Cl-r Mec-mc-ot-791-01 Rev. 0 Modificado

8/12/2019 Cl-r Mec-mc-ot-791-01 Rev. 0 Modificado

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CONSTRUCTORA HOSTOTIPAQUILLO

CARRETERA TULA - BOJAY, S/N, KM.0+300PARQUE INDUSTRIAL ATITALAQUIA.

ATITALAQUIA, HGO . MXICO

COMPRESS Pressure Vessel Design Calculations

EQUIPO: SEGUNDO ENFRIADOR DE FONDOS DEL AGOTADORTAG: MT-1-EA-3005-A

CLIENTE : PEMEXZ REFINACIN, AGUAS AMARGAS CD. MADERO

CONTRATO:

DISEADOR : RICARDO BARCENAS

FECHA: 29 OCT. 2013

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


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Table of ContentsGeneral Arrangement Drawing..............................................................................................................................1/229

Deficiencies Summary............................................................................................................................................2/229

Nozzle Schedule......................................................................................................................................................3/229

Nozzle Summary.....................................................................................................................................................4/229

Pressure Summary.................................................................................................................................................5/229

Revision History......................................................................................................................................................9/229

Settings Summary.................................................................................................................................................10/229

Radiography Summary.........................................................................................................................................12/229

Thickness Summary.............................................................................................................................................14/229

Weight Summary...................................................................................................................................................15/229

Long Seam Summary...........................................................................................................................................17/229

Test Report............................................................................................................................................................19/229

Vacuum Summary.................................................................................................................................................21/229

ENVOLVENTE CANAL..........................................................................................................................................22/229

ENVOLVENTE 1.....................................................................................................................................................24/229

ENVOLVENTE 2.....................................................................................................................................................27/229

Rear Shell Cylinder...............................................................................................................................................30/229

TAPA BRIDADA CANAL.......................................................................................................................................33/229

Straight Flange on Rear Shell Head....................................................................................................................34/229

Rear Shell Head.....................................................................................................................................................37/229

BRIDA BIPARTIDA................................................................................................................................................39/229

BRIDA BONET -- CUERPO....................................................................................................................................44/229

BRIDA CANAL --ESPEJO......................................................................................................................................51/229

BRIDA CUERPO -- BONETE.................................................................................................................................58/229

BRIDA CUERPO ESPEJO FIJO............................................................................................................................65/229

BRIDA TAPA DEL CANAL....................................................................................................................................72/229

IP1 INSTRUMENTO DE PRESION (IP1)................................................................................................................79/229


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Tableof ContentsIP2 INSTRUMENTO DE PRESION (IP2)................................................................................................................84/229



IT1 INDICADOR DE TEMPERATURA (IT1)...........................................................................................................99/229

IT2 INSTRUMENTO DE TEMPERATUIRA (IT2)..................................................................................................104/229

IT3 INSTRUMENTO DE TEMPERATUIRA (IT3)..................................................................................................109/229

IT4 INSTRUMENTO DE TEMPERATURA (IT4)...................................................................................................114/229

N1 ENTRADA DEL FONDO DEL AGOTADOR (N1)...........................................................................................119/229

N2 INTERCONEXION DE ENVOLVENTE (N2)...................................................................................................127/229

N5 INTERCONEXION DE CANALES (N5)..........................................................................................................135/229

N6 SALIDA DE AGUA DE ENFRIAMIENTO (N6)...............................................................................................143/229

N7A CONEXION PARA LIMPIEZA QUIMICA (N7A)...........................................................................................151/229

N7B CONEXION PARA LIMPIEZA QUIMICA (N7B)...........................................................................................157/229

SILLETA...............................................................................................................................................................163/229

Baffle Summary Report......................................................................................................................................169/229

Data Inputs Summary.........................................................................................................................................170/229

Design Conditions Summary.............................................................................................................................171/229

Front Stationary Tubesheet -- ASME.................................................................................................................172/229

Materials and Gaskets Summary.......................................................................................................................196/229

TEMA RCB-9.132 Pass Partition Plate Calculations........................................................................................198/229

Rear Floating Tubesheet -- ASME......................................................................................................................199/229

Shell side liquid level..........................................................................................................................................214/229

TAPA FLOTANTE................................................................................................................................................215/229

Tube side liquid level..........................................................................................................................................224/229

Tubes....................................................................................................................................................................225/229

Tubesheet Maximum Pressure Report..............................................................................................................227/229

Front Stationary Tubesheet -- TEMA.................................................................................................................228/229

i


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General Arrangement Drawing

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Deficiencies Summary

No deficiencies found.

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Nozzle Schedule

Nozzlemark

Service Size MaterialsImpactTested

NormalizedFineGrain

Flange Blind

IP1 IP1 INSTRUMENTO DE PRESIONNPS 0.5 Class 6000 DN 15 -threaded

Nozzle SA-105 No No No N/A No







IT1IT1 INDICADOR DETEMPERATURA

NPS 0.5 Class 6000 DN 15 -threaded


IT2IT2 INSTRUMENTO DETEMPERATUIRA



IT3IT3 INSTRUMENTO DETEMPERATUIRA



IT4IT4 INSTRUMENTO DETEMPERATURA



N1N1 ENTRADA DEL FONDO DELAGOTADOR

NPS 6 Sch 80 (XS) DN 150 NozzleSA-106 B Smls.Pipe

No No NoNPS 6 Class150WN A105

No

N2N2 INTERCONEXION DEENVOLVENTE



No

N5 N5 INTERCONEXION DE CANALES NPS 6 Sch 80 (XS) DN 150 NozzleSA-106 B Smls.Pipe


No

N6N6 SALIDA DE AGUA DEENFRIAMIENTO



No

N7AN7A CONEXION PARA LIMPIEZAQUIMICA

NPS 2 Sch 160 DN 50 NozzleSA-106 B Smls.Pipe


No

N7BN7B CONEXION PARA LIMPIEZAQUIMICA

NPS 2 Sch 160 DN 50 NozzleSA-106 B Smls.Pipe


No

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Nozzle Summary

Nozzlemark

OD(mm)

tn

(mm)Req t

n(mm)

A1? A2?

ShellReinforcement

Pad Corr(mm)

Aa/A

r(%)

Nom t(mm)

Design t(mm)

User t(mm)

Width(mm)

tpad

(mm)

IP1 38.1 8.38 4.7 Yes Yes 10.97 N/A N/A N/A 3.2 Exempt




IT1 38.1 8.38 4.7 Yes Yes 10.97 N/A N/A N/A 3.2 Exempt




N1 168.27 10.97 8.33 Yes Yes 9.5 7.29 N/A N/A 3.2 100.0

N2 168.27 10.97 8.33 Yes Yes 9.5 7.29 N/A N/A 3.2 100.0

N5 168.27 10.97 8.32 Yes Yes 9.5 7.28 N/A N/A 3.17 100.0

N6 168.27 10.97 8.32 Yes Yes 9.5 7.28 N/A N/A 3.17 100.0

N7A 60.33 8.74 5.34 Yes Yes 10.97 N/A N/A N/A 3.17 Exempt

N7B 60.33 8.74 5.34 Yes Yes 10.97 N/A N/A N/A 3.17 Exempt

tn: Nozzle thickness

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

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Pressure Summary

Pressure Summary for Tube side chamber

IdentifierP

Design( kg/cm2)

T

Design( C)

MAWP( kg/cm2)

MAP( kg/cm2)

MAEP( kg/cm2)

Te

external( C)

MDMT( C)

MDMTExemption

ImpactTested

TAPA BRIDADA CANAL 7 66 8.3 8.36 N/A 66 -48 Note 1 No

ENVOLVENTE CANAL 7 66 27.39 41.36 N/A 66 -105 Note 2 No

Front Stationary Tubesheet(seeMaximum PressureRating note)

7 90 16.16 17.97 11.51 90 -48 Note 3 No

Rear Floating Tubesheet(see Maximum PressureRating note)

7 90 16.16 17.97 11.51 90 -48 Note 3 No

TAPA FLOTANTE 7 90 15.38 15.66 17 90 -48 Note 4 No

Tubes 7 90 198.3 198.36 125.47 90 -105 Note 5 No

BRIDA TAPA DEL CANAL 7 66 16.27 23.86 N/A 66 -48 Note 6 No

BRIDA TAPA DEL CANAL - Flange Hub 7 66 27.39 41.36 N/A 66 -105 Note 2 No

BRIDA CANAL --ESPEJO 7 66 16.7 23.86 N/A 66 -48 Note 6 No

BRIDA CANAL --ESPEJO - Flange Hub 7 66 27.39 41.36 N/A 66 -105 Note 2 No

BRIDA BIPARTIDA 7 90 14.51 14.51 70.24 90 -44.58 Note 7 No

IP2 INSTRUMENTO DE PRESION (IP2) 7 66 96.5 146.38 N/A 66 -105 Note 8 No

IP3 INSTRUMENTO DE PRESION (IP3) 7 66 96.43 146.38 N/A 66 -105 Note 9 No

IT2 INSTRUMENTO DE TEMPERATUIRA (IT2) 7 66 96.5 146.38 N/A 66 -105 Note 8 No

IT3 INSTRUMENTO DE TEMPERATUIRA (IT3) 7 66 96.43 146.38 N/A 66 -105 Note 9 No

N5 INTERCONEXION DE CANALES (N5) 7 66 17.84 19.99 N/A 66 -48 Note 10 No

N6 SALIDA DE AGUA DE ENFRIAMIENTO (N6) 7 66 17.91 19.99 N/A 66 -48 Note 10 No

N7A CONEXION PARA LIMPIEZA QUIMICA (N7A) 7 66 19.09 19.99 N/A 66 -48 Note 10 No

N7B CONEXION PARA LIMPIEZA QUIMICA (N7B) 7 66 19.02 19.99 N/A 66 -48 Note 10 No

Chamber design MDMT is -17.78 C

Chamber rated MDMT is -44.58 C @ 8.3 kg/cm2

Chamber MAWP hot & corroded is 8.3 kg/cm2@ 66 C

Chamber MAP cold & new is 8.36 kg/cm2@ 21.11 C

This pressure chamber is not designed for external pressure.

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Pressure Summary for Shell side chamber

IdentifierP

Design( kg/cm2)

T

Design( C)

MAWP( kg/cm2)

MAP( kg/cm2)

MAEP( kg/cm2)

Te

external( C)

MDMT( C)

MDMTExemption

ImpactTested

Front Stationary Tubesheet(seeMaximum PressureRating note)

11.5 90 11.51 13.32 16.16 90 -48 Note 3 No

ENVOLVENTE 1 11.5 90 27.26 41.36 N/A 90 -48 Note 11 No

ENVOLVENTE 2 11.5 90 27.26 41.36 N/A 90 -48 Note 11 NoRear Shell Cylinder 11.5 90 24.39 37.01 N/A 90 -48 Note 12 No

Straight Flange on Rear Shell Head 11.5 90 24.39 37.01 N/A 90 -48 Note 12 No

Rear Shell Head 11.5 90 24.9 37.5 N/A 90 -48 Note 13 No

Rear Floating Tubesheet(see Maximum PressureRating note)

11.5 90 11.51 13.32 16.16 90 -48 Note 3 No

TAPA FLOTANTE 11.5 90 17 31.36 15.38 90 N/A Note 14 No

BRIDA BIPARTIDA 11.5 90 70.24 70.24 14.51 90 -44.58 Note 7 No

Tubes 11.5 90 125.47 125.47 198.3 90 N/A N/A No

BRIDA CUERPO ESPEJO FIJO 11.5 90 16.84 24.06 N/A 90 -48 Note 15 No

BRIDA CUERPO ESPEJO FIJO - Flange Hub 11.5 90 27.39 41.36 N/A 90 -48 Note 16 No

BRIDA CUERPO -- BONETE 11.5 90 11.67 14.77 N/A 90 -48 Note 17 No

BRIDA CUERPO -- BONETE - Flange Hub 11.5 90 27.39 41.36 N/A 90 -48 Note 16 No

SILLETA 11.5 90 11.51 N/A N/A N/A N/A N/A N/A

BRIDA BONET -- CUERPO 11.5 90 11.66 14.77 N/A 90 -48 Note 17 No

BRIDA BONET -- CUERPO - Flange Hub 11.5 90 24.51 37.01 N/A 90 -48 Note 18 No

IP1 INSTRUMENTO DE PRESION (IP1) 11.5 90 96.03 146.38 N/A 90 -105 Note 19 No

IP4 INSTRUMENTO DE PRESION (IP4) 11.5 90 95.96 146.38 N/A 90 -105 Note 20 No

IT1 INDICADOR DE TEMPERATURA (IT1) 11.5 90 96.03 146.38 N/A 90 -105 Note 19 No

IT4 INSTRUMENTO DE TEMPERATURA (IT4) 11.5 90 95.96 146.38 N/A 90 -105 Note 20 No

N1 ENTRADA DEL FONDO DEL AGOTADOR (N1) 11.5 90 17.82 19.99 N/A 90 -48 Note 21 No

N2 INTERCONEXION DE ENVOLVENTE (N2) 11.5 90 17.75 19.99 N/A 90 -48 Note 22 No

Chamber design MDMT is -17.78 CChamber rated MDMT is -44.58 C @ 11.51 kg/cm2

Chamber MAWP hot & corroded is 11.51 kg/cm2@ 90 CMAWPis the maximum allowable shell side pressure for the component.

Chamber MAP cold & new is 13.32 kg/cm2@ 21.11 C

This pressure chamber is not designed for external pressure.

Notes for Maximum Pressure Rating:

Note # Details

1.The largest tubesheet MAWP/MAP values have been selected from the multiple design conditions to maximize the hydrotest pressure and to complywith UG-20(b). The MAWP/MAP selected for the shell side may not be coincident with the MAWP/MAP selected for the tube side (and vice versa).

2.The chamber MAWP listed above is based on the largest tubesheet MAWP values from the multiple design conditions. The lowest tubesheet MAWPvalues should be considered when determining the final chamber MAWP. Refer to the Tubesheet Maximum Pressure Reportfor the lowest tubesheetmaximum pressure ratings.

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Notes for MDMT Rating:

Note # Exemption Details

1.Bolted cover impact test exemption temperature from Fig UCS-66M Curve D = -48 C17 C MDMT reduction per UCS-68(c) applies.Rated MDMT of -65C is limited to -48C by UCS-66(b)(2)

UCS-66 governing thickness = 8 mm

2. Material is impact test exempt to -105 C per UCS-66(b)(3) (coincident ratio = 0.302)

3.Tubesheet impact test exemption temperature from Fig UCS-66M Curve D = -48 C17 C MDMT reduction per UCS-68(c) applies.Rated MDMT of -65C is limited to -48C by UCS-66(b)(2)

UCS-66 governing thickness = 9.23 mm

4.

impact test exemption temperature from Fig UCS-66M Curve B = -15.04 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 17.5 C, (coincident ratio = 0.6874)Rated MDMT of -49.54C is limited to -48C by UCS-66(b)(2)UCS-66 governing thickness = 15.88 mm

Flange limits MDMT rating.

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

6.UCS-66(b)(1)(b) has been applied.Flange is impact test exempt to -105 C per UCS-66(b)(3) (coincident ratio = 0.3477)

Bolts rated MDMT per Fig UCS-66 note (c) = -48 C

7.

UCS-66(b)(1)(b) has been applied.Flange impact test exemption temperature from Fig UCS-66M Curve B = -19.38 CFig UCS-66.1M MDMT reduction = 25.2 C, (coincident ratio = 0.5716)UCS-66 governing thickness = 13.75 mm


8. Nozzle is impact test exempt to -105 C per UCS-66(b)(3) (coincident ratio = 0.0158).


10.Flange rating governs:Flange rated MDMT = -65 C (UCS-68(c) applies.)Bolts rated MDMT per Fig UCS-66 note (c) = -48 C

UCS-66(b)(1)(b)

11.

Material impact test exemption temperature from Fig UCS-66M Curve D = -48 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 45.3 C, (coincident ratio = 0.4207)Rated MDMT of -110.3C is limited to -48C by UCS-66(b)(2)


12.

Material impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 35.3 C, (coincident ratio = 0.4707)Rated MDMT of -81.3C is limited to -48C by UCS-66(b)(2)


13. Straight Flangegoverns MDMT

14. UCS-66 does not apply. Reference Fig. UCS-66.2 General Note (2)

15.

UCS-66(b)(1)(b) has been applied.Flange impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 34.3 C, (coincident ratio = 0.4782)Rated MDMT of -80.3C is limited to -48C by UCS-66(b)(2)UCS-66 governing thickness = 9.5 mm


16.

Material impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 45.9 C, (coincident ratio = 0.4186)Rated MDMT of -91.9C is limited to -48C by UCS-66(b)(2)


17.

UCS-66(b)(1)(b) has been applied.Flange impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 12.4 C, (coincident ratio = 0.779)Rated MDMT of -58.4C is limited to -48C by UCS-66(b)(2)UCS-66 governing thickness = 9.5 mm


18.Material impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 35.7 C, (coincident ratio = 0.4684)Rated MDMT of -81.7C is limited to -48C by UCS-66(b)(2)




21.

Nozzle impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 46 C, (coincident ratio = 0.4183)Rated MDMT of -92C is limited to -48C by UCS-66(b)(2)

UCS-66 governing thickness = 9.5 mm.

22. UCS-66 governing thickness = 9.5 mm.

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Nozzle impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 45.3 C, (coincident ratio = 0.4207)Rated MDMT of -91.3C is limited to -48C by UCS-66(b)(2)

Design notes are available on the Settings Summarypage.

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Revision History

No. Date Operator Notes

0 10/28/2013 rbarcenas New vessel created Heat Exchanger. [COMPRESS 2013 Build 7330]

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Settings Summary

COMPRESS 2013 Build 7330

Units: MKS

Datum Line Location: -34.00 mm from left seam

Design

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

Design or Rating: Get Thickness from Pressure

Minimum thickness: 1.5 mm 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 MAPCorrosion weight loss: 100% of theoretical loss

UG-23 Stress Increase: 1.20

Skirt/legs stress increase: 1.0

Minimum nozzle projection: 152.4 mmJuncture 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 : YesUG-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): No

UG-22(d)(2) Vessel supports such as lugs, rings, skirts, saddles and legs: YesUG-22(f) Wind reactions: No

UG-22(f) Seismic reactions: No

UG-22(j) Test pressure and coincident static head acting during the test: NoNote: UG-22(b),(c) and (f) loads only considered when supports are present.

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Radiography Summary

Radiography for Tube side chamber

Component

Longitudinal Seam Left Circumferential Seam Right Circumferential Seam

MarkCategory(Fig

UW-3)

Radiography /Joint Type

Category(Fig

UW-3)


Category(Fig

UW-3)

Radiography / JointType

TAPA BRIDADA CANAL N/A Seamless No RT N/A N/A N/A N/A / Gasketed N/A

ENVOLVENTE CANAL A Full UW-11(a) /Type 1

C Full UW-11(a) /Type 1

C Full UW-11(a) / Type1

RT1

BRIDA TAPA DEL CANAL N/A Seamless No RT N/A N/A / Gasketed CFull UW-11(a) / Type1

RT1

BRIDA CANAL --ESPEJO N/A Seamless No RT CFull UW-11(a) /Type 1

N/A N/A / Gasketed RT1

Front Stationary Tubesheet N/A Seamless No RT N/A N/A / Gasketed N/A N/A / Gasketed N/A

Rear Floating Tubesheet N/A Seamless No RT C N/A / Gasketed N/A N/A / Gasketed N/A

BRIDA BIPARTIDA N/A Seamless No RT N/A N/A / Gasketed C N/A N/A

TAPA FLOTANTE N/A Seamless No RT C N/A / Gasketed N/A N/A N/A

Tubes N/A Seamless No RT N/A N/A / Type 7 N/A N/A / Type 7 N/A

Nozzle Longitudinal SeamNozzle to Vessel

Circumferential Seam

Nozzle free end Circumferential

Seam

N6 SALIDA DE AGUA DE ENFRIAMIENTO (N6) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt/ Type 1

N/A

N7A CONEXION PARA LIMPIEZA QUIMICA (N7A) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt/ Type 1

N/A

IT2 INSTRUMENTO DE TEMPERATUIRA (IT2) N/A Seamless No RT D N/A / Type 7 N/A N/A N/A

IP2 INSTRUMENTO DE PRESION (IP2) N/A Seamless No RT D N/A / Type 7 N/A N/A N/A

N5 INTERCONEXION DE CANALES (N5) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt/ Type 1

N/A

N7B CONEXION PARA LIMPIEZA QUIMICA (N7B) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt/ Type 1

N/A


IT3 INSTRUMENTO DE TEMPERATUIRA (IT3) N/A Seamless No RT D N/A / Type 7 N/A N/A N/A

Nozzle Flange Longitudinal Seam Flange FaceNozzle to Flange


ASME B16.5/16.47 flange attached to N6 SALIDADE AGUA DE ENFRIAMIENTO (N6)

N/A Seamless No RT N/A N/A / Gasketed CUW-11(a)(4) exempt/ Type 1

N/A

ASME B16.5/16.47 flange attached to N7ACONEXION PARA LIMPIEZA QUIMICA (N7A)


N/A

ASME B16.5/16.47 flange attached to N5INTERCONEXION DE CANALES (N5)


N/A

ASME B16.5/16.47 flange attached to N7BCONEXION PARA LIMPIEZA QUIMICA (N7B)


N/A

Tube side chamber - UG-116(e) Radiography:RT1

Radiography for Shell side chamber

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Component

Longitudinal Seam Left Circumferential Seam Right Circumferential Seam

MarkCategory(Fig

UW-3)


Category(Fig

UW-3)


Category(Fig

UW-3)

Radiography / JointType

Front Stationary Tubesheet N/A Seamless No RT N/A N/A / Gasketed N/A N/A / Gasketed N/A

ENVOLVENTE 1 AFull UW-11(a) /Type 1

CFull UW-11(a) /Type 1

BFull UW-11(a) / Type1

RT1

BRIDA CUERPO ESPEJO FIJO N/A Seamless No RT N/A N/A / Gasketed CFull UW-11(a) / Type1

RT1

ENVOLVENTE 2 A Full UW-11(a) /Type 1 B Full UW-11(a) /Type 1 C Full UW-11(a) / Type1 RT1

BRIDA CUERPO -- BONETE N/A Seamless No RT CFull UW-11(a) /Type 1

N/A N/A / Gasketed RT1

Rear Shell Cylinder AFull UW-11(a) /Type 1

CFull UW-11(a) /Type 1

BFull UW-11(a) / Type1

RT1

BRIDA BONET --CUERPO N/A Seamless No RT N/A N/A / Gasketed CFull UW-11(a) / Type1

RT1

Rear Shell Head N/A Seamless No RT BFull UW-11(a) /Type 1

N/A N/A RT1

Rear Floating Tubesheet N/A Seamless No RT C N/A / Gasketed N/A N/A / Gasketed N/A

Nozzle Longitudinal SeamNozzle to Vessel

Circumferential SeamNozzle free end Circumferential

Seam

N2 INTERCONEXION DE ENVOLVENTE (N2) N/A Seamless No RT D N/A / Type 7 C UW-11(a)(4) exempt/ Type 1

N/A


IT4 INSTRUMENTO DE TEMPERATURA (IT4) N/A Seamless No RT D N/A / Type 7 N/A N/A N/A

N1 ENTRADA DEL FONDO DEL AGOTADOR (N1) N/A Seamless No RT D N/A / Type 7 CUW-11(a)(4) exempt/ Type 1

N/A


IT1 INDICADOR DE TEMPERATURA (IT1) N/A Seamless No RT D N/A / Type 7 N/A N/A N/A

Nozzle Flange Longitudinal Seam Flange FaceNozzle to Flange


ASME B16.5/16.47 flange attached to N2INTERCONEXION DE ENVOLVENTE (N2)


N/A

ASME B16.5/16.47 flange attached to N1 ENTRADADEL FONDO DEL AGOTADOR (N1) N/A Seamless No RT N/A N/A / Gasketed C UW-11(a)(4) exempt/ Type 1 N/A

Shell side chamber - UG-116(e) Radiography:RT1

Tubesheets are always considered to be seamless.

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Thickness Summary

ComponentIdentifier

Material Diameter(mm)

Length(mm)

Nominal t(mm)

Design t(mm)

Total Corrosion(mm)

JointE

Load

TAPA BRIDADA CANAL SA-516 70 788 OD 32 32* 29.42 0 1.00 Internal

ENVOLVENTE CANAL SA-516 70 635 ID 355 9.5 4.79 3.17 1.00 Internal

Front Stationary Tubesheet SA-516 70 665 OD 36.94 36.94 36.93 6.37 1.00 Unknown

Rear Floating Tubesheet SA-516 70 630 OD 36.94 36.94 36.93 6.37 1.00 Unknown

Tubes SA-179 Smls. Tube 19 OD 4,877 2.11 0.37 0 1.00 External

ENVOLVENTE 1 SA-516 70 635 ID 2,214 9.5 5.85 3.2 1.00 Internal

ENVOLVENTE 2 SA-516 70 635 ID 2,214 9.5 5.85 3.2 1.00 Internal

Rear Shell Cylinder SA-516 70 711 ID 243 9.5 6.16 3.2 1.00 Internal

Straight Flange on Rear Shell Head SA-516 70 711 ID 50.8 9.5 6.16 3.2 1.00 Internal

Rear Shell Head SA-516 70 711 ID 187.25 9.5* 6.12 3.2 1.00 Internal

Flange - TAPA FLOTANTE SA-105 609 ID 51.49 51.49 57.73 3.17 1.00 Unknown

TAPA FLOTANTE SA-516 70 609 ID 120.2 15.88* 13.46 6.37 1.00 External

Nominal t: Vessel wall nominal thickness

Design t: Required vessel thickness due to governing loading + corrosionJoint 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 ( kg) Contributed by Vessel Elements SurfaceAream2Metal

New*

Metal

Corroded* InsulationInsulationSupports

LiningPiping

+ Liquid

Operating Liquid Test Liquid

New Corroded New Corroded

TAPA BRIDADA CANAL 122.2 122.2 0 0 0 0 0 0 0 0 0.57

ENVOLVENTE CANAL 50.2 33.6 0 0 0 0 176.1 179.8 179.4 183.5 0.68

Front Stationary Tubesheet 80.6 47.8 0 0 0 0 0 0 0 0 0.08

Rear Floating Tubesheet 64.3 36.3 0 0 0 0 0 0 0 0 N/A

TAPA FLOTANTE 76.9 59.3 0 0 0 0 18.4 19.4 18.4 19.5 0

ENVOLVENTE 1 331.9 221.2 0 0 0 0 491.8 506.6 491.8 506.9 4.53

ENVOLVENTE 2 331.9 221.2 0 0 0 0 487 501.4 489.9 505 4.53

Tubes 1,581.3 1,581.3 0 0 0 0 309.5 309.5 309.5 309.5 N/A

Rear Shell Cylinder 40.9 27.3 0 0 0 0 76 79.1 77.6 80.9 0.56

Rear Shell Head 53.4 35.7 0 0 0 0 66.4 68.3 63.6 66 0.76

SILLETA 74.4 74.4 0 0 0 0 0 0 0 0 1.59

TOTAL: 2,808 2,460.3 0 0 0 0 1,625.1 1,664 1,630.2 1,671.3 13.29

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

Component

Weight ( kg) Contributed by Attachments

Surface Aream2Body Flanges Nozzles &Flanges

PackedBeds

TraysBaffles

Pass Partitions

TraySupports

Rings &Clips

VerticalLoads

New Corroded New Corroded

TAPA BRIDADA CANAL 0 0 0 0 0 0 0 0 0 0

ENVOLVENTE CANAL 175.4 166.1 46.4 40.7 0 0 0 0 0 1.02

Front Stationary Tubesheet 0 0 0 0 0 47.9 0 0 0 0

Rear Floating Tubesheet 29.8 27.1 0 0 0 0 0 0 0 0

TAPA FLOTANTE 0 0 0 0 0 0 0 0 0 0

ENVOLVENTE 1 87.7 83.1 19.6 17 0 49.8 0 0 0 0.45

ENVOLVENTE 2 113.6 109.4 19.6 17 0 49.8 0 0 0 0.45

Rear Shell Cylinder 90.8 85.6 0 0 0 0 0 0 0 0.25

Rear Shell Head 0 0 0 0 0 0 0 0 0 0

TOTAL: 497.3 471.3 85.5 74.7 0 147.4 0 0 0 2.17

Vessel operating weight, Corroded: 4,794 kg

Vessel operating weight, New: 5,163 kgVessel empty weight, Corroded: 3,130 kg

Vessel empty weight, New: 3,538 kg

Vessel test weight, New: 5,150 kgVessel test weight, Corroded: 4,782 kg

Vessel surface area: 15.47 m2

Vessel center of gravity location - from datum - lift condition

Vessel Lift Weight, New: 3,538 kg

Center of Gravity: 2,843.58 mm

Vessel Capacity

Shell side Capacity** (New): 1,130 litersShell side Capacity** (Corroded): 1,165 liters

Tube side Capacity** (New): 502 liters

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Tube side Capacity** (Corroded): 506 liters**The shell and tube capacity does not include volume of nozzle, piping or other attachments.

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Long Seam Summary

Shell Long Seam Angles

Component Seam 1

ENVOLVENTE CANAL 45

ENVOLVENTE 1 30

ENVOLVENTE 2 315

Rear Shell Cylinder 30

Shell Plate Lengths

ComponentStartingAngle

Plate 1

ENVOLVENTE CANAL 45 2,024.76 mm

ENVOLVENTE 1 30 2,024.76 mm

ENVOLVENTE 2 315 2,024.76 mm

Rear Shell Cylinder 30 2,263.52 mm

*Plate Lengths use the circumference of the vessel based on the mid diameter of the components

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Shell Rollout

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Test Report

Shop test pressure determination for Tube side chamber based on user defined pressure

Shop test gauge pressure is 9.1 kg f/cm2at 21.11 C

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

IdentifierLocal testpressurekgf/cm

2

Testliquidstatichead

kgf/cm2

ENVOLVENTE CANAL 9.19 0.09

TAPA FLOTANTE 9.19 0.09

Tubes 9.19 0.09

BRIDA TAPA DEL CANAL - Flange Hub 9.19 0.09

BRIDA CANAL --ESPEJO - Flange Hub 9.19 0.09

TAPA BRIDADA CANAL 9.19 0.09BRIDA TAPA DEL CANAL 9.19 0.09

BRIDA CANAL --ESPEJO 9.19 0.09

Front Stationary Tubesheet 9.19 0.09

Rear Floating Tubesheet 9.19 0.09

BRIDA BIPARTIDA 9.19 0.09

IP2 INSTRUMENTO DE PRESION (IP2) 9.12 0.02


IT2 INSTRUMENTO DE TEMPERATUIRA (IT2) 9.12 0.02

IT3 INSTRUMENTO DE TEMPERATUIRA (IT3) 9.2 0.1

N5 INTERCONEXION DE CANALES (N5) 9.22 0.12

N6 SALIDA DE AGUA DE ENFRIAMIENTO (N6) 9.13 0.03

N7A CONEXION PARA LIMPIEZA QUIMICA (N7A) 9.12 0.02

N7B CONEXION PARA LIMPIEZA QUIMICA (N7B) 9.2 0.1

Notes:(1) 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 Tube side chamber.

The test temperature of 21.11 C is warmer than the minimum recommended temperature of -27.58 C so the brittlefracture provision of UG-99(h) has been met.

Shop test pressure determination for Shell side chamber based on user defined pressure

Shop test gauge pressure is 14.95 kg f/cm2at 21.11 C

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

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IdentifierLocal testpressurekgf/cm

2

Testliquidstatichead

kgf/cm2

ENVOLVENTE 1 15.04 0.09

ENVOLVENTE 2 15.04 0.09

Rear Shell Cylinder 15.04 0.09

TAPA FLOTANTE 15.04 0.09

Straight Flange on Rear Shell Head 15.04 0.09

Rear Shell Head 15.04 0.09

Tubes 15.04 0.09

BRIDA CUERPO ESPEJO FIJO - Flange Hub 15.04 0.09

BRIDA CUERPO -- BONETE - Flange Hub 15.04 0.09

BRIDA BONET -- CUERPO - Flange Hub 15.04 0.09

Front Stationary Tubesheet 15.04 0.09

BRIDA CUERPO ESPEJO FIJO 15.04 0.09

BRIDA CUERPO -- BONETE 15.04 0.09

BRIDA BONET -- CUERPO 15.04 0.09Rear Floating Tubesheet 15.04 0.09

BRIDA BIPARTIDA 15.04 0.09



IT1 INDICADOR DE TEMPERATURA (IT1) 14.97 0.02

IT4 INSTRUMENTO DE TEMPERATURA (IT4) 15.05 0.1

N1 ENTRADA DEL FONDO DEL AGOTADOR (N1) 14.98 0.03

N2 INTERCONEXION DE ENVOLVENTE (N2) 15.07 0.12

Notes:

(1) 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 Shell side chamber.

The test temperature of 21.11 C is warmer than the minimum recommended temperature of -27.58 C so the brittlefracture provision of UG-99(h) has been met.

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Vacuum Summary

Component Line of Support

Elevation

aboveDatum(mm)

Length Le(mm)

TAPA BRIDADA CANAL - 2 N/A

- TAPA BRIDADA CANAL 34 N/A

ENVOLVENTE CANAL Left - 130.2 545.8

ENVOLVENTE CANAL Right - 485.2 545.8

Front Stationary Tubesheet - 575 N/A

- BRIDA CANAL --ESPEJO 579.8 N/A

- BRIDA CUERPO ESPEJO FIJO 613.54 N/A

ENVOLVENTE 1 Left - 708.14 4,607.6

ENVOLVENTE 1 Right - 2,922.14 4,607.6

ENVOLVENTE 2 Left - 2,922.14 4,607.6

ENVOLVENTE 2 Right - 5,136.14 4,607.6

- BRIDA CUERPO -- BONETE 5,221.14 N/A

- BRIDA BONET -- CUERPO 5,224.34 N/A

Rear Shell Cylinder Left - 5,316.34 446.12

Rear Floating Tubesheet - 5,415.06 N/A

- Flange - TAPA FLOTANTE 5,479.34 N/A

- 1/3 depth of TAPA FLOTANTE 5,479.34 N/A

Rear Shell Cylinder Right - 5,559.34 446.12

Straight Flange on Rear Shell Head Left - 5,559.34 446.12

TAPA FLOTANTE - 5,599.55 N/A

Straight Flange on Rear Shell Head Right - 5,610.14 446.12

- 1/3 depth of Rear Shell Head 5,670.45 N/A

Rear Shell Head - 5,797.39 N/A

NoteFor main components, the listed value of 'Le' is the largest unsupported length for the component.

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ENVOLVENTE CANAL


Component: CylinderMaterial specification: SA-516 70 (II-D Metric p. 18, ln. 19)Material is impact test exempt to -105 C per UCS-66(b)(3) (coincident ratio = 0.302)

Internal design pressure: P = 7 kg/cm2@ 66 C

Static liquid head:

Ps = 0.06 kg/cm2 (SG = 1, Hs= 638.17 mm,Operating head)

Pth = 0.09 kg/cm2 (SG = 1, Hs= 907.5 mm, Horizontal test

head)

Corrosion allowance Inner C = 3.17 mm Outer C = 0 mm

Design MDMT = -17.78 C No impact test performedRated MDMT = -105 C Material is not normalized

Material is not produced to Fine Grain PracticePWHT is performed

Radiography: Longitudinal joint - Full UW-11(a) Type 1Left circumferential joint - Full UW-11(a) Type 1Right circumferential joint - Full UW-11(a) Type 1

Estimated weight New = 50.2 kg corr = 33.6 kgCapacity New = 112.43 liters corr = 114.68 liters

ID = 635 mmLengthLc

= 355 mm

t = 9.5 mm

Design thickness, (at 66 C) UG-27(c)(1)

t = P*R / (S*E - 0.60*P) + Corrosion= 7.06*320.67 / (1,407.21*1.00 - 0.60*7.06) + 3.17= 4.79 mm

Maximum allowable working pressure, (at 66 C) UG-27(c)(1)

P = S*E*t / (R + 0.60*t) - Ps= 1,407.21*1.00*6.33 / (320.67 + 0.60*6.33) - 0.06= 27.39 kg/cm2

Maximum allowable pressure, (at 21.11 C) UG-27(c)(1)

P = S*E*t / (R + 0.60*t)= 1,407.21*1.00*9.5 / (317.5 + 0.60*9.5)= 41.36 kg/cm2

% Extreme fiber elongation - UCS-79(d)

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

= (50*9.5 / 322.25)*(1 - 322.25 / infinity)

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= 1.474%

The extreme fiber elongation does not exceed 5%.

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

A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.33)

= 0.002420B = 1,092.5 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHC = min(B, S) = 1,092.5 kg/cm2

Allowable Compressive Stress, Hot and New- ScHN, (table CS-2 Metric)

A = 0.125 / (Ro/ t)

= 0.125 / (327 / 9.5)= 0.003631

B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHN = min(B, S) = 1,169 kg/cm2

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

A = 0.125 / (Ro/ t)= 0.125 / (327 / 9.5)

= 0.003631

B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCN = min(B, S) = 1,169 kg/cm2

Allowable Compressive Stress, Cold and Corroded- ScCC, (table CS-2Metric)

A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.33)= 0.002420

B = 1,092.5 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCC = min(B, S) = 1,092.5 kg/cm2

Allowable Compressive Stress, Vacuum and Corroded- ScVC, (tableCS-2 Metric)

A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.33)

= 0.002420B = 1,092.5 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScVC = min(B, S) = 1,092.5 kg/cm2

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ENVOLVENTE 1


Component: CylinderMaterial specification: SA-516 70 (II-D Metric p. 18, ln. 19)Material impact test exemption temperature from Fig UCS-66M Curve D = -48 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 45.3 C, (coincident ratio = 0.4207)

Rated MDMT of -110.3C is limited to -48C by UCS-66(b)(2)UCS-66 governing thickness = 9.5 mm

Internal design pressure: P = 11.5 kg/cm2@ 90 C

Static liquid head:



head)


Design MDMT = -17.78 C No impact test performedRated MDMT = -48 C Material is normalized



Estimated weight New = 331.9 kg corr = 221.2 kg

Capacity New = 468.9 liters corr = 483.1 liters

ID = 635 mmLengthLc

= 2,214 mm

t = 9.5 mm




P = S*E*t / (R + 0.60*t) - Ps= 1,407.21*1.00*6.3 / (320.7 + 0.60*6.3) - 0.06= 27.26 kg/cm2


P = S*E*t / (R + 0.60*t)= 1,407.21*1.00*9.5 / (317.5 + 0.60*9.5)= 41.36 kg/cm2

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EFE = (50*t / Rf)*(1 - Rf/ Ro)= (50*9.5 / 322.25)*(1 - 322.25 / infinity)

= 1.474%



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.3)

= 0.002408B = 1,091.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHC = min(B, S) = 1,091.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (327 / 9.5)

= 0.003631B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 9.5)= 0.003631

B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.3)

= 0.002408B = 1,091.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCC = min(B, S) = 1,091.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.3)

= 0.002408

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B = 1,091.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScVC = min(B, S) = 1,091.4 kg/cm2

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ENVOLVENTE 2


Component: CylinderMaterial specification: SA-516 70 (II-D Metric p. 18, ln. 19)Material impact test exemption temperature from Fig UCS-66M Curve D = -48 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 45.3 C, (coincident ratio = 0.4207)



Static liquid head:



head)







ID = 635 mmLengthLc

= 2,214 mm

t = 9.5 mm




P = S*E*t / (R + 0.60*t) - Ps= 1,407.21*1.00*6.3 / (320.7 + 0.60*6.3) - 0.06= 27.26 kg/cm2


P = S*E*t / (R + 0.60*t)= 1,407.21*1.00*9.5 / (317.5 + 0.60*9.5)= 41.36 kg/cm2

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= 1.474%



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.3)

= 0.002408B = 1,091.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHC = min(B, S) = 1,091.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (327 / 9.5)

= 0.003631B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 9.5)= 0.003631

B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.3)

= 0.002408B = 1,091.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCC = min(B, S) = 1,091.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.3)

= 0.002408

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B = 1,091.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScVC = min(B, S) = 1,091.4 kg/cm2

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Rear Shell Cylinder


Component: CylinderMaterial specification: SA-516 70 (II-D Metric p. 18, ln. 19)Material impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 35.3 C, (coincident ratio = 0.4707)



Static liquid head:



head)


Design MDMT = -17.78 C No impact test performedRated MDMT = -48 C Material is not normalized





ID = 711 mmLengthLc

= 243 mm

t = 9.5 mm




P = S*E*t / (R + 0.60*t) - Ps= 1,407.21*1.00*6.3 / (358.7 + 0.60*6.3) - 0.07= 24.39 kg/cm2


P = S*E*t / (R + 0.60*t)= 1,407.21*1.00*9.5 / (355.5 + 0.60*9.5)= 37.01 kg/cm2

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= 1.3185%



A = 0.125 / (Ro/ t)

= 0.125 / (365 / 6.3)

= 0.002157B = 1,066.9 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHC = min(B, S) = 1,066.9 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 9.5)

= 0.003253B = 1,153.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHN = min(B, S) = 1,153.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 9.5)= 0.003253

B = 1,153.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCN = min(B, S) = 1,153.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 6.3)

= 0.002157B = 1,066.9 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCC = min(B, S) = 1,066.9 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 6.3)

= 0.002157

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B = 1,066.9 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScVC = min(B, S) = 1,066.9 kg/cm2

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TAPA BRIDADA CANAL


Component: Bolted CoverAttached to: BRIDA TAPA DEL CANALMaterial specification: SA-516 70 (II-D Metric p. 18, ln. 19)Bolted cover impact test exemption temperature from Fig UCS-66M Curve D = -48 C17 C MDMT reduction per UCS-68(c) applies.

Rated MDMT of -65C is limited to -48C by UCS-66(b)(2)UCS-66 governing thickness = 8 mm


Static liquid head:

Ps = 0.06 kg/cm2 (SG = 1, Hs= 638.17 mm, Operating head)

Pth = 0.09 kg/cm2 (SG = 1, Hs= 907.5 mm, Horizontal testhead)

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



Radiography: Category A joints - Seamless No RT

Estimated weight: New = 122.2 kg corr = 122.2 kg

Head diameter, d = 675 mm

Cover thickness, t = 32 mmDesign thickness, (at 66 C) UG-34 (c)(2), flange operating

t = d*Sqr(C*P / (S*E) + 1.9*W*hG/ (S*E*d3)) + Corrosion

= 675*Sqr(0.3*7.06 / (1,407.207*1) + 100*1.9*30,880.81*29 / (1,407.207*1*6753)) + 0= 29.42 mm

Design thickness, (at 21.11 C) UG-34 (c)(2), gasket seating

t = d*Sqr(1.9*W*hG/ (S*E*d3)) + Corrosion

= 10*675*Sqr(1.9*80,471.86*29 / (1,407.207*1*6753)) + 0= 21.61 mm

Maximum allowable working pressure, (at 66 C )

P = (S*E / C)*((t / d)2- (1.9*W*hG/ (S*E*d3))) - Ps= (1,407.207*1 / 0.3)*((32 / 675)2- (1.9*100*36,546.12*29 / (1,407.207*1*6753))) - 0.0638= 8.3 kgf/cm

2

Maximum allowable pressure, (At 21.11 C )

P = (S*E / C)*((t / d)2- (1.9*W*hG/ (S*E*d3)))

= (1,407.207*1 / 0.3)*((32 / 675)2- (1.9*100*36,546.12*29 / (1,407.207*1*6753)))= 8.36 kgf/cm

2

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= 1.3185%



A = 0.125 / (Ro/ t)

= 0.125 / (365 / 6.3)

= 0.002157B = 1,066.9 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHC = min(B, S) = 1,066.9 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 9.5)

= 0.003253B = 1,153.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHN = min(B, S) = 1,153.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 9.5)= 0.003253

B = 1,153.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCN = min(B, S) = 1,153.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 6.3)

= 0.002157B = 1,066.9 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCC = min(B, S) = 1,066.9 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 6.3)

= 0.002157

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B = 1,066.9 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScVC = min(B, S) = 1,066.9 kg/cm2

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Rear Shell Head


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

Internal design pressure: P = 11.5 kg f/cm2

@ 90 C

Static liquid head:

Ps= 0.07 kgf/cm2(SG=1, Hs=676.2 mm Operating head)

Pth= 0.09 kgf/cm2(SG=1, Hs=945.5 mm Horizontal test head)

Corrosion allowance: Inner C = 3.2 mm Outer C = 0 mm

Design MDMT = -17.78C No impact test performedRated MDMT = -48C Material is not normalized

Material is not produced to fine grain practicePWHT is performed

Do not Optimize MDMT / Find MAWP

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

Estimated weight*: new = 53.4 kg corr = 35.7 kgCapacity*: new = 63.7 liters corr = 66 liters* includes straight flange

Inner diameter = 711 mmMinimum head thickness = 9.5 mmHead ratio D/2h = 2 (new)Head ratio D/2h = 1.9823 (corroded)Straight flange length Lsf = 50.8 mmNominal straight flange thickness tsf = 9.5 mmResults Summary

The governing condition is internal pressure.Minimum thickness per UG-16 = 1.5 mm + 3.2 mm= 4.7 mmDesign thickness due to internal pressure (t) = 6.12mmMaximum allowable working pressure (MAWP) = 24.9kgf/cm

2

Maximum allowable pressure (MAP) = 37.5kgf/cm2

K (Corroded)K=(1/6)*[2 + (D / (2*h))2]=(1/6)*[2 + (717.4 / (2*180.95))2]=0.988261

K (New)

K=(1/6)*[2 + (D / (2*h))2]=(1/6)*[2 + (711 / (2*177.75))2]=1

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Design thickness for internal pressure, (Corroded at 90 C) Appendix 1-4(c)

t = P*D*K / (2*S*E - 0.2*P) + Corrosion= 11.57*717.4*0.988261 / (2*1,407.21*1 - 0.2*11.57) + 3.2= 6.12 mm

The head internal pressure design thickness is 6.12mm.

Maximum allowable working pressure, (Corroded at 90 C) Appendix 1-4(c)

P = 2*S*E*t / (K*D + 0.2*t) - Ps= 2*1,407.21*1*6.3 / (0.988261*717.4 +0.2*6.3) - 0.07= 24.9 kgf/cm

2

The maximum allowable working pressure (MAWP) is 24.9kgf/cm2.

Maximum allowable pressure, (New at 21.11 C) Appendix 1-4(c)

P = 2*S*E*t / (K*D + 0.2*t) - Ps= 2*1,407.21*1*9.5 / (1*711 +0.2*9.5) - 0= 37.5 kgf/cm

2

The maximum allowable pressure (MAP) is 37.5kgf/cm2.


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

= (75*9.5 / 125.62)*(1 - 125.62 / infinity)= 5.6719%

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42/232

BRIDA BIPARTIDA

ASME VIII-1, 2010 Edition, A11 Addenda Metric, Appendix 2 Flange Calculations

Flange is attached to: Rear Floating TubesheetFlange type: Lap joint loose

Flange material specification: SA-105 (II-D Metric p. 18, ln. 5)

Bolt material specification:SA-193 B7 Bolt


43/232

UCS-66(b)(1)(b) has been applied.Flange impact test exemption temperature from Fig UCS-66M Curve B = -19.38 C

Fig UCS-66.1M MDMT reduction = 26 C, (coincident ratio = 0.5614)UCS-66 governing thickness = 13.75 mmBolts rated MDMT per Fig UCS-66 note (c) = -48 C

The rated flange MDMT is -45.38 C

Flange calculations for Internal Pressure + Weight Only

Gasket details from facing sketch 1(a) or (b), Column II

Gasket width N = 10 mm

b0= N/2 = 5 mm

Effective gasket seating width, b = b0= 5 mm

hG= (C - G)/2 = (660 - 619)/2 = 20.5 mm

hD= (C - B)/2 = (660 - 608)/2 = 26 mm

hT= (C - G)/2 = (660 - 619)/2 = 20.5 mm

Hp= 2*b*3.14*G*m*P= 0.01*2*5*3.14*619*3.75*7

= 5,102.11 kgf

H = 0.785*G2*P

= 0.01*0.785*6192*7= 21,054.7 kgf

HD= 0.785*B2*P

= 0.01*0.785*6082*7

= 20,313.04 kgf

HT= H - HD= 21,054.7 - 20,313.04

= 741.66 kgf

Wm1= H + Hp= 21,054.7 + 5,102.11

= 26,156.81 kgf

Wm2= 3.14*b*G*y

= 0.01*3.14*5*619*534.3324= 51,928.08 kgf

Required bolt area, Am= greater of Am1, Am2= 29.607 cm2

Am1= Wm1/Sb= 26,156.81/1,753.911 = 14.9134 cm2

Am2= Wm2/Sa= 51,928.08/1,753.911 = 29.607 cm2

Total area for 32- 0.625 in dia bolts, corroded, Ab= 41.7031 cm2

W = (Am+ Ab)*Sa/2

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44/232

= (29.607 + 41.7031)*1,753.911/2= 62,535.86 kgf

MD= HD*hD= 20,313.04*0.026 = 528.1 kgf-mMT= HT*hT= 741.66*0.0205 = 15.2 kgf-m

HG= Wm1- H = 26,156.81 - 21,054.7 = 5,102.11 kgf

MG= HG*hG= 5,102.11*0.0205 = 104.6 kgf-m

Mo= MD+ MT+ MG= 528.1 + 15.2 + 104.6 = 647.9 kgf-m

Mg= W*hG= 62,535.86*0.0205 = 1,282 kgf-m

From FIG. 2-7.1, where K = A/B = 700/608 = 1.1513, Y = 13.8319

Stresses at operating conditions - VIII-1 Appendix 2-7

SR= SH= 0

ST= Y*Mo/(t2*B)

= 1e5*13.8319*647.9/(552*608)

= 487.287 kgf/cm2

Allowable stress Sfo= 1,407.207 kgf/cm2

STdoes not exceed Sfo

Stresses at gasket seating - VIII-1 Appendix 2-7

ST= Y*Mg/(t2*B)

= 1e5*13.8319*1,282/(552*608)

= 964.13 kgf/cm2

Allowable stress Sfa

= 1,407.207 kgf

/cm2

STdoes not exceed Sfa

Flange rigidity per VIII-1 Appendix 2-14

J = 109.4*Mo/(E*t3*KL*ln(K))

= 109.4*1,282/(20.52E+05*553*0.3*ln(1.1513))

= 0.9718

The flange rigidity index J does not exceed 1; satisfactory.

Flange calculations for External Pressure + Weight Only per VIII-1, Appendix 2-11



b0= N/2 = 5 mm


hG= (C - G)/2 = (660 - 619)/2 = 20.5 mm

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45/232

hD= (C - B)/2 = (660 - 608)/2 = 26 mm

hT= (C - G)/2 = (660 - 619)/2 = 20.5 mm

Hp= 2*b*3.14*G*m*P= 0.01*2*5*3.14*619*3.75*11.5

= 8,382.03 kgf

H = 0.785*G2

*P= 0.01*0.785*6192*11.5= 34,589.86 kgf

HD= 0.785*B2*P

= 0.01*0.785*6082*11.5= 33,371.42 kgf

HT= H - HD= 34,589.86 - 33,371.42

= 1,218.44 kgf

Wm1= H + Hp

= 34,589.86 + 8,382.03= 42,971.89 kgf

Wm2= 3.14*b*G*y= 0.01*3.14*5*619*534.3324= 51,928.08 kgf


Am1= 0.785*G2*(Pm- Pr)/Sb= 0/1,753.911 = 0 cm

2

Am2= Wm2/Sa= 51,928.08/1,753.911 = 29.607 cm2


W = (Am2+ Ab)*Sa/2= (29.607 + 41.7031)*1,753.911/2

= 62,535.86 kgf

Mo= HD*(hD- hG) + HT*(hT- hG)

= 33,371.42*(0.026 - 0.0205) + 1,218.44*(0.0205 - 0.0205)= 183.5 kgf-m

Mg= W*hG= 62,535.86*0.0205 = 1,282 kgf-m

From FIG. 2-7.1, where K = A/B = 700/608 = 1.1513, Y = 13.8319


SR= SH= 0

ST= Y*Mo/(t2*B)

= 1e5*13.8319*183.5/(552*608)= 138.035 kgf/cm

2

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STdoes not exceed Sfo


ST= Y*Mg/(t2*B)

= 1e5*13.8319*1,282/(552*608)= 964.13 kgf/cm

2

Allowable stress Sfa= 1,407.207 kgf/cm2

STdoes not exceed Sfa


J = 109.4*Mo/(E*t3*KL*ln(K))

= 109.4*1,282/(20.52E+05*553*0.3*ln(1.1513))= 0.9718


42/227


47/232

BRIDA BONET -- CUERPO


Flange is attached to: Rear Shell Cylinder (Left)Flange type: Weld neck integralFlange material specification: SA-105 (II-D Metric p. 18, ln. 5)



48/232

17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 12.4 C, (coincident ratio = 0.779)Rated MDMT of -58.4C is limited to -48C by UCS-66(b)(2)UCS-66 governing thickness = 9.5 mmBolts rated MDMT per Fig UCS-66 note (c) = -48 C

The rated flange MDMT is -48 C




b0= N/2 = 6.5 mm

Effective gasket seating width, b = 2.5*b01/2= 6.37 mm

G = gasket OD - 2*b = 743 - 2*6.37 = 730.25 mm

hG= (C - G)/2 = (799 - 730.25)/2 = 34.37 mm

hD= R + g1/2 = 25 + 15.83/2 = 32.92 mm

hT= (R + g1+ hG)/2 = (25 + 15.83 + 34.37)/2 = 37.6 mm

Hp= 2*b*3.14*G*m*P= 0.01*2*6.37*3.14*730.25*3.75*11.5675= 12,677.72 kgf

H = 0.785*G2*P= 0.01*0.785*730.252*11.5675= 48,423.88 kgf

HD= 0.785*B2

*P= 0.01*0.785*717.342*11.5675= 46,726.29 kgf

HT= H - HD= 48,423.88 - 46,726.29= 1,697.59 kgf

Wm1= H + Hp= 48,423.88 + 12,677.72= 61,101.6 kgf

Wm2= 3.14*b*G*y

= 0.01*3.14*6.37*730.25*534.3324= 78,081.84 kgf


Am1= Wm1/Sb= 61,101.6/1,753.911 = 34.8373 cm2

Am2= Wm2/Sa= 78,081.84/1,753.911 = 44.5187 cm2


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W = (Am+ Ab)*Sa/2= (44.5187 + 70.2837)*1,753.911/2= 100,676.66 kgf

MD= HD*hD= 46,726.29*0.0329 = 1,538 kgf-mMT= HT*hT= 1,697.59*0.0376 = 63.8 kgf-m

HG= Wm1- H = 61,101.6 - 48,423.88 = 12,677.72 kgf

MG= HG*hG= 12,677.72*0.0344 = 435.8 kgf-m

Mo= MD+ MT+ MG= 1,538 + 63.8 + 435.8 = 2,037.6 kgf-m

Mg= W*hG= 100,676.66*0.0344 = 3,460.5 kgf-m

The bolts are adequately spaced so the TEMA RCB-11.23 load concentration factor does not apply.

46/229


50/232

Hub and Flange Factors

g0= min(g0, tn) = min(6.33, 6.3) = 6.3

h0= (B*g0)1/2= (717.34*6.3)1/2= 67.22 mm

From FIG. 2-7.1, where K = A/B = 854/717.34 = 1.1905

T = 1.8428 Z = 5.7926 Y = 11.2272 U = 12.3376

h/h0= 0.476 g1/g0= 2.5129

F = 0.8234 V = 0.1921 e = F/h0= 0.1225

d = (U/V)*h0*g02= (12.3376/0.1921)*6.7223*0.632

= 171.3114 cm3


f = 2.1263

L = (t*e + 1)/T + t3/d

= (6*0.1225 + 1)/1.8428 + 63

/171.3114= 2.2023

SH= f*Mo/(L*g12*B)

= 1e5*2.1263*2,037.6/(2.2023*15.832*717.34)= 1,094.397 kgf/cm

2

SR= (1.33*t*e + 1)*Mo/(L*t2*B)

= (1.33*60*0.0122 + 1)*1e5*2,037.6/(2.2023*602*717.34)= 70.845 kgf/cm

2

ST= Y*Mo/(t2*B) - Z*SR

= 1e5*11.2272*2,037.6/(602*717.34) - 5.7926*70.845

= 475.482 kgf/cm2


Allowable stress Sno= 1,407.207 kgf/cm2

STdoes not exceed SfoSHdoes not exceed Min[ 1.5*Sfo, 2.5*Sno] = 2,110.811 kgf/cm

2

SRdoes not exceed Sfo0.5(SH+ SR) = 582.621 kgf/cm

2does not exceed Sfo0.5(SH+ ST) = 784.94 kgf/cm

2does not exceed Sfo


SH= f*Mg/(L*g12*B)= 1e5*2.1263*3,460.5/(2.2023*15.832*717.34)= 1,858.663 kgf/cm

2

SR= (1.33*t*e + 1)*Mg/(L*t2*B)

= (1.33*60*0.0122 + 1)*1e5*3,460.5/(2.2023*602*717.34)= 120.319 kgf/cm

2

ST= Y*Mg/(t2*B) - Z*SR

= 11.2272*1e5*3,460.5/(602*717.34) - 5.7926*120.319

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51/232

= 807.533 kgf/cm2


Allowable stress Sna= 1,407.207 kgf/cm2

STdoes not exceed SfaSHdoes not exceed Min[ 1.5*Sfa, 2.5*Sna] = 2,110.811 kgf/cm

2

SRdoes not exceed Sfa0.5(SH+ SR) = 989.491 kgf/cm

2does not exceed Sfa

0.5(SH+ ST) = 1,333.098 kgf/cm2

does not exceed Sfa


J = 52.14*V*Mo/(L*E*g02*KI*h0)

= 1e5*52.14*0.1921*3,460.5/(2.2023*20.52E+05*6.32*0.3*67.22)= 0.9585


BRIDA BONET -- CUERPO - Flange hub


Component: Flange hubMaterial specification: SA-105 (II-D Metric p. 18, ln. 5)Material impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 35.7 C, (coincident ratio = 0.4684)Rated MDMT of -81.7C is limited to -48C by UCS-66(b)(2)UCS-66 governing thickness = 9.5 mm


Static liquid head:



head)




Radiography: Longitudinal joint - Seamless No RT

Left circumferential joint - N/ARight circumferential joint - Full UW-11(a) Type 1



ID = 711 mmLengthLc

= 32 mm

t = 9.5 mm

48/229


52/232




P = S*E*t / (R + 0.60*t) - Ps

= 1,407.21*1.00*6.33 / (358.67 + 0.60*6.33) - 0.07= 24.51 kg/cm2


P = S*E*t / (R + 0.60*t)= 1,407.21*1.00*9.5 / (355.5 + 0.60*9.5)= 37.01 kg/cm2


A = 0.125 / (Ro/ t)= 0.125 / (365 / 6.33)

= 0.002168B = 1,067.9 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHC = min(B, S) = 1,067.9 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 9.5)

= 0.003253B = 1,153.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHN = min(B, S) = 1,153.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 9.5)= 0.003253

B = 1,153.4 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCN = min(B, S) = 1,153.4 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 6.33)

= 0.002168B = 1,067.9 kg/cm2

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53/232

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCC = min(B, S) = 1,067.9 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (365 / 6.33)

= 0.002168B = 1,067.9 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScVC = min(B, S) = 1,067.9 kg/cm2

50/229


54/232

BRIDA CANAL --ESPEJO


Flange is attached to: ENVOLVENTE CANAL (Right)Flange type: Weld neck integralFlange material specification: SA-105 (II-D Metric p. 18, ln. 5)



55/232






b0= N/2 = 5 mm


G = (gasket OD + gasket ID) / 2 = (685 + 665) / 2 = 675 mm

hG= (C - G)/2 = (733 - 675)/2 = 29 mm

hD= R + g1/2 = 35 + 10.83/2 = 40.42 mm

hT= (R + g1+ hG)/2 = (35 + 10.83 + 29)/2 = 37.42 mm

Hp= 2*P*(b*3.14*G*m + br*rl*m')= 0.01*2*7.0638*(5*3.14*675*3.75 + 3.17*2*2)= 5,616.16 kgf

H = 0.785*G2*P= 0.01*0.785*6752*7.0638= 25,264.65 kgf

HD= 0.785*B2*P

= 0.01*0.785*641.342*7.0638= 22,807.73 kgf

HT= H - HD= 25,264.65 - 22,807.73= 2,456.91 kgf

Wm1= H + Hp= 25,264.65 + 5,616.16= 30,880.8 kgf

Per VIII-1 Appendix 2-5(a)(2): Wm1from the mating flange governs so Wm1= 50,122.39 kgf

Wm2= 3.14*b*G*y + br*rl*Y'= 0.01*3.14*5*675*534.3324 + 3.17*2*175.767= 56,637.07 kgf

The pass partition gasket load has been included in the calculation of Wm1and Wm2per TEMA RGP-RCB-11.7.



Am1= Wm1/Sb= 50,122.39/1,753.911 = 28.5775 cm2

Am2= Wm2/Sa= 71,049.43/1,753.911 = 40.5091 cm2

52/229


56/232


W = (Am+ Ab)*Sa/2= (40.5091 + 59.4708)*1,753.911/2= 87,678.03 kgf

MD= HD*hD= 22,807.73*0.0404 = 921.8 kgf-mMT= HT*hT= 2,456.91*0.0374 = 91.9 kgf-m

HG= Wm1- H = 50,122.39 - 25,264.65 = 24,857.75 kgf

MG= HG*hG= 24,857.75*0.029 = 720.9 kgf-m

Mo= MD+ MT+ MG= 921.8 + 91.9 + 720.9 = 1,734.6 kgf-m

Mg= W*hG= 87,678.03*0.029 = 2,542.7 kgf-m


53/229


57/232


g0= min(g0, tn) = min(6.33, 6.33) = 6.33

h0= (B*g0)1/2= (641.34*6.33)1/2= 63.72 mm


T = 1.8273 Z = 4.9243 Y = 9.5462 U = 10.4904

h/h0= 0.5022 g1/g0= 1.7109

F = 0.8359 V = 0.2675 e = F/h0= 0.1312

d = (U/V)*h0*g02= (10.4904/0.2675)*6.3716*0.6332

= 100.1071 cm3


f = 1

L = (t*e + 1)/T + t3/d

= (6.1*0.1312 + 1)/1.8273 + 6.13

/100.1071= 3.2526

SH= f*Mo/(L*g12*B)

= 1e5*1*1,734.6/(3.2526*10.832*641.34)= 708.945 kgf/cm

2

SR= (1.33*t*e + 1)*Mo/(L*t2*B)

= (1.33*61*0.0131 + 1)*1e5*1,734.6/(3.2526*612*641.34)= 46.131 kgf/cm

2


= 1e5*9.5462*1,734.6/(612*641.34) - 4.9243*46.131

= 466.706 kgf/cm2




2

SRdoes not exceed Sfo0.5(SH+ SR) = 377.538 kgf/cm

2does not exceed Sfo0.5(SH+ ST) = 587.826 kgf/cm



SH= f*Mg/(L*g12*B)= 1e5*1*2,542.7/(3.2526*10.832*641.34)= 1,039.221 kgf/cm

2

SR= (1.33*t*e + 1)*Mg/(L*t2*B)

= (1.33*61*0.0131 + 1)*1e5*2,542.7/(3.2526*612*641.34)= 67.622 kgf/cm

2


= 9.5462*1e5*2,542.7/(612*641.34) - 4.9243*67.622

54/229


58/232

= 684.131 kgf/cm2




2



0.5(SH+ ST) = 861.676 kgf/cm2

does not exceed Sfa


J = 52.14*V*Mo/(L*E*g02*KI*h0)

= 1e5*52.14*0.2675*2,542.7/(3.2526*20.52E+05*6.332*0.3*63.72)= 0.6938


BRIDA CANAL --ESPEJO - Flange hub


Component: Flange hubMaterial specification: SA-105 (II-D Metric p. 18, ln. 5)Material is impact test exempt to -105 C per UCS-66(b)(3) (coincident ratio = 0.302)


Static liquid head:



head)




Radiography: Longitudinal joint - Seamless No RTLeft circumferential joint - Full UW-11(a) Type 1Right circumferential joint - N/A



ID = 635 mmLengthLc

= 32 mm

t = 9.5 mm

55/229


59/232




P = S*E*t / (R + 0.60*t) - Ps

= 1,407.21*1.00*6.33 / (320.67 + 0.60*6.33) - 0.06= 27.39 kg/cm2


P = S*E*t / (R + 0.60*t)= 1,407.21*1.00*9.5 / (317.5 + 0.60*9.5)= 41.36 kg/cm2


A = 0.125 / (Ro/ t)= 0.125 / (327 / 6.33)

= 0.002420B = 1,092.5 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHC = min(B, S) = 1,092.5 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (327 / 9.5)

= 0.003631B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 9.5)= 0.003631

B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.33)

= 0.002420B = 1,092.5 kg/cm2

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60/232

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScCC = min(B, S) = 1,092.5 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.33)

= 0.002420B = 1,092.5 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScVC = min(B, S) = 1,092.5 kg/cm2

57/229


61/232

BRIDA CUERPO -- BONETE


Flange is attached to: ENVOLVENTE 2 (Right)Flange type: Weld neck integralFlange material specification: SA-105 (II-D Metric p. 18, ln. 5)



62/232

17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 12.4 C, (coincident ratio = 0.779)Rated MDMT of -58.4C is limited to -48C by UCS-66(b)(2)UCS-66 governing thickness = 9.5 mmBolts rated MDMT per Fig UCS-66 note (c) = -48 C





b0= N/2 = 6.5 mm

Effective gasket seating width, b = 2.5*b01/2= 6.37 mm

G = gasket OD - 2*b = 743 - 2*6.37 = 730.25 mm

hG= (C - G)/2 = (799 - 730.25)/2 = 34.37 mm

hD= R + g1/2 = 63 + 15.83/2 = 70.92 mm

hT= (R + g1+ hG)/2 = (63 + 15.83 + 34.37)/2 = 56.6 mm

Hp= 2*b*3.14*G*m*P= 0.01*2*6.37*3.14*730.25*3.75*11.5638= 12,673.56 kgf

H = 0.785*G2*P= 0.01*0.785*730.252*11.5638= 48,407.99 kgf

HD= 0.785*B2

*P= 0.01*0.785*641.342*11.5638= 37,337.5 kgf

HT= H - HD= 48,407.99 - 37,337.5= 11,070.49 kgf

Wm1= H + Hp= 48,407.99 + 12,673.56= 61,081.54 kgf


Wm2= 3.14*b*G*y= 0.01*3.14*6.37*730.25*534.3324= 78,081.84 kgf


Am1= Wm1/Sb= 61,101.6/1,753.911 = 34.8373 cm2

Am2= Wm2/Sa= 78,081.84/1,753.911 = 44.5187 cm2

59/229


63/232


W = (Am+ Ab)*Sa/2= (44.5187 + 70.2837)*1,753.911/2= 100,676.66 kgf

MD= HD*hD= 37,337.5*0.0709 = 2,647.8 kgf-mMT= HT*hT= 11,070.49*0.0566 = 626.6 kgf-m

HG= Wm1- H = 61,101.6 - 48,407.99 = 12,693.61 kgf

MG= HG*hG= 12,693.61*0.0344 = 436.3 kgf-m

Mo= MD+ MT+ MG= 2,647.8 + 626.6 + 436.3 = 3,710.7 kgf-m

Mg= W*hG= 100,676.66*0.0344 = 3,460.5 kgf-m


60/229


64/232


g0= min(g0, tn) = min(6.33, 6.3) = 6.3

h0= (B*g0)1/2= (641.34*6.3)1/2= 63.56 mm


T = 1.7838 Z = 3.5869 Y = 6.9337 U = 7.6194

h/h0= 0.5034 g1/g0= 2.5129

F = 0.8161 V = 0.1837 e = F/h0= 0.1284

d = (U/V)*h0*g02= (7.6194/0.1837)*6.3562*0.632

= 104.6257 cm3


f = 1.9795

L = (t*e + 1)/T + t3/d

= (5.3*0.1284 + 1)/1.7838 + 5.33

/104.6257= 2.365

SH= f*Mo/(L*g12*B)

= 1e5*1.9795*3,710.7/(2.365*15.832*641.34)= 1,932.593 kgf/cm

2

SR= (1.33*t*e + 1)*Mo/(L*t2*B)

= (1.33*53*0.0128 + 1)*1e5*3,710.7/(2.365*532*641.34)= 165.914 kgf/cm

2


= 1e5*6.9337*3,710.7/(532*641.34) - 3.5869*165.914

= 833.051 kgf/cm2




2

SRdoes not exceed Sfo0.5(SH+ SR) = 1,049.254 kgf/cm

2does not exceed Sfo0.5(SH+ ST) = 1,382.822 kgf/cm



SH= f*Mg/(L*g12*B)= 1e5*1.9795*3,460.5/(2.365*15.832*641.34)= 1,802.302 kgf/cm

2

SR= (1.33*t*e + 1)*Mg/(L*t2*B)

= (1.33*53*0.0128 + 1)*1e5*3,460.5/(2.365*532*641.34)= 154.729 kgf/cm

2


= 6.9337*1e5*3,460.5/(532*641.34) - 3.5869*154.729

61/229


65/232

= 776.889 kgf/cm2




2



0.5(SH+ ST) = 1,289.596 kgf/cm2

does not exceed Sfa


J = 52.14*V*Mo/(L*E*g02*KI*h0)

= 1e5*52.14*0.1837*3,710.7/(2.365*20.14E+05*6.32*0.3*63.56)= 0.9859


BRIDA CUERPO -- BONETE - Flange hub


Component: Flange hubMaterial specification: SA-105 (II-D Metric p. 18, ln. 5)Material impact test exemption temperature from Fig UCS-66M Curve B = -29 C17 C MDMT reduction per UCS-68(c) applies.Fig UCS-66.1M MDMT reduction = 45.9 C, (coincident ratio = 0.4186)Rated MDMT of -91.9C is limited to -48C by UCS-66(b)(2)UCS-66 governing thickness = 9.5 mm


Static liquid head:



head)




Radiography: Longitudinal joint - Seamless No RT

Left circumferential joint - Full UW-11(a) Type 1Right circumferential joint - N/A



ID = 635 mmLengthLc

= 32 mm

t = 9.5 mm

62/229


66/232




P = S*E*t / (R + 0.60*t) - Ps

= 1,407.21*1.00*6.33 / (320.67 + 0.60*6.33) - 0.06= 27.39 kg/cm2


P = S*E*t / (R + 0.60*t)= 1,407.21*1.00*9.5 / (317.5 + 0.60*9.5)= 41.36 kg/cm2


A = 0.125 / (Ro/ t)= 0.125 / (327 / 6.33)

= 0.002420B = 1,092.5 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

ScHC = min(B, S) = 1,092.5 kg/cm2


A = 0.125 / (Ro/ t)

= 0.125 / (327 / 9.5)

= 0.003631B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 9.5)= 0.003631

B = 1,169 kg/cm2

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2



A = 0.125 / (Ro/ t)

= 0.125 / (327 / 6.33)

= 0.002420B = 1,092.5 kg/cm2

63/229


67/232

S = 1,407.2 / 1.00 = 1,407.2 kg/cm2

Cl-r Mec-mc-ot-791-01 Rev. 0 Modificado

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Transcript of Cl-r Mec-mc-ot-791-01 Rev. 0 Modificado