0 + 0 - (-0.0005)

= 0.0005"

tc = |tmc+ twc- tpc|(total, net

tensile)

= |0+ (-0.0005) - (0)|

= 0.0005"

Operating, Hot & Corroded, Seismic, Above Support Point


= 80*17.765 / (2*15,700*1.20*1.00 + 0.40*|80|)

= 0.0377"


= 68,200 / (*17.88252*15,700*1.20*1.00)

= 0.0036"

tw = W / (2**Rm*St*Ks*Ec) (Weight)= 2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0012"


= 0.0377 + 0.0036 - (0.0012)

= 0.0401"


= 1.20*2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0014"


= |0.0036 + (0.0014) - (0.0377)|

= 0.0327"



= 2*15,700*1.20*1.00*(0.235 - 0.0036 + (0.0012)) / (17.765 - 0.40*(0.235 - 0.0036 + (0.0012)))

= 495.88 psi

33/240


35/241

Operating, Hot & New, Seismic, Above Support Point


= 80*17.765 / (2*15,700*1.20*1.00 + 0.40*|80|)

= 0.0377"


= 68,200 / (*17.88252*15,700*1.20*1.00)

= 0.0036"


= 2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0012"


= 0.0377 + 0.0036 - (0.0012)

= 0.0401"


= 1.20*2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0014"


= |0.0036 + (0.0014) - (0.0377)|

= 0.0327"



= 2*15,700*1.20*1.00*(0.235 - 0.0036 + (0.0012)) / (17.765 - 0.40*(0.235 - 0.0036 + (0.0012)))

= 495.88 psi

Hot Shut Down, Corroded, Seismic, Above Support Point

tp = 0" (Pressure)


= 68,200 / (*17.88252*15,700*1.20*1.00)

= 0.0036"


= 2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0012"


= 0 + 0.0036 - (0.0012)

= 0.0024"


= 68,200 / (*17.88252*14,151.54*1.20)

= 0.004"


= 1.20*2,483.2 / (2**17.8825*14,151.54*1.20)

= 0.0016"

34/240


36/241


= 0.004+ (0.0016) - (0)

= 0.0056"

Hot Shut Down, New, Seismic, Above Support Point

tp = 0" (Pressure)


= 68,200 / (*17.88252*15,700*1.20*1.00)

= 0.0036"


= 2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0012"


= 0 + 0.0036 - (0.0012)

= 0.0024"


= 68,200 / (*17.88252

*14,151.54*1.20)= 0.004"


= 1.20*2,483.2 / (2**17.8825*14,151.54*1.20)

= 0.0016"


= 0.004+ (0.0016) - (0)

= 0.0056"

Empty, Corroded, Seismic, Above Support Point

tp = 0" (Pressure)


= 66,237 / (*17.88252*15,700*1.20*1.00)

= 0.0035"


= 2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0012"


= 0 + 0.0035 - (0.0012)

= 0.0023"tmc = M / (*Rm

2*Sc*Ks) (bending)

= 66,237 / (*17.88252*14,151.54*1.20)

= 0.0039"


= 1.20*2,483.2 / (2**17.8825*14,151.54*1.20)

= 0.0016"


35/240


37/241

= 0.0039 + (0.0016) - (0)

= 0.0054"

Empty, New, Seismic, Above Support Point

tp = 0" (Pressure)


= 66,237 / (*17.88252*15,700*1.20*1.00)

= 0.0035"


= 2,483.2 / (2**17.8825*15,700*1.20*1.00)

= 0.0012"


= 0 + 0.0035 - (0.0012)

= 0.0023"


= 66,237 / (*17.88252*14,151.54*1.20)

= 0.0039"twc = (1 + VAccel)*W / (2**Rm*Sc*Ks) (Weight)

= 1.20*2,483.2 / (2**17.8825*14,151.54*1.20)

= 0.0016"


= 0.0039 + (0.0016) - (0)

= 0.0054"

Operating, Hot & Corroded, Seismic, Below Support Point


= 80*17.765 / (2*15,700*1.20*1.00 + 0.40*|80|)

= 0.0377"


= 1,099 / (*17.88252*15,700*1.20*1.00)

= 0.0001"

tw = (1 + VAccel)*W / (2**Rm*St*Ks*Ec) (Weight)

= 1.20*-933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0005"


= 0.0377 + 0.0001 - (-0.0005)= 0.0383"


= -933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0004"


= |0.0001 + (-0.0004) - (0.0377)|

= 0.0381"

36/240


38/241



= 2*15,700*1.20*1.00*(0.235 - 0.0001 + (-0.0005)) / (17.765 - 0.40*(0.235 - 0.0001 + (-0.0005)))

= 499.83 psi

Operating, Hot & New, Seismic, Below Support Point


= 0.0377"


= 1,099 / (*17.88252*15,700*1.20*1.00)

= 0.0001"


= 1.20*-933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0005"


= 0.0377 + 0.0001 - (-0.0005)

= 0.0383"


= -933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0004"


= |0.0001 + (-0.0004) - (0.0377)|

= 0.0381"



= 2*15,700*1.20*1.00*(0.235 - 0.0001 + (-0.0005)) / (17.765 - 0.40*(0.235 - 0.0001 + (-0.0005)))

= 499.83 psi

Hot Shut Down, Corroded, Seismic, Below Support Point

tp = 0" (Pressure)


= 1,099 / (*17.88252*15,700*1.20*1.00)

= 0.0001"


= 1.20*-933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0005"


= 0 + 0.0001 - (-0.0005)

= 0.0006"


37/240


39/241

= -933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0004"


= |0.0001 + (-0.0004) - (0)|

= 0.0004"

Hot Shut Down, New, Seismic, Below Support Point

tp = 0" (Pressure)


= 1,099 / (*17.88252*15,700*1.20*1.00)

= 0.0001"


= 1.20*-933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0005"


= 0 + 0.0001 - (-0.0005)

= 0.0006"twc = W / (2**Rm*St*Ks*Ec) (Weight)

= -933.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0004"


= |0.0001 + (-0.0004) - (0)|

= 0.0004"

Empty, Corroded, Seismic, Below Support Point

tp = 0" (Pressure)


= 852 / (*17.88252*15,700*1.20*1.00)

= 0"


= 1.20*-684.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0004"


= 0 + 0 - (-0.0004)

= 0.0004"

twc = W / (2**Rm*St*Ks*Ec) (Weight)= -684.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0003"


= |0 + (-0.0003) - (0)|

= 0.0003"

38/240


40/241

Empty, New, Seismic, Below Support Point

tp = 0" (Pressure)


= 852 / (*17.88252*15,700*1.20*1.00)

= 0"


= 1.20*-684.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0004"


= 0 + 0 - (-0.0004)

= 0.0004"


= -684.4 / (2**17.8825*15,700*1.20*1.00)

= -0.0003"


= |0 + (-0.0003) - (0)|

= 0.0003"

39/240


41/241

F&D Head #1

ASME Section VIII, Division 1, 2010 Edition

Component: F&D Head

Material Specification: SA-285 C (II-D p.6, ln. 42)Straight Flangegoverns MDMT


Static liquid head:

Ps= 0 psi (SG=1, Hs=0" Operating head)

Ptv= 0.758 psi (SG=1, Hs=21" Vertical test head)

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

Design MDMT = -20F No impact test performed

Rated MDMT = -55F Material is not normalizedMaterial is not produced to fine grain practice


Do not Optimize MDMT / Find MAWP

Radiography: Category A joints - Seamless No RT

Head to shell seam - Spot UW-11(b) Type 1

Estimated weight*: new = 72.1 lb corr = 72.1 lb

Capacity*: new = 29.9 US gal corr = 29.9 US gal* includes straight flange

Outer diameter = 36"

Crown radius L = 28.8"Knuckle radius r = 3.6"Minimum head thickness = 0.235"

Straight flange length Lsf = 2"Nominal straight flange thickness tsf = 0.25"

Results Summary

The governing condition is internal pressure.Minimum thickness per UG-16 = 0.0625" + 0"= 0.0625"

Design thickness due to internal pressure (t) = 0.1264"Maximum allowable working pressure (MAWP) = 149.3psi

Maximum allowable pressure (MAP) = 149.3psi

M (Corroded)

M=1/4*[3 + (L / r)1/2]=1/4*[3 + (28.8 / 3.6)1/2]=1.457107

M (New)

M=1/4*[3 + (L / r)1/2]=1/4*[3 + (28.8 / 3.6)1/2]=1.457107

40/240


42/241

Design thickness for internal pressure, (Corroded at 100 F) Appendix 1-4(d)

t = P*Lo*M / (2*S*E + P*(M - 0.2)) + Corrosion= 80*29.035*1.4571 / (2*15,700*0.85 + 80*(1.4571 - 0.2)) + 0= 0.1263"

The head internal pressure design thickness is 0.1264".

Maximum allowable working pressure, (Corroded at 100 F) Appendix 1-4(d)

P = 2*S*E*t / (M*Lo- t*(M - 0.2)) - Ps= 2*15,700*0.85*0.235 / (1.4571*29.035 - 0.235*(1.4571 - 0.2))- 0

= 149.3 psi

The maximum allowable working pressure (MAWP) is 149.3psi.

Maximum allowable pressure, (New at 70 F) Appendix 1-4(d)

P = 2*S*E*t / (M*Lo- t*(M - 0.2)) - Ps= 2*15,700*0.85*0.235 / (1.4571*29.035 - 0.235*(1.4571 - 0.2)) - 0= 149.3 psi

The maximum allowable pressure (MAP) is 149.3psi.


EFE = (75*t / Rf)*(1 - Rf/ Ro)

= (75*0.25 / 3.725)*(1 - 3.725 / )

= 5.0336%

The extreme fiber elongation exceeds 5 percent. Heat treatment per UCS-56 may be required. See UCS-79(d)(4) or(5).

41/240


43/241

Straight Flange on F&D Head #1


Component: Straight Flange





Static liquid head:

Ps = 0 psi (SG = 1, Hs=

0",Operating head)

Ptv = 0.83 psi (SG = 1, Hs= 23",Vertical test head)


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

Material is not produced to Fine Grain Practice


Radiography: Longitudinal joint - Seamless No RT

Circumferential joint - Spot UW-11(b) Type 1



OD = 36"

LengthLc

= 2"

t = 0.25"


t = P*Ro/ (S*E + 0.40*P) + Corrosion

= 80*18 / (15,700*0.85 + 0.40*80) + 0= 0.1077"


P = S*E*t / (Ro- 0.40*t) - Ps= 15,700*0.85*0.25 / (18 - 0.40*0.25) - 0= 186.38 psi


P = S*E*t / (Ro- 0.40*t)

= 15,700*0.85*0.25 / (18 - 0.40*0.25)= 186.38 psi

42/240


44/241


EFE = (50*t / Rf)*(1 - Rf/ Ro)

= (50*0.25 / 17.875)*(1 - 17.875 /)

= 0.6993%







psi)



Temperature (F)

Corrosion C(in)


Tension (in)

Req'd Thk Dueto

Compression(in)

St Sc


Seismic 0.044 0.0435


Seismic 0.044 0.0435


Seismic 0.0003 0.0007


Seismic 0.0003 0.0007


Seismic 0.0003 0.0007

Empty, New 0 15,700 14,404 70 0Wind 0.0003 0.0005

Seismic 0.0003 0.0007




A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.25)

= 0.001736

B = 14,404 psi

S = 15,700 / 1.00 = 15,700 psi



= 14,404 psi

43/240


45/241


A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.25)

= 0.001736

B = 14,404 psi

S = 15,700 / 1.00 = 15,700 psi



= 14,404 psi


A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.25)

= 0.001736

B = 14,404 psi

S = 15,700 / 1.00 = 15,700 psi


Operating, Hot & Corroded, Wind, Bottom Seam


= 80*17.75 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"


= 176 / (*17.8752*15,700*1.20*0.85)

= 0"


= 0.60*894.7 / (2**17.875*15,700*1.20*0.85)

= 0.0003"


tensile)

= 0.0443 + 0 - (0.0003)

= 0.044"


= 894.7 / (2**17.875*15,700*1.20*0.85)

= 0.0005"

tc = |tmc+ twc- tpc|(total, net

tensile)

= |0 + (0.0005) - (0.0443)|

= 0.0438"

44/240


46/241



= 2*15,700*1.20*0.85*(0.25 - 0 + (0.0003)) / (17.75 - 0.40*(0.25 - 0 + (0.0003)))

= 454.18 psi

Operating, Hot & New, Wind, Bottom Seam


= 0.0443"


= 176 / (*17.8752*15,700*1.20*0.85)

= 0"


= 0.60*894.7 / (2**17.875*15,700*1.20*0.85)

= 0.0003"

tt = tp+ tm- tw

(total required,

tensile)= 0.0443 + 0 - (0.0003)

= 0.044"


= 894.7 / (2**17.875*15,700*1.20*0.85)

= 0.0005"

tc = |tmc+ twc- tpc|(total, nettensile)

= |0 + (0.0005) - (0.0443)|

= 0.0438"



= 2*15,700*1.20*0.85*(0.25 - 0 + (0.0003)) / (17.75 - 0.40*(0.25 - 0 + (0.0003)))

= 454.18 psi

Hot Shut Down, Corroded, Wind, Bottom Seam

tp = 0" (Pressure)


= 176 / (*17.8752

*14,404.47*1.20)= 0"


= 0.60*894.7 / (2**17.875*14,404.47*1.20)

= 0.0003"


= |0 + 0 - (0.0003)|

= 0.0003"

45/240


47/241


= 894.7 / (2**17.875*14,404.47*1.20)

= 0.0005"


= 0 + (0.0005) - (0)

= 0.0005"

Hot Shut Down, New, Wind, Bottom Seam

tp = 0" (Pressure)


= 176 / (*17.8752*14,404.47*1.20)

= 0"


= 0.60*894.7 / (2**17.875*14,404.47*1.20)

= 0.0003"


= |0 + 0 - (0.0003)|= 0.0003"


= 894.7 / (2**17.875*14,404.47*1.20)

= 0.0005"


= 0 + (0.0005) - (0)

= 0.0005"

Empty, Corroded, Wind, Bottom Seam

tp = 0" (Pressure)


= 176 / (*17.8752*14,404.47*1.20)

= 0"


= 0.60*894.7 / (2**17.875*14,404.47*1.20)

= 0.0003"


= |0 + 0 - (0.0003)|

= 0.0003"twc = W / (2**Rm*Sc*Ks) (Weight)

= 894.7 / (2**17.875*14,404.47*1.20)

= 0.0005"


= 0 + (0.0005) - (0)

= 0.0005"

46/240


48/241

Empty, New, Wind, Bottom Seam

tp = 0" (Pressure)


= 176 / (*17.8752*14,404.47*1.20)

= 0"


= 0.60*894.7 / (2**17.875*14,404.47*1.20)

= 0.0003"


= |0 + 0 - (0.0003)|

= 0.0003"


= 894.7 / (2**17.875*14,404.47*1.20)

= 0.0005"


= 0 + (0.0005) - (0)

= 0.0005"

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

tp = 0" (Pressure)


= 88 / (*17.8752*14,404.47*1.00)

= 0"


= 894.7 / (2**17.875*14,404.47*1.00)

= 0.0006"


= |0 + 0 - (0.0006)|

= 0.0005"


= 0 + (0.0006) - (0)

= 0.0006"

Operating, Hot & Corroded, Seismic, Bottom Seam


= 80*17.75 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"


= 2,857 / (*17.8752*15,700*1.20*0.85)

= 0.0002"


= 894.7 / (2**17.875*15,700*1.20*0.85)

47/240


49/241


50/241

Hot Shut Down, Corroded, Seismic, Bottom Seam

tp = 0" (Pressure)


= 2,857 / (*17.8752*14,404.47*1.20)

= 0.0002"


= 894.7 / (2**17.875*14,404.47*1.20)

= 0.0005"


= |0 + 0.0002 - (0.0005)|

= 0.0003"


= 1.20*894.7 / (2**17.875*14,404.47*1.20)

= 0.0006"


= 0.0002 + (0.0006) - (0)

= 0.0007"

Hot Shut Down, New, Seismic, Bottom Seam

tp = 0" (Pressure)


= 2,857 / (*17.8752*14,404.47*1.20)

= 0.0002"


= 894.7 / (2**17.875*14,404.47*1.20)

= 0.0005"


= |0 + 0.0002 - (0.0005)|

= 0.0003"


= 1.20*894.7 / (2**17.875*14,404.47*1.20)

= 0.0006"


= 0.0002 + (0.0006) - (0)

= 0.0007"

Empty, Corroded, Seismic, Bottom Seam

tp = 0" (Pressure)


= 2,759 / (*17.8752*14,404.47*1.20)

= 0.0002"


49/240


51/241

= 894.7 / (2**17.875*14,404.47*1.20)

= 0.0005"


= |0 + 0.0002 - (0.0005)|

= 0.0003"


= 1.20*894.7 / (2**17.875*14,404.47*1.20)

= 0.0006"


= 0.0002 + (0.0006) - (0)

= 0.0007"

Empty, New, Seismic, Bottom Seam

tp = 0" (Pressure)


= 2,759 / (*17.8752*14,404.47*1.20)

= 0.0002"tw = W / (2**Rm*Sc*Ks) (Weight)

= 894.7 / (2**17.875*14,404.47*1.20)

= 0.0005"


= |0 + 0.0002 - (0.0005)|

= 0.0003"


= 1.20*894.7 / (2**17.875*14,404.47*1.20)

= 0.0006"


= 0.0002 + (0.0006) - (0)

= 0.0007"

50/240


52/241

Straight Flange on F&D Head #2


Component: Straight Flange





Static liquid head:

Ps = 0.07 psi (SG = 1, Hs= 2",Operating head)

Ptv = 5.21 psi (SG = 1, Hs= 144.375", Vertical testhead)


Design MDMT = -20 F No impact test performed

Rated MDMT = -55 F Material is not normalizedMaterial is not produced to Fine Grain PracticePWHT is not performed

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



OD = 36"Length

Lc= 2"

t = 0.25"


t = P*Ro/ (S*E + 0.40*P) + Corrosion= 80.07*18 / (15,700*0.85 + 0.40*80.07) + 0

= 0.1078"


P = S*E*t / (Ro- 0.40*t) - Ps= 15,700*0.85*0.25 / (18 - 0.40*0.25) - 0.07

= 186.31 psi


P = S*E*t / (Ro- 0.40*t)= 15,700*0.85*0.25 / (18 - 0.40*0.25)

= 186.38 psi

51/240


53/241


EFE = (50*t / Rf)*(1 - Rf/ Ro)

= (50*0.25 / 17.875)*(1 - 17.875 /)

= 0.6993%







psi)



Temperature (F)

Corrosion C(in)


Tension (in)

Req'd Thk Dueto

Compression(in)

St Sc


Seismic 0.0448 0.0446


Seismic 0.0448 0.0446


Seismic 0.0005 0.0003


Seismic 0.0005 0.0003


Seismic 0.0005 0.0003

Empty, New 0 15,700 14,404 70 0Wind 0.0004 0.0002

Seismic 0.0005 0.0003




A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.25)

= 0.001736

B = 14,404 psi

S = 15,700 / 1.00 = 15,700 psi



= 14,404 psi

52/240


54/241


A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.25)

= 0.001736

B = 14,404 psi

S = 15,700 / 1.00 = 15,700 psi



= 14,404 psi


A = 0.125 / (Ro/ t)

= 0.125 / (18 / 0.25)

= 0.001736

B = 14,404 psi

S = 15,700 / 1.00 = 15,700 psi


Operating, Hot & Corroded, Wind, Top Seam


= 80*17.75 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"


= 72 / (*17.8752*15,700*1.20*0.85)

= 0"


= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= 0.0443 + 0 - (-0.0004)

= 0.0447"


= 0.60*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0002"


= |0 + (-0.0002) - (0.0443)|

= 0.0445"



= 2*15,700*1.20*0.85*(0.25 - 0 + (-0.0004)) / (17.75 - 0.40*(0.25 - 0 + (-0.0004)))

53/240


55/241

= 452.96 psi

Operating, Hot & New, Wind, Top Seam


= 80*17.75 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"


= 72 / (*17.8752*15,700*1.20*0.85)

= 0"


= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= 0.0443 + 0 - (-0.0004)

= 0.0447"


= 0.60*-676.9 / (2**17.875*15,700*1.20*0.85)= -0.0002"


= |0 + (-0.0002) - (0.0443)|

= 0.0445"



= 2*15,700*1.20*0.85*(0.25 - 0 + (-0.0004)) / (17.75 - 0.40*(0.25 - 0 + (-0.0004)))

= 452.96 psi

Hot Shut Down, Corroded, Wind, Top Seam

tp = 0" (Pressure)


= 72 / (*17.8752*15,700*1.20*0.85)

= 0"


= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"

tt = tp+ tm- tw (total required, tensile)= 0 + 0 - (-0.0004)

= 0.0004"


= 0.60*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0002"


= |0 + (-0.0002) - (0)|

54/240


56/241

= 0.0002"

Hot Shut Down, New, Wind, Top Seam

tp = 0" (Pressure)


= 72 / (*17.8752*15,700*1.20*0.85)

= 0"


= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= 0 + 0 - (-0.0004)

= 0.0004"


= 0.60*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0002"

tc = |tmc+ twc- tpc| (total, net tensile)= |0 + (-0.0002) - (0)|

= 0.0002"

Empty, Corroded, Wind, Top Seam

tp = 0" (Pressure)


= 72 / (*17.8752*15,700*1.20*0.85)

= 0"


= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= 0 + 0 - (-0.0004)

= 0.0004"


= 0.60*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0002"


= |0 + (-0.0002) - (0)|= 0.0002"

Empty, New, Wind, Top Seam

tp = 0" (Pressure)


= 72 / (*17.8752*15,700*1.20*0.85)

= 0"

55/240


57/241


= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= 0 + 0 - (-0.0004)

= 0.0004"


= 0.60*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0002"


= |0 + (-0.0002) - (0)|

= 0.0002"

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

tp = 0" (Pressure)


= 72 / (*17.8752

*15,700*1.00*0.85)= 0"


= -676.9 / (2**17.875*15,700*1.00*0.85)

= -0.0005"


tensile)

= 0 + 0 - (-0.0005)

= 0.0005"

tc

= |tmc

+ twc

- tpc

|(total, net

tensile)= |0+ (-0.0005) - (0)|

= 0.0004"

Operating, Hot & Corroded, Seismic, Top Seam


= 80*17.75 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"


= 987 / (*17.8752*15,700*1.20*0.85)

= 0.0001"


= 1.20*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0005"


= 0.0443 + 0.0001 - (-0.0005)

= 0.0448"

56/240


58/241


= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= |0.0001 + (-0.0004) - (0.0443)|

= 0.0446"



= 2*15,700*1.20*0.85*(0.25 - 0.0001 + (-0.0005)) / (17.75 - 0.40*(0.25 - 0.0001 + (-0.0005)))

= 452.72 psi

Operating, Hot & New, Seismic, Top Seam


= 80*17.75 / (2*15,700*1.20*0.85 + 0.40*|80|)

= 0.0443"

tm = M / (*Rm2*St*Ks*Ec) (bending)= 987 / (*17.8752*15,700*1.20*0.85)

= 0.0001"


= 1.20*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0005"


= 0.0443 + 0.0001 - (-0.0005)

= 0.0448"

twc

= W / (2**Rm

*St

*Ks

*Ec

) (Weight)

= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= |0.0001 + (-0.0004) - (0.0443)|

= 0.0446"



= 2*15,700*1.20*0.85*(0.25 - 0.0001 + (-0.0005)) / (17.75 -0.40*(0.25 - 0.0001 + (-0.0005)))

= 452.72 psi

Hot Shut Down, Corroded, Seismic, Top Seam

tp = 0" (Pressure)


= 987 / (*17.8752*15,700*1.20*0.85)

= 0.0001"

57/240


59/241


= 1.20*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0005"


= 0 + 0.0001 - (-0.0005)

= 0.0005"


= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= |0.0001 + (-0.0004) - (0)|

= 0.0003"

Hot Shut Down, New, Seismic, Top Seam

tp = 0" (Pressure)


= 987 / (*17.875

2

*15,700*1.20*0.85)= 0.0001"


= 1.20*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0005"


= 0 + 0.0001 - (-0.0005)

= 0.0005"


= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= |0.0001 + (-0.0004) - (0)|

= 0.0003"

Empty, Corroded, Seismic, Top Seam

tp = 0" (Pressure)


= 777 / (*17.8752*15,700*1.20*0.85)

= 0"


= 1.20*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0005"


= 0 + 0 - (-0.0005)

= 0.0005"


58/240


60/241

= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= |0 + (-0.0004) - (0)|

= 0.0003"

Empty, New, Seismic, Top Seam

tp = 0" (Pressure)


= 777 / (*17.8752*15,700*1.20*0.85)

= 0"


= 1.20*-676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0005"


= 0 + 0 - (-0.0005)

= 0.0005"twc = W / (2**Rm*St*Ks*Ec) (Weight)

= -676.9 / (2**17.875*15,700*1.20*0.85)

= -0.0004"


= |0 + (-0.0004) - (0)|

= 0.0003"

59/240


61/241

F&D Head #2

ASME Section VIII, Division 1, 2010 Edition

Component: F&D Head

Material Specification: SA-285 C (II-D p.6, ln. 42)Straight Flangegoverns MDMT


Static liquid head:

Ps= 0.3595 psi (SG=1, Hs=9.9579" Operating head)

Ptv= 5.4988 psi (SG=1, Hs=152.3329" Vertical test head)

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

Design MDMT = -20F No impact test performed

Rated MDMT = -55F Material is not normalizedMaterial is not produced to fine grain practice


Do not Optimize MDMT / Find MAWP

Radiography: Category A joints - Seamless No RT

Head to shell seam - Spot UW-11(b) Type 1

Estimated weight*: new = 81.3 lb corr = 81.3 lb

Capacity*: new = 29.9 US gal corr = 29.9 US gal* includes straight flange

Outer diameter = 36"

Crown radius L = 28.8"Knuckle radius r = 3.6"Minimum head thickness = 0.235"

Straight flange length Lsf = 2"Nominal straight flange thickness tsf = 0.25"

Results Summary

The governing condition is internal pressure.Minimum thickness per UG-16 = 0.0625" + 0"= 0.0625"

Design thickness due to internal pressure (t) = 0.1269"Maximum allowable working pressure (MAWP) = 148.94psi

Maximum allowable pressure (MAP) = 149.3psi

M (Corroded)

M=1/4*[3 + (L / r)1/2]=1/4*[3 + (28.8 / 3.6)1/2]=1.457107

M (New)

M=1/4*[3 + (L / r)1/2]=1/4*[3 + (28.8 / 3.6)1/2]=1.457107

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Design thickness for internal pressure, (Corroded at 100 F) Appendix 1-4(d)

t = P*Lo*M / (2*S*E + P*(M - 0.2)) + Corrosion= 80.36*29.035*1.4571 / (2*15,700*0.85 + 80.36*(1.4571- 0.2)) + 0= 0.1269"

The head internal pressure design thickness is 0.1269".

Maximum allowable working pressure, (Corroded at 100 F) Appendix 1-4(d)

P = 2*S*E*t / (M*Lo- t*(M - 0.2)) - Ps= 2*15,700*0.85*0.235 / (1.4571*29.035 - 0.235*(1.4571 - 0.2)) - 0.36

= 148.94 psi

The maximum allowable working pressure (MAWP) is 148.94psi.

Maximum allowable pressure, (New at 70 F) Appendix 1-4(d)

P = 2*S*E*t / (M*Lo- t*(M - 0.2)) - Ps= 2*15,700*0.85*0.235 / (1.4571*29.035 - 0.235*(1.4571 - 0.2)) - 0= 149.3 psi

The maximum allowable pressure (MAP) is 149.3psi.


EFE = (75*t / Rf)*(1 - Rf/ Ro)

= (75*0.25 / 3.725)*(1 - 3.725 / )

= 5.0336%

The extreme fiber elongation exceeds 5 percent. Heat treatment per UCS-56 may be required. See UCS-79(d)(4) or(5).

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ACIDO (B3)


tw(lower)= 0.375 in

Leg41= 0.1875 in

Leg43= 0 in

hnew= 1 in

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

Located on: Cylinder #2

Liquid static head included: 0 psi

Nozzle material specification: SA-106 B Smls pipe (II-D p. 10, ln. 40)

Nozzle longitudinal joint efficiency: 1

Nozzle description: NPS 2 Sch 40 (Std)

Flange description: 2 inch Class 150 WN A105

Bolt Material: SA-193 B7 Bolt


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Reinforcement Calculations for Internal Pressure

The attached ASME B16.5 flange limits the nozzle MAWP.

UG-37 Area Calculation Summary(in2)

For P = 285 psi @ 100 F

UG-45 NozzleWall

ThicknessSummary (in)The nozzle passes

UG-45

Arequired

Aavailable

A1 A2 A3 A5A

weldstreq tmin

This nozzle is exempt from areacalculations per UG-36(c)(3)(a)

0.1348 0.1348

UG-41 Weld Failure Path Analysis Summary

The nozzle is exempt from weld strength calculations

per UW-15(b)(2)

UW-16 Weld Sizing Summary

Weld descriptionRequired weldthroat size (in)

Actual weldthroat size (in)

Status

Nozzle to shell fillet (Leg41) 0.1078 0.1312 weld size is adequate

Calculations for internal pressure 285 psi @ 100 F

Fig UCS-66.2 general note (1) applies.

Nozzle is impact test exempt per UCS-66(d) (NPS 4 or smaller pipe).

Nozzle UCS-66 governing thk: 0.1348 in

Nozzle rated MDMT: -155 F

Parallel Limit of reinforcement per UG-40

LR = MAX(d, Rn+ (tn- Cn) + (t - C))

= MAX(2.067, 1.0335 + (0.154 - 0) + (0.375 - 0))

= 2.067 in

Outer Normal Limit of reinforcement per UG-40

LH = MIN(2.5*(t - C), 2.5*(tn- Cn) + te)

= MIN(2.5*(0.375 - 0), 2.5*(0.154 - 0) + 0)

= 0.385 in

Inner Normal Limit of reinforcement per UG-40

LI = MIN(2.5*(t - C), 2.5*(ti- Cn- C))

= MIN(2.5*(0.375 - 0), 2.5*(0.154 - 0 - 0))

= 0.385 in

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

trn = P*Rn/ (Sn*E - 0.6*P)

= 285*1.0335 / (17,100*1 - 0.6*285)

= 0.0174 in

Required thickness trfrom UG-37(a)

tr = P*Ro/ (S*E + 0.4*P)

= 285*18 / (15,700*1 + 0.4*285)

= 0.3244 in

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

UW-16(c) Weld Check

Fillet weld: tmin= lesser of 0.75 or tnor t = 0.154 in

tc(min)= lesser of 0.25 or 0.7*tmin= 0.1078in

tc(actual)= 0.7*Leg = 0.7*0.1875 = 0.1313 in

The fillet weld size is satisfactory.

Weld strength calculations are not required for this detail whic

Memoria de Calculo Recipiente a Presion

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