Section VIII_Division 2_Rules for Construction of Pressure Vessels

Date of Issuance: July l, 2007

was developed under procedures accredited as meeting the criteria for American National Arnerlcain National Standard. The Standards Committee that approved the code or standard was balanced competent and concerned interests have had an opportunity to participate. The proposed code or standard was made available for public review and comment that provides an opportunity for additional public input from industry, academia, regulatory agencies, and the public-at-large. ASME does not "approve," "rate," or "endorse" any item, construction, proprietary device, or activity. ASME does not take any position with respect to the validity of any patent rights asserted in connection with any items mentioned in this document, and does not undertake to insure anyone utilizing a standard against liability for infringement of any applicable letters patent, nor assume any such liability. Users of a code or standard are expressly advised that determination of the validity of any such patent rights, and the risk of infringement of such rights, is entirely their own responsibility. Participation by federaI agency representative( s) or person( s) affiliated with industry is not to be interpreted as government or industry endorsement of this code or standard. ASME accepts responsibility far only those interpretations of this document issued in accordanee with the established ASME procedures and policies, which precludes the issuance of interpretations by individuals. The footnotes in this document are part of this American National Standard.

ASME collective membership mark

The above ASME symbols are registered in the U.S. Patent Office.

is

trademark of

American

of Mechanical Engineers.

No part of this document may be reproduced in any fonn, in an electronic retrieval system or otherwise, without the prior written pennission of the publisher. Library of Congress Catalog Card Number: 56-3934 Printed in the United States of America Adopted by the Council of the American Society of Mechanical Engineers, 1914. Revised 1940, 1941, 1943, 1946, 1949, 1952, 1953, 1956, 1959, 1962, 1965, 1968, 1971, 1974, 1977, 1980, 1983, 1986, 1989, 1992, 1995, 1998, 2001, 2004, 2007 The American Society of Mechanical Engineers Three Park Avenue, New York, NY 10016-5990

Copyright © 2007 by Alt Rights Reserved

Rules for Construction of Power Boilers II

Materials Part A Part Part C -

Ferrous Material ;:,pleClllC,aU()llS Nonferrous Material ;:)peClnCatHJns for "-"'-'_""~"'-''"',..,,>, and Filler Metals

Rules for Construction of Nuclear Subsection NCA - GeneraI KeQUJlrelments for Division l and Division Division Subsection NB Class Subsection NC - Class 2 Compom~nts Subsection ND - Class 3 Compommts Subsection - Class MC LO]mpIOne~nts Subsection NF -.:"..,,""''''.,.!- Structures Subsection NG Subsection Lo,m{'Onlenlts in Elevated 'errmeratllre Service 2-

Code for

"'--vu,.''"'~''''

Containments

Division 3 Containments for and and Level Radioactive Material and Waste

u V'-_'U"';:;;'''''

of

Nuclear Fuel

Rules for Construction of He:atulg Boilers V

Nondestructive Examination for

VII

Recommended liUIOellTIleS

...,."t,,,,,,

11-""..

It"""...... "'t,''''''

Rules Rules for Construction

Pressure Vessels

IX "",ni"",.,.,,,,,,,f'j

Plastic Pressure Vessels

for Inservice mS,pe<;nOln of Nuclear Rules for Construction

Plant LOmr'OI1tents of

Tanks

LAJIIUl~~U-SIlt~~l r1U'U\.-l.IUa., which include additions and revisions to individuaI Sections of sent aultonlatlcaH the Sections up to the pUbll<:atJlOn of Code. The 2007 in loose-Ieaf f\.UU~IlUa will be issued the 'epJlaClement-p'l.ge formato

The Boiler and Pressure VesseI Committee meets reguto consider additions and revisions to the Code and to formulate Cases to the intent reCIUlI'eIl1lell1ts or when the need is rules for materials or constructions not covered Code rules. Those Cases that have been ad()pte~d will appear in the 2007 Code Cases book: "Boilers and Pressure Vessels" and "Nuclear LOlmlJOIlerlts. ments will be sent to the of the of the 20 l O Code. Code Cases books up to the

ASME issues written mt1erpret:itlcm of technicai of the Code. The pn~tat:lOrlS for each individuaI Section will be nnnl1,,, ... e,,... set=lar::l.tely and will be included as of the to that Section. of Section Divisions l service to Subsecand 2, will be included with the tion NCA.

iv

A"'''''UTA1rri

xix

t'ersonnel

xxiii

1.1

1.2.1 1.2.2 1.2.3 1.2.4 .2.5 1.2.6 1.2.7 1.3 l

1.6 Annex .A. 1.A.2 1.A.3 .A.4 .A.5 .A.6

GeneraI .. Introduetion . >rganìzatìon . Definitions 1-2 .................................................................................................................................................. 1-3 Overview 1-3 Additional for Pressure Vessels 1-4 of This Division 1-4 Geometrie Classifieations Outside the of this Division 1-4 1-5 Combination Units Field ofVessels 1-5 Pressure Relief Deviees . Standards Refereneed Division 1-6 1-6 Units ofMeasurement Teehnieal 1-7 Tables 1-8 Boiler And Introduetion Format. Code Revisions or Additions Code Cases Code

Vessel Standards LOlmlnlttee 1-1O 1-10 1-1 1-1l 1-1

Annex I.B.2

Introduetion Definition ofTerms

1-13 1-13 ASME Boiler And

1-15 1-16 l.C.4

2.1. 2.1 2.1.3 2.2 2.2. 2.2.2

Introduetion Definitions Code

..

lJser

v

2.3.3 2.3.4 2.3.5

............. 2-6

2.4 2.4.1 2.4.2 2.4.3

Annex 2.A.l 2.A.2

Annex 2.B.l 2.B.2 2.B.3

User's GeneraI Certification ofthe User's Tables

2-1 O 2-12

Guide For A lVI::mlilla«:tulrer's GeneraI Certification ofManufacture's Tables

Annex 2.C 2.C.l Manufacturer's Data 2.C.2 Partial Data 2.C.3 Maintenance ofRecords

Annex 2.D.2

2-13 2-13

2-17

Manufacturer's Data Introduction Tabies

2.E.I 2.E.3

2.E.6 2.E.8 2.E.9

lO 2.E.l3 2.E.l4 2.E.15 2.E.16

Controi Examination Correction ofNonconformities

2-29

Nondestructive EX,lmlnatlOn Reat Treatment Calibration ofMeasurement and Test Records Retention Forms lns:De(~tlcm ofVessels and Vessel Parts lnS:De(~t1cm of Pressure Relief Vaives

2-29 2-29 2-30 2-30 2-30 2-30

.1'1JlQ.L"-'JlJUI

Lo/.UUfi.J'HF,

Vesseis with

lnd[ep~~nC1ent

Chambers

2-31

lJUl=lHcate l'\lamt;plale

2-33 of Characters for of Vesseis or ...............................................................................................................................................2-34 \.mmg~errtents

2.F.8

2.G.2 2.G.3 2.G.4 2.G.5 2.G.6 2.G.7

tle::mnllZ Officiai for Authorization Issuance of Authorization

2-35 2-35

Controi Evaluation for Authorization and Reauthorization Code Construction Before ofCertificate of Authorization

2-36 2-36 2-37

Introduction Tables

2-38 2-39

Annex 2.H.2 2.H.3

PART3 MATERIALS 3.1 3.2 3.2.1 3.2.2 3.2.3 3.2.5 3.2.6 3.2.7 3.2.8 3.2.9 3.2.10 3.2.1 3.3 3.3.2 3.3.3 3.3.4 3.3.5 3.3.6 3.4 3.4.1 3.4.2 3.4.3 3.4.4 3.4.5 3.5.1 3.5.3

GeneraI Materials Permitted For Construction ofVessel Materials for Pressure Parts Materials for Attachments to Pressure Parts Materials Dissimilar MateriaIs

3-4 3-4 3-4 3-4 3-5 .

Product~~<~~'T·'~~hA'~0

Certification Product Identification and Prefabricated or Preformed Pressure Parts Definition ofProduct Thiclmess Product Form Tolerances Purchase

3-6 3-6 3-7 3-8 3-8 3-9 3-9 3-9 3-9 3-9 3-9

NorLten~ous

GeneraI. It-

,,,,,

,,...

LJIU.U.UJ.HUU\.JU

, ofPlates

Ma1tenalls ,

,

,

3-13 3-13 3-13

,

,.,

3.6.4 3.7 3.7.2 3.7.3 3.7.4 3.7.6 3.7.7 3.8.1 3.8.2 3.8.3 3.9 3.9.1 3.9.2 3.9.3 3.9.4 3.10 3.10. 3.10.2 3.10.3 3.10.4 3.10.5 3.10.6 3.11 3.1 L 3.11.2 3.11.3 3.11.4 3.11.5 3.11.6 1.7 3.11.8 3.12 3.13 3.14 5 3.17 3.18 3.19

3.A. 3,A,2 3.A.3

and Nuts ofStuds hre:adlIlg and Use ofvVashers ,." Ferrous ,.'"., Nonferrous Materials for Ferrous and Nonferrous Nuts of :SU1DPlemental R.eOll1n;~me;nts for '-'u,:nUJl;:;:," . G·enerai. .. eml1re:ments for Ferrous '-''',''.UI;:;:,'' Reamrenlenìs for Nonferrous '-''''''''Uj'''U SulDplementaLK.eOllln;~memtsfor Rubs :Machined From Plate

" ,.,3-15 3-15 3-15

,

3-16

,

Material ReaUJlrelnellts, Examination " , " , ,.. ", , , , , Data and , , , , , , , Material Test ." , , , , , " , "., ,., , , Generai., , emlln;~mtmts for Test I_i..., .......,."... ..... ,,""'c from of Test Procedure for and Procedure for Reat Test from Ferrous Materials Test Reat for Nonferrous Materials Material , Generai. Carbon and Low Steels , Ferritic Steels Non-Ferrous , , 1vIaterials Procedures ,., , Procedures and Test Plates ofFerrous Materials Allowable Stresses Stn~nQth Parameters \.../V

IJ'-'H0

3-19

, ,", ,

,.. , ,

3-19 3-19 3-20 3-20

,

\.../V .... IJ.VH..:l

\.../V' .... IJ'VHC' . . . . . . . . ,. . .

, ,

,.. ,

3-22 3-22 3-23 3-23 3-23

3-32 3-32 3-32 3-34 3-36 3-36

N omenclature Definitions Tables

Allowable Stress Basis - An Materials Allowable Stress Basis Materials Tables

3-70 3-70 3-72 '.. """"",,,,,,+1117

viii

Not

3.D.5.1

3.D.7

3.E.1 3.E.2 3.E.3 3.E.4

Modulus Thermal Coefficìent Thermal COJlc1uctnllty

!lJ'""
Cm"ves Curves Curves

Welded Joìnt Nomenciature Tables

DESIGN

3-107 3-107

3-1 08 . 3-111 3-112

RULE <>r'I111"'''''"''t:.nte

.1

4. .2 4.1.3 4.1.5 4.1.6 4.1.7 4.1.8

4. .9 4.1.10 1. 4.1 4.1

4.2

KeqmremeI1lts ............'

4-7

Corrosion Allowance Basis Allowable Stress Materiais Combination Combination Units "n""'''',,,,,,,,, and WeId InternaI and Nomenciature Tables Rules for WeIded Joints ..!WH,UHi';;."

4-6 4-6 4-6 4-7 4-7 4-9 4-10 4-10

.

4-1 4-12 4-13

4-14

4.2.2 4.2.4 4.2.6 4.2.7 4.2.8 4.3 4.3.2 4.3.3 4.3.4 4.3.5 4.3.6 4.3.7 4.3.8 4.3.9

Shell To1erances 'uh11"1r!ru'n! Shells Conica1 Shells ~pIlerJcal Shells and OflS'phl:;flCal Heads .t'.,lllPSl~IQal Heads Areas Not

1-II",.,."",lt...

4-48 4-49 4-49 Heads

4-49

4-49

·<:>1t1r,,,,

.LAU-V'W-,,"U

lO

IX

"'~""Io<"""'''-''''''' •••••••••••••••••••••••••••••••••••• 4-55 ... ~ 'Io<"".."- "" •••••••••••••••••••••••••••••••••••••••••• 4-58

Nomenclature

4.4 4.4.1 4.4.2 4.4.4 4.4.6 4.4.7 4.4.8 4.4.10 4.4.11 4.4.12 4.4.13 4.4.14 4.4.15 4.4.16 4.4.17 4.5 4.5.1 4.5.2 4.5.3 4.5.4 4.5.5 4.5.6 4.5.7 4.5.8 4.5.9 4.5.10 4.5.12 4.5.14 4.5.15 4.5.16 4.5.17 4.5.18 4.5.19 4.6 4.6.1 4.6.2 4.6.3 4.6.4 4.6.5 4.6.6 4.6.7 4.7 4.7. 4.7.2 4.7.3 4.7.4 4.7.5

4-60

.......................................................................................................................................4-74 .4-81 Rules Shells Under Extemal Pressure Stresses Factors 4-82 MateriallJ...",,,,,,,, 'tl"''' Shell Tolerances 4-83 :Yllnancal Shell 4-84 Conical Shell 4-88 ~pnenc:al Shell and Head 4-89 oru,phl~ncal Head 4-90 blllpSOlOal Head 4-91 Local Thin Areas 4-91 Drilled Holes Not the Vessel Wall .4-91 .4-91 Combined and Allowable Stresses Shell Transition Junctions Without A Knuckle 4-1 00 v ''-.VBj''''' Shell Transition Junctions With A Knuckle 4-1 00 4-1 01 Nomenclature TabIes 4-1 05 .....................................................................................................................................4-106 Ru1es for Shells in Shells and Heads 4-113 .......................................................................................................................................4-113 Dimensions and ofNozzles .4-113 .4-113 Method ofNozzle Attachment. Nozzle Neck Minimum Thickness .4-114 RadiaI Nozzle in a Shell 4-114 .4-118 Hillside Nozzle in a Shell Nozz1e in a Shell Oriented at an from the Axis .4-118 RadiaI Nozzie in a Conical Shell 4-118 Nozzle in a Conical Shell 4-119 RadiaI Nozzie in a Shell or 19 Hillside or Nozzle in a Formed Head 4-123 .4-123 Circular Nozzles in a Flat Head ~p,lcmlg l{,eql11rE~m{mts for Nozzles 4-124 ~tn~ng~m ofNozzle Attachment Welds .4-125 Local Stresses in Nozzles in Shells and Formed Heads from Extemal Loads 4-128 lnSl)ec1tlOn upEmmgs 4-129 upemngs ~UlDlelCI to Stress ..r''\,...vUJl''''

Tables

4-147

Rules for Dished Bolted Covers .4-154 .......................................................................................................................................4-154 A Thickness Thickness KelJUrrenlents C Thickness KelJUlrenlents Head

x

Nomenclature TabIes

4-160 4-162

4.7.8

4.8.3 4.8.4 4.8.5 4.8.6 4.9 4.9.1 4.9.2 4.9.3 4.9.4 4.9.5 4.9.6 4.9.7 4.10 4.10. 4.10.2 4.10.3 10.4 4.10.5 4.11 4.1 4.1 .2 4.11.3 4.11.4 4.11.5 4.1 .6 1.7 4.11.8 1.9 4.12 4.12.1 4.12.3 4.12.4 4.12.5 4.12.6 4.12.7 4.12.8 4.12.9 4.12.10 4.12.12 4.12.13 13 4.13.1 4.13.2 4.13.3 4.13.4 4.13.5 4.13.6 4.13.7 4.13.8 4.13.9

uperateet Closures 4-167 for Closures .4-167 Rules for and Surfaces .4-168 .......................................................................................................................................4-168 .I.."-""''-II.<''J.'"'''' Thickness ofBraced and Surfaces .4-168 .I.."-""''-II.<''J.'"'''' UlntlenSlOllS and and 4-168 KelQUlrenlents for Welded-in and Welded 4-168 Nomenclature 4-170 Tables 4-171 .....................................................................................................................................4-172 Rules for 4-173 . 4-173 HA

'iH

Uy

"'f'l111 a,l'na,Mi-",

LIg;amem bII]CI~enc:y and the Weld Joint Factor 4-174 Nomenclature 4-174 .....................................................................................................................................4-175 Rules for Jacketed Vessels 4-179 .......................................................................................................................................4-179 of Jacketed Shells and Jacketed Heads 4-179 of Closure Member of Jacket to VesseI 4-180 of Penetrations Jackets 4-180 ofPartial Jackets , 4-181 Jackets 4-181 , , 4-182 Nomenclature Tables 4-183 Rules for NonCircular Vessels 4-197 .......................................................................................................................................4-197 GeneraI 4-197 "'r111"'·"'l'n".n1-", for Vessels With Reinforcement. .4-198 "''-'I111''''''l'n".ni-", for Vessels With ",r'l111"''''l'n".ni-", for Vessels With Small Ratios .4-20 l Weld Joint Factors Noncircular Vessels to External Pressure ",,...1-<.n,,,,,,l I",.,. Vessels With Two or More Fabrication

Size

.4-206 4-206

Vessels

4-261

Definitions GeneraI. for InternaI Pressure for External Pressure ofWelded Joints Nozzle

4-261 4-261 4-261 4-262 4-262

Xl

""'l1rln"l''t~

...

4.15.3 4.15.5 4.15.6 4.15.7 4.15.8 4.16 4.16. 4.16.2 4.16.3 4.16.4 4.16.5 4.16.6 4.16.7 4.16.8 4.16.9 4.16.10 16.1 4.16.12 4.16.13 4.16. 4.17 4.17.1 4.17.2 4.17.3 4.17.4

4.17.8 4.18 4.18.1 18.2 4.18.3 18.4 4.18.5 4.18.6 18.7 4.18.8 4.18.9 4.18.10 l 4.18.12 18.13 18.14

~

...........•.•..••......••.•• , ......••••.•••.....•..•••• , ....•.. , •••......• "., .....• , ", .....• " •..•.

,4-264

... , " , , ,.,., ,, , " 4-268 ofVessels Outside ofTolerance " ,.. , , , ,.,., ..,., , .4-281 Tolerances,,, " 4-281 Local Areas " " " " 4-281 ...............................................................................................................4-281 .....................................................................................................................................4-282 Attachments 4-283 ...............................................................................................................................................4-283 of 4-283 Saddle for Horizontal Vessels .4-283 Skirt for Vertical Vessels .4-290 And Nomenclature 4-292 Tables 4-293 .....................................................................................................................................4-295 Rules for Joints 4-303 .......................................................................................................................................4-303 Considerations 4-303 IA . . U'H

Materials Gasket Materials Bolt Loads Procedure ...

4-304 4-305 4-305 4-306

'n~~"n ~~GG~

••••••••••••• O ••••••••• "

•••••••••••••••••••••• "

with a Circular Bore with Nut Joint Procedures Nomenclature Tables

ermmologv GeneraI Considerations GeneraI Conditions for "'V"''''H''''''~ L.·"~_.~~r< Extension ublesheet Characteristics Rules for the ofU-Tube Tubesheets Rules for the ofFixed Tubesheets Rules for the Tubesheets Tube-to-Tubesheet Welds Thin-Walled Joints

•• •••••••••••••••••••••••••••••••••••• "

•••••••••••

".4-308

4-308 4-308 4-308 4-309 4-312

4-344 4-344 4-345 4-345 .4-347 4-352 .4-365 4-375 4-378

.....................................................................................4-379

Xll

4.18.15

Nomenciature TabIes

4-381 4-386

4.18.17

4.19.2

.....................................................................................................4-404 4-404 Materiais 4-406 Unreinforced Bellows .4-406 u-~,naìDeG Reinforced Bellows .4-409 Kplln"'lC 4-410 Bellows to or 4-41 4-414 Fabrication Examination 4-414 Pressure Test Ke iQmrenlents U~n._U~F, and 4-414 ~pe~C1IJlcatlOn Sheet for Joints 4-415 4-416 Nomenciature TabIes 4-418 Conlslett~ratJ:ons

'LJ-L'UUI""''-''

4.19.6 4.19.7 4.19.8 4.19.9 4.19.10 4.19. 4.19.12 4.19.13 4.19.14 4.19. 5 4.19.16 4.19.17

H

>,.:"",,,,,,.,,-j--,,-,,..d-''-''14>

Sheets

4-438

4.A

4.:8 Introduction

And

Closures 4-441 4-441

Kes.porlslbll1t1I~S

4.B.3 4.B.5 4.B.6 4.B.7

Annex 4.C.l 4.C.2 4.C.3 4.C.4 4.C.5 4.C.6 4.C.7 4.C.8

Installation 4-442 lnS1Jec1tlOn 4-443 ...........................................................................................................................................4-443 Administrative Controls 4-443

GeneraI Maximum Axiai Loads Shear Load Test \cceptan<:e Standards for Joint \cceptam:e Standards for Nomenciature Tabies

Factor Determined Test.. Determined

Test

4-445 4-445 .4-447 .4-447 4-448

5-3 5.1. 5.1.2 5.1.3 5.2.1 5.2.2 5.2.3 5.3 5.3.1 5.3.2 5.3.3

Protection Overview Stress Method Limit-Load Method Elastic-Plastic Stress Method Protection Locai Failure

5-5 5-5 5-8 5-9 5-11 1 1 1

5.5.1 5.5.3 5.5.4 5.5.6 5.5.7 5.6 5.7 5.7.1 5.7.2 5.7.3 5.8 5.9 5.10 l

5.14 5.15

Service Stress Rel:lulrenlents . Assessment OfBolts Arnl1 ""1Y'Y'l"" 1"c for Perforated Plates ""1Y'Y'l"" 1"c for Vessels bXpeI'lmental Stress Fracture Mechanic Evaluations Definitions Nomenclature Tables Arll11

Stress 5.A.l

5-30 5-31 5-31 5-31 5-31 5-34 5-40

For Stress Classification

.................................................................................................................................................5-56

5.A.3 .Selection of Stress Classification Lines 5.A.4 Stress Method 5.A.4.1 Continuum Elements 5.A.4.2 Shell Elements 5.A.5 Structural Stress Method Based on Nodal Forces 5.A.5.1 Overview 5.A.5.2 Continuum ~~"'''H''''H'''' 5.A.5.3 Shell Elements Structural Stress Method Based on Stress 1 1"'''''''.. '''+'r .... 5.A.6 5.A.7 Nomenclature 5.A.8 Tables 5.A.9

5-56 5-57 5-57 5-58 5-59

5-60

,

,

,

5-61 5-62

,.. ,

5.B.3 ."''''''1"1 ,,,,

5.B.6

Method

,

,

5-76

Nomenclature

ute~m(:lt1rlg

Nomenclature '"

Stress for Elastic 5-84

.:> 5-88 ....................................................................................................................................5-89 ",,-,UI•..,U4

5.D.5

Tables

5.E.4 5.E.5 5.E.6 5.E.7 5.E.8

ofthe Solid Stlithess Effects of the Tubes 5-96 Effective Material for the Solid Plate 5-96 Pressure Effects Tubesheet Perforations 5-98 Protection Plastic Protection ">c'a.. Nomenclature 5-1 03 Tables 5-107 .............................................................................................................................................5-132 '-'VBUIV"'"

I !,'OH.

5.E.10

Annex 5.F 5.F.I Overview 5-137 Strain Measurement Test Procedure for Stress Lomj:lonent:s. 5.F.3 Protection 5-142 Nomenclature .............................................................................................................................................5-144

6 6.1 6.1.1 6.1.2 6.1.3 6. 6.1.5 6.1.6 6.2. 6.2.2 6.2.3 6.2.4 6.2.5 6.2.6 6.2.7 6.2.8 6.3 6.3.1 6.3.2 6.3.3 6.3.4 6.4.1 6.4.2 6.4.3 6.4.4 6.4.5 6.5

Procedure Treatment of Weldments Ke'ClUIrenlents for ofWelds Ke'ClUIrenlents for Postweld Treatment Procedures for Postweld Treatment. '~~'.n"'''~~ of Postweld Treatment. Postweld Heat Treatment after reaLtmem ofNonferrous Materials Ke ClUlrenlents For CIad or Weld o

"" .. "

i

xv

O"

"

•• "

""""

""

,,

o

,,""""""" ,.

"" • • ""

0

""" 0,.0

"'

6-16 6-18 6-20 6-20 6-22

6.5.7 6.5.8 6.5.9 6.6 6.6.1 6.6.2 6.6.3 6.6.4 6.6.5 6.6.6 6.6.7 6.6.8 6.6.9 6.6.10 6.7 6.7.1 6.7.2 6.7.3 6.7.4 6.7.5 6.7.6 6.7.7 6.7.8 6.7.9 6.7.10 6.7.1 6.7.12 6.8 6.8.1 6.8.2 6.8.3 6.8.4 6.8.5 6.8.6 6.8.7 6.8.9 6.8.10 6.9 6.10 6.11

6-24

Tests IJ'rAnprtu bnnalnc~~a.

Q

Ferritic Steels

GeneraL and Other Materials After Minimum Thickness after "'r"""''''.....-.'''.... 'I-.-.

•••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• '"

Postweld Treatment Heat Treatment Certification Tests Examination lns,oe<;tlcln and Tests Stamp1mg and Keamrenlents for Fabrication General. Ultrasonic Examination VU~.HH Requllrelnenlts Tolerances on Methods Heads Heat Treatment for Fabrication For Fabrication ofDefects in Material. Threaded Connections to Vessel and Heads lnSoe(~tlOn, and Stamping and for Vessels Pressure ReliefDevices Fabrication for Vesseis GeneraL Fabrication Ke!(lmrenlents Fabrication vual1:nc,;ll1cm and Records -': < + J:{.eqllln;~me~nts for Welded Joints Nondestmctive Examination ofWelded Joints Welded Joint bI][lClenc~v Contact between Vent Holes Heat of Weldments " .. Nomenclature Tables .H.V.....U .. ""U.À""H

6-24 6-24 6-24 6-24 6-24 .6-25 6-27 6-28

.,

..''''''

6-29 6-29 6-29 6-29 6-29 6-30 6-30 6-31 6-32 6-33

-'-'AUJ.HH.JUUVJJ,

6-34 6-34 6-34 6-34 6-34 6-34 6-35 6-36

6-3ì

INSPECTION AND EXAMINATION 7.1 7.2 7.2.1 7.2.2 7.2.3 7.3 7.3.1 7.3.2 7.3.3 7.3.4

and ofthe Manufacturer and Access for Notification ofWork Verification and Examination Prior To ofMaterial with DimensionaI

xvi

7-3 7-3 7-3 7-3 7-3 7-3 7-3 7-3 7-3 7-3

'-'!J""A"',~'VA

Pertormance

VUUUJU"-"Ul\J'H

.

7.4 Vesseis Extent ofNondestructive Examination 7-4 Selection of Examination Method for FIaws 7-6 Selection Method for Surface Flaws 7-6 Surface Condition and 7-6 SU1JPl iemiental Examination for Service 7-6 EX:lmllnatlon and of Vessels with Protective and 7-6 Examination and ofTensile Q and T Vessels 7-7 Examination and Vessels 7-8 Examination ofFabricated Vessels 7-9 Examination Method Criteria 7-11 7-1 GeneraI. Visual Examination 7-Il KadlO,gr2lPhlC Examination 7-12 Ultrasonic Examination 7-14 Ultrasonic Examination Used in Lieu Examination 7-15 Malgn~;tlc Particle Examination 7-17 Perletr'ant Examination 7-19 Current Surface Examination Procedure Evaluation and Retest for Partial Examination 7-23 7-23 Examination of Vessel. Surface Examination after Hu,rlrryr",,,l' lm:pec:::tìcm of Lined VesseI after 7-23 Leak Acoustic Emission 7-23 Tables 7-24 ...............................................................................................................................................7-36 IJ'rp'~~111I'P

7.4.5 7.4.6 7.4.7 7.4.8 7.4.9 7.4.10 7.4.11 7.5 7.5.1 7.5.2 7.5.3 7.5.4 7.5.5 7.5.6 7.5.7 7.5.8 7.5.9 7.6.1 7.6.2 7.7 7.8 7.9 7.10

Annex 7.A And Duties 7.A.1 GeneraI 7.A.2 Manufacturer's 7.A.2.1 Manufacturer 7.A.2.2 and Examination 7.A.3 7.A.3.1 7.A.3.2 lnspe(:t1oln and Examination Duties 7.A.4 Tables

8.1 8.1. 8.1 8.1.3 8.1.4 8.2 8.2.1 8.2.2 8.2.3 8.2.4 8.2.5 8.3 8.3.

And Examination Activities 7-50 7-50 7-50 7-50 7-51 7-51 7-53

8-2 Selection of Pressure Test Methods Construction

Test Test Procedures Test Examination and

8.3.3

XVll

8-2 8-3 8-4 8-5 8-5 8-5 8-5 8-5 8-6 8-6 8-6 ............... 8-6

8.4 8.4.2 8.5 8.6

~~'H"'~,yv>~,,,,,+C'

9.

h,A"" A"''''" A n"'"Arr,rA""'"1"'A Protection

.2

9.lJ 1.4

9.3 9.3.1 9.3.2 9.3.3

9.4.2 9.4.3 9.5 9.6 9.6.1

9.7 9.7.1 9.7.2 9.7.3

and Allowable Pressure ofPressure ReliefDevices Pressure ReliefValves on··Ke:C!CISUlg Pressure ReliefDevices U,,,,,,+,,,..,,, Disk Devices Devices Loaded Pressure ReliefDevices For Different Pressures And/Or Fluids Calculation OfRated GeneraI. U".r."."+,,,,,,,, of Certified for Different Pressures Conversion of Certified for Different In-Service Fluids lVlarKulg and Devices Provisions for Installation of Pressure GeneraI. .. " Inlet for Pressure Relief Devices from Pressure Relief Devices ~orH{eCJlOS]lllg Pressure ReliefDevices Protection eouwernenlts Documentation Manufacturer' s Data hlA"rr\1l",CH'<'"n1l"A

9.A 9.A.l 9.A.2 9.i\oc.3 9.A.4 9.A.6 9.A.7 9.A.8 9.A.9 9.A.I0

Introduction Provisions for

For

Installation And

Installation of

OfPressure ReliefDevices

Valves in the Relief Path

into Common Header Regar'dulg Pressure Relief Device 1l.... "'".,,+,~~ ~.--'-Fl-.. for Pressure ReliefValves Pressure ReliefValve Orientation Reaction Forces of Pressure Relief Devices for Conditions D".",coC'" .."" Ir,rl"~"+".",,,,, Devices to Monitor Pressure Differential -f

xviii

9-2 9-2 9-2 9-2 9-3 9-3 9-3 9-3 9-3 9-3 9-3 9-3 9-3 9-4 9-4 9-4 9-4 9-4 9-4 9-4 9-4 9-4 9-5

9-6 9-6 9-9 9-9 9-10

of LVlt;;cnamCal bnguleerS set up a purpose of formlliating steam boilers and other pressure cornmlìttf~e is now called the and Pressure VesseI Committee. Committee' s is to establish rules of to pressure the construcpressure tanks and COJmoon;ents, and inservice for pressure ''''''0''''-''''' of nuclear and and '... ;'",~, ..a" these rules when arise their code does not address other to the construction pressure tanks nuclear and the inservice mspe(;t!cm of nuclear and tanks. The user of the Code should to other """"";'111"l,,,,,... or other relevant documents. With few eX(;eDltìons, the rules do not, of reflect the likelihood and consequences of deterioration in service related to service fluids or extemal environments. the Committee has wide of construction rules this Section to allow the user or his to select those which will r'I-r"',UlrfP a pressure vessel for deterioration in service so as to safe of usefulness. it is not intended that this Section beusedas

The Committee recogltUZ(eS used for and resses and

nor of cornpo'nerlts Code. ....,"""'''''''''''.. COJmDutf~r programs for are cautioned are resno:nsltHe as~mn[}ptlOrlS inherent in the programs use and of these programs to are res.ponslble for the their The Code does not address tolerances. When or other are not with the values of these are considered nominaI and allowable tolerances or Iocal variances may be considered when based on enl~ìneermg luclgrnellt and standard as determined the

f

01J'-''''UA'-''Y

""J",'I.lJlUUV.U0,


and Pressure VesseI Committee deals with of boilers and pressure vesseis in rules of to the extent of pnlctlce as an aid to owners and their lm;oectC)rs. The rules established the Committee are not to be rec:onlm,en(lm:g, or any or as in any way manufacturer' s freedom to choose any method of or any of construction that conforms Code rules. reguBoiler and Pressure VesseI Committee new rules as dictated to consider revisions of the tecnn()lo:glcal (1levelODlmeIlL Code and requests Pressure Vessel ....-rr" .. offidal ,.....,,,........""..,"

the care and

r'<:J>

of the Code. tmgmeermg luclgnlents with Code be used to overrule mand,ltOJry prC)hltHt!lons of the Code.

consideration and action Dn:~DaratLOn of technical mOIUUles sions to Code from lnCI1Hf'leS Main Committee for Jlu.'''' COlmlnìttee becomes effective of Committee and U L " J ' L'L'.!.

Construction, as used in this Foreword, is an alI-inclusive commaterials, design, fabrication, examination, inspection, testing, centiticatlO,n, and pressure relief. l

xix

nationai or~:amlzatlOnls. When is made in an ASME H~"""VAH.U "n~,,,,jh,,,,hr,..-. to a non-ASME for which a COlmpamon ASME the referas to the ASME ence shall be alI materiais included the material sp~~cljt1c,lt1(mS in Section have been for Code is limited to thosemateriais and lise. at Ieast one of the other Sections of the Code for aU1Dw..:ation under rules that Section. An materials allowed these various Sections and used for construction scope of their rules shall be fumished accordance material contained in Section II or referenced in the Guidelines for ASTM Editions Section Parts A and except where otherwise Code Cases or in the Section of the Code. Materials covered these are for use items covered the Code Sections to the indicated the Section. Materials for Code use should and documented on this ASTM Editions in Section Part A and Guideline for ASTM Editions in Section Part list editions of ASME and that meet ASME reCluu'emlen1ts year dates of and which may be used in Code construction. Material n ...",;h"~orl to an with reqluu'errlents different the reclulI'errlents fications listed in the Guideline for ASTM Editions in Part A or Part B may also be used in accordance with the the material manufacturer or vesseI manufacturer certifies with evidence to the Authorized that of listed in ASTM Editions n"''',f!H,~""rI to an limited as to ",-,."..-.1h'" When reQU1fE~a shall be .nt,"rn-..""t'::'r! re(:og;m:l~ea

HA....'VJ.A ...A

may date of issuance shown on for revisions to sp~~Cl'nc,m(ms in Parts A and become mandasix months after such date of for boilers or pressure vessels contracted for to the end of the six-month Revisions to material "nco"-n,,,,., tions are the American for and Materials and other national or intemational and are ASME. those revisions may or may not any effect on the of to earlier editions of for use ASME construction. ASME material for use in each construction Code are listed in the Guidelines for "'L'~L""_able ASTM Editions in Section Parts A and B. These Guidelines for each the latest edition and earlier and later editions considered to be identical for ASME construction. Boiler and Pressure Vessel Committee in formuestablishment of maximum lation of its rules and and pressures considers HA"'''V~.~UJ.LJ, methods of 1-on..n"o,",;-.-, devices. The Code Committee does on whether a composhall or shall not be constructed to the of the Code. of each Section has been established to the Committee the Code rules. Vu,esl1011S or issues of a COlmpon~~nt with the Code rules to be directed to the ASME Certificate Holder conof Code are to directed the to ASME and Pressure Vessel Committee. AH'-WVAA",A

LJU'''''''''A'JU,

',",O"-'T'1rU

xx

ASME has established

to authorize various activities in accordance reqluu'ernlen:ts of the ASME Boiler and Pressure is the or~~anlZanOJl1s so authorized. to various activities in accordance with the of the Code rnay state this its literature. that are authorized to use Code 'u1mhn'" n.""E> iterns or constructions that have been constructed in with the ASME Boiler and Pressure Vessel Code are issued Certificates of Authorization. lt is the airn ofthe to rnaintain the of Code for the benefit of users, enforcernent and the holders of the "'''..,....k,-"I''' who with aH reClluu'ernient:s. Based on these ,."k'la"'~H""":' established on usage Certificates of Code construction. The Arnerican does not " or YU";UUl'b-U

Or!l~anlzatlo]ls to

or!~an.iz2ltìoln u v ............., a Authorization rnay state in 'O'Irh,TPrh""n:rr lite:rature COllstructions, or activities "are built (prodll1ce~d or activities conducted with the of the ASME Boiler and Pressure Vessel of the ASME and " or "rneet the Pressure Vessel Code." shaH be used for and The ASME in the Code. i-InuT"""""" nalne'plates as facsirniles rnay be used for the purpose of tos:tering use of such construction. Such usage rnay be who tion or or a holder of a Code rnay also use the facsimile in to show that spe~cHlea iterns will carry the GeneraI usage is when aH of a rnanufacturer' s iterns are constructed under the rules. ASME which is the cloverleaf with the letters shaH not be used any other ASME than ASME.

'-PJ.F,<'U.U"""Ul.U'JU'::> J.u"...

",j-.,nri1,nn

-'-'Hl;;;'J.U'b-''''J..::>

xxi

2007 Edition of Section ASME and ufiider'stancimg of the code ae~vell:mrnerlt .......,,""""'''' OuiblH:atJlOn ABB Lummus

hngmeermg Co. lnspe<;tlOln & Insurance LOlmp:my

Inc. Inc. The Board of Boiler and Pressure Vessellns,oec:;tors The Pressure VesseI Research Council LLC Material

Division 2 addresses user reOIUlrem,ent:s, To ensure that the 2007 edition of Section Certificate Holders listed below a beta test of the new Section the 2004 edition of Section Division 2. The a vesseI new code. ASME would like to

ATB Riva CBI Inc. Hitachi Zosen Mechanical ,"-,U'.L.VAH,

Kobe Ltd. Larsen & Toubro Sumitomo The Steel

Ariake Works Ltd.- Nuclear Power Division

LlrrnH~Q-jl1e,lVY I-H'\,"",n,"",,,,, ...,nnr

As of

1,2007

MAIN COMMITTEE G. G. Karcher, Chair

J. G. Feldstein, Vice Chair J. S. Brzuszkiewicz, ""'r-r",f':::lrll R. W. Barnes R. J. Basile

J. D. L. Berger M. N. Bressler D. A. Canonico R. P. Deubler D. A. Douin R. E. Gimple M. Gold T. E. Hansen C. L. Hoffmann D. F. Landers W.M. J. R.

U. R. Miller P. A. Molvie C. C. W. E. Norris G. C. Park P. Pastor M. D. Rana B. W. Roberts F. J. Schaaf, Jr. A. Selz R. W. Swayne D. E. Tanner S. V. Voorhees F. B. Kovacs, Alternate R. A. Moen, Honorary Member Tahara, '-"'-'C""CIlC

COMMITTEE (MAIN

J. G. Feldstein, Chair G. G. Karcher, Vice Chair J. S. Brzuszkiewicz, ''''r-,..",f'"",,, R. W. Barnes D.L. M. Gold G. C. Park

T. P. Pastor A. Selz D. E. Tanner A. Canonico, Ex-Officio Member M. Kotb, Ex-Officio Member

MEMHEKS (MAIN

F. P. Barton R. D. Bonner R. j. Bosnak R. J. Cepluch L. J. Chockie T. M. Cullen W.D. j. R. Farr

E.

M. H. Jawad A. J. Justin E. L. Kemmler W. G. Knecht J. LeCoff T. G. McCarty G. C. Millman

HONORS AND AWARDS

J. R. MacKay, Chair M. Gold, Vice Chair G. Moino, '",r-rp.t':::lrll R. J. Basile J. E. Batey D. L. Berger j. G. Feldstein F. E. Gregor

W. L. Haag, Jr. S. F. Harrison, Jr. R. M. Jessee W. C. Larochelle T. Pastor A. Selz R. R. Stevenson

MARINE CONFERENCE GROUP

J. Petow

H. N. Patel, Chair L. W. Douthwaite

R.

D. A. Douin - Illinois (Chair) R. D. Reetz - North Dakota (Vice Chair) D. E. Tanner - Ohio (Secretary) R. j. Aben, jr. - 1\III1'h"~:::ln j. S. Adaro - California A. Adkins - West j. T. Amato - Minnesota E. A. Anderson - Illinois F. Andrus B. P. Island R. D. Austin - Colorado E. W. Bachellier - Nunavut, Canada M. M. Barber - I\Alt'hl
D. C. Cook - California R. A. Coomes - Kentucky D. Eastman - Newfoundland and Labrador, Canada G. L. Ebeyer Louisiana E. Everett J. M. Given, Jr. - North Carolina P. Hackford - Utah

R. F.

D. E. Burns -

W. E. Somers K. K. Tam Zick, Jr.

J. H.

-

C. j. Canada P. A. Conklin -

Nebraska Maine Nova Scotia, New Vork

R. j.

J.

Delaware - Oklahoma Pri nce Edward K. Canada D. -Ohio D. J. - Kansas S. Katz - British Columbia, Canada M. Kotb Canada K. T. Lau - Alberta, Canada M. A. Malek - Florida G. F. Mankel Nevada R. Marvin Il - \l\Ioleh,inntn.n l. W. Mault - Manitoba, Canada McEwen B. Harlan

M.

(se R. D. Mile - Ontario, Canada M. F. Massachusetts G. R. - Arkansas Y. - Hawaii W. R. Owens Louisiana T. M. Parks - Texas R. P. Pate Alabama J. D. Payton - Pennsylvania M. R. Peterson - Alaska H. D. Pfaff - South Dakota J. L. Pratt - Missouri D. C. Price - Yukon Territory, Canada

R. S. Pucek - Wisconsin D. E. Ross New Brunswick, Canada N. Surtees - '-::l<:!<::ltrh':'\A1::1,n Canada M. R. Toth - Tennessee \/A,·h::l."An Wisconsin \fl/~,<:h!lnatr.n New Jersey lowa M. - Vermont D. J. Willis - Indiana E. Zarate - Arizona

ON

M. D. Rana, Chair G. M. Eisenberg, Secretary F. L. Brown D. A. Canonico D. C. Cook J. W. Felbaum T. Joseph J. M. Lacy N. L. Newhouse G. B. Rawls, Jr. J. R. Sims, Jr. N. Sirosh J. H. Smith S. Staniszewski T. Tahara D. W. Treadwell E. Upitis C. T. L. Webster H. Barthelemy, Corresponding Member

'''''',.§....,,'' TANKS

R. C. Biel, Corresponding

U. D'Urso, ..,p,'rPT::lrlf D. A. Canonico K. K. Coleman P. D. Edwards J. G. Feldstein J. Hainsworth T. E. Hansen J. S. Hunter C. F. Jeerings J. P. Libbrecht

D. N. French W. E. Somers

J. J. P. C. F. Jeeri ngs G. B. Komora

Examination

(se

I)

T. E. Hansen T. C. McGough R. E. McLaughlin Y.Oishi R. V. Wielgoszinski

J. T. Pillow, Chair J. L. Arnold D. L. Berger S. W. Cameron G. W. Galanes J. Hainsworth

Member Member l>"tMY"''1I'''''

M. Duncan, Corresponding

on Generai Ke«milrerrlents (Se I)

Member

D. R. Frikken, Corresponding Member

L. E. Hayden, Jr., Corresponding Member K. T. Lau, Corresponding Member K. Oyamada, Corresponding Member C. H. Rivkin, Corresponding Member C. San Marchi, Corresponding Member B. Somerday, Corresponding Member

Y. Park P. Williamson Y. Kim,

R. E. McLaughlin, Chair J. Hainsworth, Secretary G. Cook P. D. Edwards T. E. Hansen W. L. Lowry F. Massi

Sutl~:r(miP

B. W. Roberts, Chair J. S. Hunter, Secretary D. A. Canonico K. K. Coleman G. W. Galanes K. L. Hayes

T. C. McGough J. T. Pillow D. Tompkins S. V. Torkildson R. V. Wielgoszinski D.J. Willis

on Materials (Se I) J. F. Henry J. P. Libbrecht J. R. MacKay F. Masuyama J. M. Tanzosh

(se ON

L. B. W.

J. P. Libbrecht J. C. Light B. W. Moore R. D. Schueler, Jr. J. L. Seigle J. P. Swezy, Jr. S. V. Torkildson

P. A. Molvie, Chair G. L. Hiler, Secretary L. Coats

J. Cameron, Corresponding

INTERNATIONAllNTEREST REVIEW GROUP

V. Felix S. H. Leong W. Lin C. Minu

I)

T. E. Hansen, Chair D. L. Berger P. D. Edwards G. W. Galanes W. L. Lowry

(Se I)

W. L. Lowry J. R. MacKay T. C. R. P. A. Molvie Y.Oishi J. T. Pillow R. D. Schueler, Jr. J. P. Swezy, Jr. J. M. Tanzosh R. V. Wielgoszinski D.J. Willis
Recovery T. E. Hansen, Chair E. M. Ortman, Secretary R. W. Anderson J. P. Beli L. R. Douglas J. D. Fishburn G. B. Komora J. P. Libbrecht L. Marriott

R. L. Williams

xxiv

I)

F. Massi T. C. McGough D. Tompkins E. A. Whittle

Generators B. W. Moore A. L. Plumley R. D. Schueler, Jr. J. C. Steverman, Jr. S. R. Timko D. S. V. B. C. A. Turhan

(Se I)

j. F. Chair M. Gold, Vice Chair N. Lobo, Secretary F. Abe D. C. Agarwal W. R. Apblett, jr. A. Appleton M. N. Bressler H. D. Bushfield j. Cameron D. A. Canonico A. Chaudouet P. Fallouey D. W. Gandy M. H. Gilkey j. F. Grubb

C. L. Hoffmann P. A. Larkin F. Masuyama R. K. Nanstad M. L. E. G. D. W. Rahoi B. W. Roberts E. Shapiro R. C. Sutherlin R. W. Swindeman j. M. Tanzosh B. E. Thurgood R. A. Moen, Honorary

C. L. Hoffmann, Chair j. M. Tanzosh, '",,-r"'i';>rl' F. Abe jr. W. R. D. A. Canonico K. K. Coleman P. Fallouey M. Gold j. F. Henry E. L. Hibner

F. Masuyama H. Matsuo H. Murakami D. W. Rahoi B. W. Roberts M. S. Shelton R. W. Swindeman B. E. Thurgood T. P. Vassallo, jr.

j. F. Grubb, Chair D. C. Agarwal H. D. Bushfield

P. Fallouey E. Shapiro

Member D. Kwon, Delegate

Hnnnw'::I!I'V

Members (Se Il)

A. P. Ahrendt T. M. Cullen R. Dirscherl W. D. Doty W. D. Edsall

of Weldments (Se Il &

j. j. Heger G. C. Hsu R. A. Moen C. E. Spaeder, jr. A. W. Zeuthen

~I.U)~rl:)I.lp

on Edemal Pressure

R. W. Mikitka, Chair j. A. A. Morrow, Secretary L. F. Campbell D. S. Griffin j. F. Grubb

R. M. Davison B. M. Dingman M. j. Dosdourian T. Graham j. F. Grubb K. M. Hottle D. S. janikowski

on

Sp(~diicatioins (Se

Int.>l'n~~tin,n::ll1

Materiai

Sp~~cltlcaUolns (Se

D.O.Henry M. Higuchi H. Lorenz A. R. N\lWpnlrlO

H. D. Bushfield D. A. Canonico

jr. R. D. E. A. Steen E. Upitis D. Kwon, L/,--,'--,<;un_

P. A. F. LJarocllev'SKV Sut~2:r()up

D. W. Rahoi, Chair M. Katcher, Secretary D. C. Agarwal W. R. Apblett, jr. H. D. Bushfield L. G. Coffee

W. S. jacobs, Chair j. L. Arnold R. j. Basile j. Cameron H. E. Gordon D. C. Lamb

Il)

Chair A. Chaudouet, Vice Chair j. P. D. C. W. M.

c. W. Rowley,

E. R. C. Sutherlin R. Zawierucha

Chair

F. L. Brown S. R. Frost P. S. Hill

Il &

VIII)

K. Mokhtarian

C. C. Neely T. T. Phillips M. D. Rana D. A. Swanson

E.

M. R. Kessler R. H. Walker j. W. Wegner F. Worth

Il)

A. G. Kireta, jr. j. Kissell P. A. Larkin H. Matsuo j. A. McMaster D. T. Peters

M. H.

(se

Nonmetallic Materiais (Se II)

on Nonferrous

j. F. Grubb E. L. Hibner G. C. Hsu

j. F. Henry D. W. Rahoi B. W. Roberts W. j. Sperko B. E. Thurgood

Sul)!r()I..Ip on TOll~hlless

D. C. Krouse L. j. Lavezzi W. C. Mack j. K. Mahaney A. S. Melilli K. E. Orie E. Upitis R. Zawierucha A. W. Zeuthen

A.

Sul)~rl)uP

&

M. Katcher D. L. Kurle E. Michalopoulos D. Nadel C. H. Sturgeon

ferrous

E. G. Nisbett, Chair Vice Chair

(se

j. M. Tanzosh, Chair W. F. Newell, jr., Secretary K. K. Coleman P. D. Flenner D. W. Gandy K. L. Hayes

IX)

xxv

R. W. Barnes, Chair R. M. jessee, Vice Chair C. A. Sanna, Secretary W. H. Borter M. N. Bressler j. R. Cole E. Cornman, jr. R. P. Deubler B. A. Erler G. M. Foster R. S. Hilllll C. L. Hoffmann C. C. Kim

V. Kostarev D. F. Landers W. C. LaRochelle K. A. E. A. Mayhew W. N. McLean D. K. Morton

R. j. Bosnak E. B. Branch W.D.

F. Drahos R. Moen C. j. Pieper

0.0.

R. F. B. B. Scott j. D. Stevenson K. R. Wichman Y. H. Choi, Delegate

P. G. M. Foster, Chair G. j. Vice Chair D. K. Morton, <';'pr'rpt::lrll W. Borter G. R. Cannell E. L. Farrow R. S. HilllIl D. W. Lewis

T. H. P.

Fun~ "'ar-~t:>rl/

T. M. Adams C. Basavaraju j. Catalano j. R. Cole R. J. Gurdal R. W. Haupt j. Kawahata

"hrl\l;}<:t::ll.l::l

N. M. Simpson R. H. Smith J. D. Stevenson C. j. Temus P. Turula A. D. Watkins

C. G. P. E. McConnel1 l. D. Mclnnes

D. Landers j. F. McCabe J. C. Minichiello

H,"'crr,ha'r.....

R. C.

A. B. Meichler R. E. Nickell E. L. Pleins

A. N. 0.0. R. D. Patel

E. C.

"V\.. Ul...IUU,h'

M. S. Sills G. C. Slagis E. A. Wais c.-I. Wu

R. B. V. Kostarev

Pr(Jlball)i!i!;fic (SG-D) (SC III)

011

(SC III) R. P. Deubler, Chair R. S. Hill III, Vice Chair A. N. Nguyen, Secretary T. M. Adams M. N. Bressler

D. F. Landers K. A. Manoly R. J. Masterson W. N. McLean j. C. Minichiello M. Morishita F. F. Naguib T. Nakamura W. Z. Novak E. L. Pleins I. Saito G. C. Siagis j. D. Stevenson j. P. Tucker K. R. Wichman

C. W. D. L. Caldwell j. R. Cole R. E. Cornman, Jr. A. A. Dermenjian P. Hirschberg R. I. jetter R. B. Keating J. F. Kielb

H. Ori

R. S. Hill III, Chair T. M. Adams

T. B. M.

I. Saito j. R. Stinson

W. P. Golini A. N. Nguyen

c.-I. Wu

I. Saito M. E. Schmidt J. P. Tucker R. M. Wilson

T. A. Bacon A. A. Dermenjian

M. R. D.O.Henry E. V. Imbro

(SC III)

Supports (SG-D)

R. j. Masterson, Chair F. J. Birch, ,ar'rat:>rll U. S. K:>'1i1\1nné.rlh,,"''' P.

S. D. Kulat

A. McNeilll1l P. j. N. A. Palm

R. E. Cornman, Jr., M. D. Eftychiou A. A. Fraser M. Higuchi G. R. jones

III)

Chair

Group

Valves (SG-D) (SC III)

J.

j. P. Tucker, Chair R. R. Brodin G. A. jolly W. N. McLean T. A. McMahon

T. G. D. V.

j. W. Leavitt j. E. Livingston j. R. Rajan A. G. Washburn

S. N. H. R. "nfH'Iprpoopr j. C. Tsacoyeanes R. G. Visalli

III)

J. F.

Kielb, j. T. Land

J. F.

Chair

Grol.lp on Vessels Mullooly F. F. Naguib, G. K. Miller,

Met.hodiOIOl~Y

B. Keating, Chair Anderson, ,a,-rat''''rll M. Adams M. K. Au-Yang R. D. Blevins D. L. Caldwell M. Hartzman

(SG-D)

D. F. Landers W. S. Lapay Lockert j. F. McCabe P. R. Olson j. D. Stevenson j. Yang

E. L. Pleins, Chair T. M. Adams

G.

K,{)rk'n-.",n

W. Lewis Mclnnes j. Minichiello

I.

A. Kalnins R. B. Keating

C. W. Bruny

K.

G. D. Cooper M. Hartzman W. j. Heilker

M. Nakahira R. M. Wilson

D. E.

M::ltthF'\A/<:

(SG-D) (SC III) W. Novak, Chair R. S. Hillill C. L. Hoffmann

H. Ori

Chair ,",pr-rpt",rll

S. Yukawa Y. H. Choi,

&

3 Containmel1lts W. C. LaRochelle, Chair C. A. Lizotte, Secretary

D. K. Morton R. E. N ickell H. P. Shrivastava C. J. Temus P. Turula

A.

An,nlAtnn

j.

W. P. E. A. R.

xxvi

Mclntyre

R. D. Mile M. R. Minick B. B. Scott H. K. Sharma W. K. Sowder D.M. V. Walshe

3C)

Sul)l!r()UD

Ori

Materials, Fal)ri(:ation,

C. L. Hoffmann, Chair G. P. Secretary W. H. Borter D. M. Doyle G. M. Foster G. B. Georgiev R. M. jessee C. C. Kim M. Lau

Pressure S. F. Harrison, jr., Chair E. M. Petrosky

Sullgr()lJp

(SC III)

A. L. Szeglin D. G. Thibault

(SC IV) K. M. MeTague P. A. Molvie

S. V. Voorhees, Chair T. L. Bedeaux K. j. Hoey

Ori

(SC III, IU""""U!"" R. W. Barnes, Chair j. R. Cole, Secretary B. K. Bobo N. Broom B. A. Erler C. M. Faidy j. M. Helmey

2)

Cast Imn Boilers (SC IV)

M. F. Hessheimer R. S. Hilllli E. V. Imbro R. M. jessee R. F. Reedy Y. Urabe

P. A. Larkin W. D. Lemos C. P. MeQuiggan

K. M. MeTague, Chair T. L. Bedeaux j. P. Chieoine j. A. Hall

Sul)gr()up and Review

R. F. Chair W. H. Borter M. N. Bressler D. L. Caldwell

K. M. MeTague B. W. Moore E. A. Nordstrom T. M. Parks j. L. Seigle R. V. WiE~lgo~;zin~;ki F. P. Bartorl, Honorary Member R. B. Duggan, Honorary Member R. H. Weigel, Honorary Member j. I. Woodworth, Honorary Member

P. A. Molvie, Chair S. V. Voorhees, Vice Chair G. Moino, Secretary T. L. Bedeaux D. C. G. Bynog j. Calland j. P. Chieoine C. M. Dove W. L. Haag, jr. j. A. Hall j. D. Hoh D. j. jenkins W. D. Lemos

H. Murakami M. Nakahira C. j. Pieper N. M. W.j. j. R. Stinson K. B. Stuekey A. D. Watkins S. Yukawa

P. A. Larkin, Chair j. A. Hall

III)

R. P. Deubler 8. A. Erler W. C. LaRoehelie j. D. Stevenson

011

Materials (SC IV) W. D. Lemos j. L. Seigle

IV) K. M. MeTague F. j. Sehreiner M. A. Taylor T. E. Trant

W. L. Haag, jr., Chair j. Calland T. D. Gantt W. D. Lemos

Lornpoll1el1lts (SC In) IV) T. D. 8urehell, Chair C. A. Sanna, . . t:>r·,.t:>r;:,,.'1 R. L. Bratton M. W. Davies S. W. Doms

O. Gelineau

E. A. Nordstrom j. L. Seigle R. V. Wielgoszinski

T. L. Bedeaux, Chair j. Calland C. M. Dove W. D. Lemos

M. N. Mitehell N. N. Nemeth T.Oku M. Srinivasan

S. F. ..."'.............~,~,;'i~.'/~ i'TT'=IL O N

NONDESTRUCTIVE EXAMINATION (SC V) 3C) T. C. Inman, Chair A. C. Eberhardt, Vice Chair C. A. Sanna, . . "',-,."'r·;:,,.'1 N. Alchaar T. D. Al-Shawaf j. F. Artuso H. G. Ashar M. B. A. Erler F. Farzam

j. Gutierrez j. K. Harrold M. F. Hessheimer T. E. johnson N.-H. Lee B. 8. Seott R. E. Shewmaker j. D. Stevenson A. Y. C. Wong T. Watson, Liaison Member

j. E. Batey, Chair F. B. Kovaes, Vice Chair S. Vasquez, Secretary S. j. Akrin j. E. Ayeoek A. S. Birks P. L. Brown N. Y. Faransso A. F. G. W. Hembree W. Kruzie J. F. JVlainnlt12 R. D. MeGuire

xxvii

D. R. jr. F. J. Sattler B. H. Clark, jr., Honorary Member H. C. Graber, Honorary Member O. F. Hedden, Honorary Member j. R. MacKay, Honorary Member G. McCarty, Honorary Member

V)

R. D. McGuire, Chair J. E.

U. R. Miller, Chair R. E. Knoblock, çnr'"at",,"

G. W. Hembree J. W. Houf J. R. J. P. Jr.

A. S.

N. Y. Faransso

Examilf1latilm Methods (se V)

A. S. Birks, Chair S. J. Akrin P. L. Brown N. Y. Faransso G. W. Hembree Su!:)@"rlrlUIl

R. W. Kruzic D. Quattlebaum, Jr. F. J. Sattler M. j. Wheel

O.A. R. j. Basile

T. P. Pastor M. D. Rana G. B. Rawls, Jr. S. C. Roberts

M. R. Breach F. L. Brown J. R. Farr J. P. Glaspie C. E. Hinnant W. S. Jacobs M. D. lower R. W. Mikitka K. Mokhtarian

A. Selz S. C. Shah J. C. Sowinski C. H. Sturgeon D. A. Swanson K. K. Tam E. L Thomas, Jr. R. A. Whipple

on Voilulf1rletric Methods (se V)

G. W. Hembree, Chair S. J. Akrin J. E. Aycock J. E. Batey P. L. Brown N. Y. Faransso A. F. Garbolevsky

R. W. Hardy R. A. Kellerhall F. B. Kovacs R. W. Kruzic J. F. Manning F. J. Sattler

C. D.

SUi)2rl)UIl on Fal~ricatil)n

C. D. Chair E. A. Steen, Vice Chair J. L Arnold

F. Campbell H. E. Gordon W. S. Jacobs D. J. Kreft L.

Inspedil[)n (Se VIII)

C. D. lamb

S. lee B. R. Morelock M. J. Pischke M. J. Rice B. F. Sheliey j. P. jr.

j.

Acoustic Emissions (SG~VM) (Se V)

N. Y. Faransso, Chair

J. E. Batey J. F. Manning

J. E. on

R=uilinl[lllr~l!1\lllv (SG~VM)

F. B. Kovacs, Chair S. J. Akrin

(se V)

F. Garbolevsky R.W. G. W. H<>mhr<><> R. W. Kruzic T. L. Plasek A.

J. E. J. E. Batey P. L. Brown N. Y. Faransso

Ultrasonics (SGNM) (se V)

R. W. Kruzic, Chair

R. A. Kellerhall J. F. Manning M. D. Moles F. j. Sattier

J. E. N. Y. Faransso O. F. Hedden ON

T. P. Pastor, Chair K. Mokhtarian, Vice Chair S. J. Rossi, <':Lv-~n'-~~" R. J. Basile J. Cameron D. B. Demichael J. P. M. Gold W. S. Jacobs G. G. Karcher K. T. Lau j. S. Lee R. Mahadeen S. Malone W. Mikitka U. R. Miller

S. C. Roberts, Chair D. B. Demichael, Secretary R. j. Basile j. P. Glaspie K. T. lau M. D. Lower C. C. Neely

D. B. Stewart D. A. Swanson K. K. Tam

Equliplf1rlent (Se VIII)

R. Mahadeen, Chair G. Aurioles, Secretary S. R. Babka j. H. Barbee

M. (se

A. S. Olivares F. L. Richter K. j. Schneider

J. \. Gordon M. j. Holtz E. Jehrio

B. j. Lerch S. Mayeux U. R. Miller T. W. Norton Osweiller R. j. S. Yokell R. P. Zoldak S. M. Caldwell, Honorary Member

C.

D. T. Peters M. J. Pischke M. D. Rana G. B. Rawls, Jr. S. C. Roberts C. D. K. j. Schmeirler A. Selz j. R. Sims, Jr. E. A. Steen K. K. Tam E. Upitis E. L. Thomas, jr., Honorary Member

R. Sims, Jr., Chair S. Vasquez, Secretary L. P. R. C. Biel D. j. Burns P. N. Chaku R. D. Dixon M. E. Dupre D.M. W. Hiller A. M. M. james jansson

j. A. Kapp j.

D. P. Kendall K. Khare M. Mann S. C. Mordre G. j. Mraz E. Perez D. T. Peters E. Roll F. W. Tatar S. Terada

A.

IX)

j. Cameron, Chair

E. E.

W.M. E. G. Nisbett D. W. Rahoi R. C. Sutherlin E. Upitis

J\An,ro<:>,n<:>(Jo

D. C. j.

F.

E. L. Hibner M. Katcher

S. Malone, Chair U. D'Urso, Secretary F. L. Brown

D. A. Sowers, Chair V. A. Beli L. P. Connor R. S. Corbit P. R. Evans P. D. Flenner j. M. Given, jr.

SutlP"l'llUIl 01'1

M. R. Minick E. Soltow A. A. Stupica

Pi"Jfli"3"lr'liu'3"

D. A. Sowers, Chair M. j. Rice, Secretary M. Bernasek R. K. Brown, jr. A. S. Olivares S. D. Reynolds, jr.

S. Vasquez, Secretary

Task

K. L. Hayes j. S. Lee W.M. R. D. McGuire M. B. Sims G. W. Spohn II!

Qualification (SC IX)

M. B. Sims W. j. Sperko S. A. Sprague j. P. jr. P. L. Van Fosson T. C. Wiesner

Vessels (SC VIU)

R. E. Nickell, Chair G. A. Antaki D. D. Barker R. C. Biel D. W. Bowman D. L. Caldwell A. M. Clayton

j. E. Didlake, jr. T. A. R. Forgan B. L. Haroldsen H. L. Heaton E. A. Rodriguez j. R. Sims, jr.

Honorary

(SC IX)

W. K. Scattergood

(SC X)

SUBCOMMITTEE ON WElDlNG (SC IX) j. G. Feldstein, Chair W. J. Sperko, Vice Chair j. D. Wendler, Secretary D. A. Bowers R. K. Brown, jr. M. L. Carpenter L. P. Connor P. D. Flenner j. M. Given, jr. j. S. Lee W. M. Lundy

D. Eisberg, Chair P. j. Conlisk, Vice Chair S. Vasquez, Secretary F. L. Brown J. L. Bustillos W. Cowley T. j. Fowler D. H. Hodgkinson L. E. Hunt D. L. Keeler B. M. Linnemann

R. D. McGuire S. R. Newmark A. S. Olivares M. j. Pischke S. D. jr. M. J. Rice M. B. Sims G. W. Spohn III M. J. Stanko P. L. Van Fosson R. R. Young IX)

M. j. Pischke, Chair E. W. Beckman

L. F.

'--
NUClEAR

A. F. C. F. j. P. Swezy, jr.

R. Newmark, Chair P. R. Evans R. M. jessee A. S. Olivares SUI)~rl[mD 01'1

M.

Chair

H. S. Porter P. L. Sturgill K. R. Willens

Materials

IX)

T. Melfi

j. L.

S. D.

M. Bernasek L. Connor R. M. Jessee C. C. Kim

C. E. Sainz W.j. M. j. Stanko R. R. Young

SUBCOMMITTEE ON INSPECTION

G. C. Park, Chair R. W. Swayne, Vice Chair R. L. Crane, Secretary W. H. Bamford, jr. R. C. D. D. Davis R. L. E. L. Farrow R. E. Gimple F. E. Gregor K. Hasegawa D.O.Henry R. D. Kerr S. D. Kulat G.L. D. W. Lamond

M. L. Carpenter

jr.

j.

T. R. Newton

xxix

j. C. Murphy D. j. Painter D. j. Pinell G. Ramirez J. R. Richter j. A. Roiston B. F. Shelley F. W. Van Name D. O. Yancey, jr. P. H. Ziehl

XI)

W. E. Norris K. W. R. Rogers III D. A. Scarth j. Schaaf, jr. jr. j. C. j. E. G. L. Stevens E. W. Throckmorton III D. E. Waskey R. A. West C. j. Wirtz C. S. Withers R. A. Yonekawa K. K. Yoon T. Yuhara Y.-S.

(se

XI)

Chair

R. W.

K.

W. H. Bamford, Jr. D. D. Davis R. L. Dyle R. E. Gimple F. E. Gregor

F. J. jr. j. C Spanner, Jr. E. W. Throckmorton III R. A. Yonekawa

Honorary Members (Se XI) J. P. Houstrup L. R. Katz P. C Riccardella

L. J. Chockie

C D. Cowfer O. F. Hedden

SUll2:rlrmn on Evaluation Standards W. H. Bamford, Jr., Chair G. L. Stevens, 'DE'YDI'''Y'' R. C Cipolla S. Coffin G. H. De Boo B. R. Ganta T. J. Griesbach K. Hasegawa D. N. Hopkins Y.lmamura

P. H. D. N. Y.lmamura K. Koyama D. R. Lee H. S. Mehta

K. Kashima H. S. Mehta

K. Mi\i'aza.ki J. S. Panesar P. J. Rush K. K. Yoon V. A. Zilberstein

Chair

C G.

XI)

XI)

W. L. Chase

Sul)2rl[)UD on Nondestructive Ex'lmina1:ion (SC XI)

K. Koyama D. R. Lee H. S. Mehta J. G. Merkle S. Ranganath D. A. Scarth K. R. Wichman K. K. Yoon Y.-S. Chang, Delegate

j. C Spanner, jr., Chair G. A. Lofthus, (.:""'YL"d'..,y,.

D. O. M. R. Hum

N. R.

G. L.

T. L. Chan C B. Cheezem D. R. Cordes F. j. Dodd F. E. Dohmen M. E. Gothard

j. T. G. R. Perkins A. S. Reed F. j. Schaaf, jr. C J. Wirtz

on Personnel QUlali1fic.ltioln and Surface, Current (SG=NDE) (SC XI) R. Cordes,

j. G. Merkle M. A. Mitchell K. Miyazaki R. K. Qashu S. Ranganath P. j. Rush D. A. Scarth T. S. Schurman W. L. Server F. A. Simonen K. R. Wichman M. Wilkowski K. K. Yoon S. Yukawa V. A. Zilberstein

,,,,r'yat"YlI

R.

jr.

A. S. Reed

B. L. Curtis N. Farenbaugh G. B. Georgiev

D. Spake j. C Spanner, jr. C j. Wirtz

D.O. j. T.

on D. W. Lamond, Chair j. M. ~ollghrnan j. j. G. Fechter K. W. Hall

(se T. J. Griesbach, Chair K. R. Baker W. H. Bamford, Jr. H. Behnke B. A. T. L. Dickson S. R. Gosselin S. N. Malik H. S. Mehta

1-l"':Da:lUf"

P. H. D. N.

(se

on flaw Evaluation (SG=ES) (Se XI) R. C Cipolla, Chair G. H. De Boo, Secretary W. H. Bamford, Jr. M. Basol J. M. Bloom B. R. Ganta T. J. Griesbach H. L. Gustin F. D. Hayes

K.

D. A. Scarth, Chair G. M. Wilkowski, T. A. Bacon W. H. Bamford, Jr. R. C Cipolla N. G. Cofie S. K. Daftuar G. H. De Boo E. Friedman B. R. Ganta L. F. Goyette

O. F. Hedden C G. McCargar W. E. Norris

G. C Vice Chair R. L. Crane, Secretary

XI)

XI)

R. Hall j. K. McClanahan A. McNeill1ll L. 1\A".ntrr"...... or\l E. j. Sullivan, jr.

on Procedlure Qualifica1:ion

R. Pace S. Ranganath W. L. Server

M. E. Gothard, Chair G. R. Perkins, <';""'yol'"y,, C Cheezem A. D. Chockie S. R. Doctor F. J. Dodd F. E. Dohmen K. j.

E. A. F. A. Simonen G. L. Stevens D. P. Weakland K. K. Yoon

xxx

R. Kellerhall D. Kurek G.L.

G. A. CE.

S. A. R. V. Swain

R. A. Yonekawa, Chair E. V. Farrell, jr., "Dr-rDt"lr\/ S. B. Brown R. E. Cantrell P. D. Fisher E. B. Gerlaeh R. E. Gimple D. R. Graham R. A. Hermann E. V. 1mbro

R. D. Kerr S. L. MeCraeken B. R. Newton j. E. O'Sullivan W. R. III R. R. Stevenson R. W. Swayne D. E. Waskey j. G. Weicks C. S. Withers Programs (SG=RRA) (Se XI)

E. B. Gerlaeh, Chair S. B. Brown, Secretary A. V. Du Bouehet G. G. Elder E. V. Farrell, jr. S. K. Fisher j. M. Gamber

D. R. Graham G. F. Harttraft R. R. Stevenson R. W. Swayne A. H. Taufique T. P. Vassallo, Jr. R. A. Yonekawa

D. E. Waskey, Chair R. E. Cantrell, Secretary S. j. Findlan P. D. Fisher K. A. Gruss M. L. Hall R. A. Hermann R. P. Indap

K. B. Thomas, Chair D. Song, Secretary V. L. Armentrout G. L. Belew C. H.Q.Do R. Fougerousse M. R. Hum

(Se XI)

R. D. Kerr M. Lau S. L. MeCraeken B. R. Newton j. E. O'Sullivan j. G. Weieks K. R. Willens

E. W. Throekmorton III, Chair j. M. Agold, "Dr'rDt"lrl/ G. L. Belew j. M. Boughman D. D. Davis H. Q. Do j. D. Ellis E. L. Farrow M. j. Ferlisi O. F. Hedden M. L. Herrera

D. R. R. L. Turner, "Dr'rDt"lr\/ W. H. Bamford, jr. j.M.

A. D. K. G. Y.

E. L. Farrow R. K. Mattu S. R. Seott C. S. Withers

(se XI)

(SG~WeS)

Review (se XI)

on

S. D. Kulat D. W. Lamond A. MeNeilllll W. E. Norris D. Song j. E. Staffiera H. M. Stephens, jr. K. B. Thomas R. A. West G. E. Whitman H. L. Graves III, Alternate

on ISI Opitimiization

E. A.

Req!uiremel1lts (se XI)

K. Rhyne, Chair E. j. Maloney, Secretary T. L. Chan j. D. Ellis

R. W. Swayne, Chair C. E. Moyer

j. E. Staffiera C. j. Wirtz

Extension (se XI)

T. A. Meyer, Chair D. V. Burgess, Secretary D. D. Davis F. E. Gregor

P.-T. Kuo R. L. Turner G. G. Young

Readol's (se XI) j. Fleteher,

H. T. Hill R. D. C. N. D. Naus S. C. ~",titGl,lIt H.M. jr. W. E. Norris, Alternate

H. Ashar S. G. Brown K. K. N. Chao R. C. Cox j. W. Crider M. j. Ferlisi H. L. Graves III

S. D. Kulat D. G. Naujoek T. Nomura C. M. Ross R. L. Turner R. A. West G. E. Whitman

011

LOl1lt'lIil1lmelllt (SG=wes)

Chair

Systems (Se XI)

C. C. Kim

Water~eooled

j. E. Staffiera,

K. W. Hall D. W. Lamond j. T. R. K. Mattu P. j. O'Regan N. A. Palm M. A. Pyne F. A. Simonen R. A. West j. C. Younger A. T. Keim, Alternate

(SG~wes)

011 (SG~RRA)

S. D. Kulat, Chair A. MeNeill III, Secretary j.M. S. A. B. A. Bishop S. T. Chesworth C. Cueto-Felgueroso H.Q.Do R. Fougerousse M. R. Graybeal j. Hakii

Chair

M. A. Loekwood, Secretary N. Broom K. N. W. A. O.

B. j. Kruse M. N. Mitchell F. j. Sehaaf, jr. R. W. Swayne

sUBeOMMITTEE ON TRANSPORT TANKS

A. Selz, Chair L. Plano, Secretary P. D. Stumpf, Secretary A. N. Antoniou C. Beeht IV M. L. Coats M. A. Garrett C. H. Hochman G. G. Kareher

XI)

H. Mahindrakar G.

B. Thomas E. Whitman

xxxi

G. McRae M. R. Miniek M. D. Pham M. D. Rana S. Staniszewski M. R. Toth A. S. V. \/rH,rn""",ç,

XII)

01'1 M. D. Rana, Chair G. G. Karcher S. L. McWilliams N. j. Paulick M. D. Pham

R. j. Basile, Chair R. W. Barnes M. R. Breach R. P. Deubler G. G. Graven G. L. Hollinger R. I. jetter

T. A. A. P. \/::llrahp>c:.p> M. R. E. A. Whittle

D. P. jones R. W. Mikitka U. R. Miller W. j. O'Donnell R. D. Schueler, jr. A. Selz

XII)

S. V. Voorhees, Chair j. A. Byers B. L. Gehl L. D. Holsinger

D. j. Kreft G. McRae M. R. Minick A. S. Olivares

C. H. Hochman, Chair T. W. Alexander D. M. Allbritten C. A. Betts j. F. Cannon j. L. Freiler W. L. Garfield

G. L. Hollinger, Chair S. A. Adams M. R. Breach R. G. Brown R. j. Gurdal C. F. Heberling Il C. E. Hinnant

P.

M. A. Garrett K. L. Gilmore j. L. Rademacher T. Rummel M. R. Toth

D. P. jones A. Kalnins W. j. Koves

01'1

ANO

ACCREDITATION (SCQBPVA) W. C. LaRochelle, Chair P. D. Edwards, Vice Chair K. I. Baron, "'Pf'r'pr2r'1I

M. B. P. Hackford K. T. Lau L. E. McDonald K. M. B. R. Morelock j. D. D. E. Tanner

c. D. E. Tuttle E. A. Whittle Bynog, Alternate

M. A. DeVries, Alternate C. E. Ford, Alternate T. E. Hansen, Alternate G. L. Alternate D. j. jenkins, Alternate B. B. MacDonald, Alternate R. D. Mile, Alternate G. P. Milley, Alternate T. W. Norton, Alternate H. R. Staehr, Alternate j. A. West, Alternate

V.

\/\/ielg.os;~in:;ki,

f~lfiprrlrirp

O. E. Trapp, Senior Consultant A. j. Spencer, Honorary

T. C.

IV j. F. Cervenka D. S. Griffin B. F. Hantz M. H. jawad W. j. Koves

S.

D. H. G. Sannazzaro T. G. Seipp D. A. Swanson G. Taxacher E. L. Thomas, jr.

R. A.

W. j. O'Donnell, Chair S. A. Adams P. R. Donavin J. Gurdal

C. F.

Hp!')P>r!iina

A1ember

(SCQNA) Stevenson, Chair W. C. LaRochelle, Vice Chair j. Pang, "Pf'"pt::lrll M. N. Bressler S. M. Goodwin K. A. Huber M. Kotb j. C. Krane C. A. Lizotte

D. E. Tanner

D. M. G. Bynog, G. Alternate P. D. Alternate j. W. Alternate K. M. Hottle, Alternate B. G. Kovarik, Alternate P. F. Prescott, Alternate S. Toledo, Alternate E. A. Whittle, Alternate R. V. Alternate L. Wiger, Alternate O. E. Senior Consultant MoI/f-'rfl;.Jff-'

T. E. McGreevy K. A. Moore W. j. O'Donneli D. A. Osage j. S. Porowski B. Riou T.-L. Sham M. S. Shelton R. W. Swindeman

D. L. Marriott

P. Hsu

Prasse Quaka A. T. Roberts

W. D. Reinhardt

L. R. I. jetter, Chair

R. P. M. R.

K. Matsunaga

G. A. Miller

D. P. jones G. Kharshafdjian

S. T. Nakamura

D. H. G. Taxacher H. H. Ziada

M. R. Breach, Chair R. W. Mikitka, "'Df'/"Dr::>/"II G. G. Graven V. T. I-lwang j. C. R. B. Luney

j. Madden D. R. Palmer A. Pfeifer M. D. Rana

R. W. Mikitka, Chair G. Bibel H. A. Bouzid A. Chaudouet

j. R.

S. N. Pagay

xxxii

P. G.

~rrlP>d{prrn::lr)n

R. W. Schneider R. D. Schueler, jr. A. Selz M. S. Shelton

S. F. Harrison, jr., Chair j. A. West, Vice Chair S. j. Rossi, Secretary j. F. Bali S. Cammeresi A. Cox R. D. Danzy D. B. Demichael R. j. Doelling

j. P. Glaspie H. L W. F. Hart C. A. Neumann T. M. Parks D. K. Parrish D. j. Scallan j. C. Standfast Z.

on

j. A. West, Chair C. E. Beair R. D. Danzy R. j. Doelling

D. B. Demichael, Chair j. F. Bali G. Brazier j. P. C. A. Neumann

T. M. Parks D. K. Parrish j.W. j.W. j. C. Standfast on

A. Cox, Chair

(SC~SVR)

S. Cammeresi G. D. Goodson

W. F. Hart K. G. Roth D. j. Scallan Z. Wang

T. j. Bevilacqua, Chair S. j. Rossi, Secretary S. F. Harrison, jr.

Y.-S. Lai D. Miller j. A. West

j. E. Brit1

(SC-SVR) H. L D. Miller T. Patel T. R.

xxxiv

SUMMARY The 2007 Edition of this Code has been revised in its This as described in the l-"I"O\A/,"l"n becomes six months after the date of 2007 Edition. To invoke this revision before the use the 112007 Editionl/ in documentation by this Code. lf you choose use the designation 112004 Edition through the 2006 not to invoke this revision before the Addenda ll in documentation

NOTE: Volume 57 of the !nt'''l"nl"oto>tif"\nc to Section VIII-2 of the ASME Boiler and Pressure Vessel Code follows the last page of this Edition.

xxxv

xxxvi

1

nl"i''Il~ni'''~·.;'''n

Overview

1-3 for This Division the of this Division

IIl"annc.df"lte-

Classifications ·i"'lnt"lhin~ti,..","l Units

. . 1 1

The Introduction 11-

'''''''''''

Code Revisions or Additions Code ,hnt".itt""le-

Introduction Definition of

1-1 1-10 1-1 1 1 1-11

1 3 -13

this division and eSltablist1es

of the

aOIJlic:able materia! curves

VA~;SAIS

f) .. ",,,,,,,,,,.., ... '1-,..

i)

in this

1

" ' ' ' ' , ' " ....... '''''''

and

the examination

1

movement of oel:WE!en work sites or

shall

1)

which steam

of Section I or Section

first circumferential

1)

screwed connections. connections. to this construction rl'::llcf'rlh;::~rl on the vessel nr'!:Jl\B\lIFln tl!U'''''1o.rl

nrnnorlu

c) rloc~lnr"\orl

Sections.

to rules that

ae'/ICE~S

that serve such purposes that pressure

f)

1) other

or

when none

inrl'1I'o.,"'t

(1 ",n..,''U'1f\rH''l

0110"""0""'1''''

150 mm

i)

j)

1

1

c)

with limitation on shall not 03

Pressure ve~)sels covered in

111'0"'1'\00'\1''''

for

vessels

human occupancy

the

such ASME/ANSI ..'l''''''l9Irt,,,,, ..,,,,.. pressure vessel CICC\l\/l"'lcr'c

in this

1 IU"Oi"'l"\lO,nTC'

certification

SI or of this edition overpressure

prc)tel~tlcln

b)

than ofthat units and

rll'H',~rcfint

li"'l"\I~~nt,~tir.n

c)

units. When executed variables cvr'\rc,~c~.rI in other units shall converted to result from execution of

1)

Conversion

in the tables fraction and do not

!ctf'\i"'l"\I'!:II"\I

in units or SI

Ih ..... itt~1

of

Vessel

1)

1)

to

inf",nl"r.nl"~:lltlr\,n

c)

1)

n.II"Of"TIH

into the

c)

1"0"""'''>1141 and

revision or addition.

or

1

Definitions

l"ol~::Iltinln

words such as shall understood to mean that the rules of this Division and aPlolic:able Manufacturer's Data reSiPorlsibmtlE~S of to

nor...d"\I"n'\

to

SOE~CItIC

and/or has such review Such words

InSiPe(~tOr

administrative

administrative functions on its and examinations of "5iIr>i'~nl",'i"5il"'r>o with the

that intersect the shell or

J urisdictional

eglJialUOrls aioollcable to

in this of SI or !:Ilnf'\th&:::lfi" the units construction. nrrr·,,,,,u;,;,n

roc·n,.,.nCR'hI1i1tH

c)

i)

"" ....",""1',,,,,..,""'\1 information

that

cubie

both

converted

j)

k)

I)

1

5.5%

-0.8% 2.6%

0.3% .0%

1

Size

~.

'

1 1 ·1/8 1 ·1/4 1-1/2 2 2..1/4 2..1/2 3 3-1/2 4 4-1/2 5 6 8 12 18 20 24 36 40 54 60 72

.•.

Size

mm

25 29 32 38 50 57 64 75 89 100 114 125 150 200 300 450 500 600 900 1000 1350 1500 1800

1/8

NPS 3/8

NPS 1

NPS46 NPS48

NPS 60

.........................................................................................................................2-38 ..................................................................................................................................2-40

of the user on pressure vessel to be constructed contain sufficient to with Division. It is the userls roc'nnncll"\lll'tu Addenda to be used construction.

rQ~nnln~llnlll1tu

~rv~"", ...'i~r'''''''''''

include but not

User's

ne(~eS~SanIIV

be limited to the

Installation Site Location Jurisdictional

if apl:>lIc:aOlle

Environmental conditions i)

relevant factors

Wind

ii) Snow loads Lowest

location

Identification number

identification

wind

exposure,

TnllnUD'II"'In

c)

in 1nO,,.,,,,!",,,,,,,,, Conditions

transient f) 1)

and the based

tl"\l1l"\\u.nn

i)

ii)

/"'1"\1/""I"\.".,l"\n

and/or

",,.,.,,.,,.,/"',n

allO\Jvarlce

criteria.

i}

1}

i}

units

installation This

1)

documented in the User's pressure relief

i)

ii}

user shall

what additional restricted

f"heHYIl,~tn.1

treatments

nondestructive examinations c)

1) is

Position of

1.

The

for ali technical processo

..oe·n"" ... ",'hlo

1A1I~.,a~ij~le

Selection

"""""+"",,..,,,,1

substitutions

the

....,."'''''''''''''' a Manufacturer's Final as-built

r'l ..

that includes:

",u,,,..,,,,,,,,

actual material

",,,,,,,~,,,iifi,,,,,,'~i,,,,,,,,<,

used for each ",,,,,,,.,,.,""""n,,.,.nìl" est:ablllsn that as shown on the rI""'''u",',,,,,,,," conditions that been <'"".",,,,'f'i,,,,rI

c)

1)

Documentation of

",,,,,rVilnl,o,,,"

calculations

i) ii)

in

calculation results

x)

cf

c) the Manufacturer rOC"nnne-ihili'hl

and control is

rOT~~.n.e'rl

~f"'r"'nrr!llnn

to Section IX to

nQri'nrlrrl

the Manufacturer.

examination

.rnl""v::u-,,,,,,o,,,

in

obtain

the

of

roriifit"'.::l1·o

CH(~TOi'Tl

Inspec:tor shall

the Manufacturer's

of is in maintain the and the reconciliation

shall

to

the User's

shown in

to

c)

f)

enforcement c)

ali

included in

Manufacturer's c)

The instructions in Manufacturer's

indicate

Name and address of Manufacturer Name address purchaser. Name of user, and address where vessel is to be installed. Name and address of Manufacturer who will use the vessel part in making the complete vessel Type of vessel, such horizontal or vertical, tank, separator, heat exchanger, reactor. Brief description of part (Le., shell, two-piece head, tube, bundle). An

x

x x

10

14

x

x

15

x

16

Manufacturer's serial number marked on the vessel (or vessei

Annex

Applicable Jurisdiction Registration No. Indicate numbers, including revision numbers, which cover generai assembly and list materials. For registration, number of the drawing appraved by the applicable jurisdictional authority. Organization that prepared drawing. Where National Board Number fram Manufacturer's Series of National Board Numbers. Board Number shall not be used for owner-inspected vessels date of Section VIII, Division and Addenda under which vessel was manufactured Ali code case numbers when the vessel is manufactured to any Cases. To be completed when one or more of the vessel are furnished by others and certified on Data Form required Annex The part manufacturer's name and serial number indicated. of the actual material used in the Show the ASME Spl3cificajtion "SA-285 C"). vessel is to ::;p~3cìfìcaitìon may

of vessel in the test that do not 8 for

Show hydrostatic or other tests made with specified test IJ! !:ì';:O;::' 1.1 I 1::1 position. Cross out words (pneumatic, hydrostatic, or f'1"'Ir'nhin::llrinn Indicate if vessel requirements for combination units

x

x

33

x x x

x x x x

34

Indicate nozzle or other opening that is designated for pressure relief.

35

Show other nozzles and openings by size and type (see 50)

36

Show opening designated

x x

37

Indicate

inspection. Show location.

for support of the vessel and any attachments for superimposed

x

38

Indicate whether fatigue analysis is required per Part 4.

x

39

Describe contents

service of the vessel.

x

x

40

for additional comments, including Code restrictions on the vessei or unusual requirements that have been met, as those noted in ,22, 31, 33, or in Part 1, paragraphs 1.2.1 and 1.2.2, or Part 5, paragraph 5.10. Indicate stiffening rings, if used.

x

x

41

Certificate of block is to show the name the Manufacturer shown on his of Authorization. This should be in accordance with ASME Code organizational authority defined in the Quality ControI System (see

x

x

42

This certificate is to be by the Manufacturer to show the dispol:iitic)n of the User's Specification and the Report, and to the individuals who 2, paragraphs and respectively (see 49). them per This certificate is to be completed by the Manufacturer and signed by the Authorized Inspector who performs the shop inspection.

x

x

x

x

44

National Board Commission Number must shown when the vessel is Board." Otherwise, show only his state or province Commission Number.

"i\I"tinn<>1

to sign for any field construction or ::1<::~:Arrlhl\l Number requirements). indicate the method

45

This certificate is for the Authorized work (see 44 for National Board to pressure test the vessel.

46

Fili in information identical to that shown on the Data supplementary.

47

Fili in information for which there was insufficient for a specific item on the Data Form as identified by the notation "See attached A-3" on the Data Identify information by the applicable Report Item Number.

48

Indicate data, if known.

49

x

This

50

Registration Locale. Data entries with descriptions to Inspector. Abbreviations, coded identification, or reference to Code Figure and number be used to define name. For Flange facing and to is ASME 816.5 f1anges, the class should be not required. Some typical abbreviations are shown below Flanged fabricated nozzle: CI. 300 flg Long weld neck

CI. 300 Iwn

Weid class designation

A

Letter symbols indicate instructions that the instructions of The A3L is not available as shown. It is intended as an example of construction. It is intended that the Manufacturer reporting data far vessel of provide supplementary data describes his vessel.

c

Note the

D

Applies only when heads are of layered construction.

for to

performed (RT, PT, MT, UT).

Indicates if seamless or welded. When more than one layer thickness is used, add lines

needed.

Indicate diameter of vent holes in the layers. Indicate whether vent holes are in random locations in each layer, or are drilled through ali layers.

J

Indicate locations of nozzles and openings; layered shell; layered head. Indicate method of attachment and reinforcement of nozzles and openings in layered shells and layered heads. Refer to figure number if applicable.

1.

Manufactured and certified by (Name and address of manufaclurer) IVIi::lIlUIi::l\jI.U1t::U

for (Name and address of purchaser)

3.

installation

3 (Name and address)

4.

Type

5 Horiz. or ver!o tank

5.

The chemical and physical proper!ies of ali construction, and workmanship conform lo

6.

Shell

7

8

9

11

Mfr.'s Serial No.

CRN

Drawing No.

Nal'!. Bd. No.

Year buìlt

meel the requirements of material specifications of the ASME BOILER AND PRESSURE VESSEL CODE. The design, Code, Seclion VIII, Division 2.

ta

7.

15

16

17

18

19

Material (Spec. No., Grade)

Nom. thk.

Corr. allow.

diameter

Length (overall)

Seams

20

21

24

Longitudinal

Heat treatment

Nondestructive Examination

23

21

24

25

Gir!h

Heat treatment

Nondestructive Examination

No. of Courses

8.

Heads: (a) Matl.

9.

If removable, bolts used (describe other fastenings):

27 Matl. Spec. No. Grade Size Number

10. Jacket closure _---::=--__::_----2-c8-~,__

- - - - l f bar, give dimensions

----------

Describe as ogee and weld, bar. etc 11.

30 Min. design metal tempo __3_2_ _ at __3_2_ (external) At test temperature of ._ _:...-.3::..1:...-. _ 33

MAWP Impact test Hydro., pneu.,

13 12. Tubesheets

15

16

17

Diam. (Subject to pressure)

Nom. thk.

Corr. Allow.

16

17

(Diam.)

Nom. thk.

Corr. Allow.

Attach. (wid., bolted)

Number

Type (straight or IIU")

15 13. Tubes

If bolted, describe or sketch.

Attach. (wid., bolted)

15 Mati. (Spac. No.. Grade)

0.0.

NOlll.

thk.

19 Length (overall)

diameter

15.

20 Heat treatment

Radiographic treatment

Radiographic treatment

No. of Courses

Longitudinal

21 Gir!h

Heat treatment

Matl.

17. ~removab~,bo~sused~escribeo~erfu~enings~

~

~-,____::_

=_____::-,__----------~

Matl. Spec. No. Grade Size Number

18.

Min. design metaI tempo terrlpel'ature of

This Form (E001121) may be obtained fram ASME, arder Dept..

Law Drive.

2300, Fairfield. NJ 07007-2300

__3_2_ _ at __3_2_ 31

2007 Items below to be

19. Nozz!es inspection and safety valve openings PU! No Diam. or Size (!n!et, Out!et, Drain, etc) 34,35,36

20. Support Skirt

VIII - D!V!S!ON FORM A-1 (Back)

ali vessels where

-:-:Ye-s-30-7r7N:-o-LU9S

21. Service: Fatigue analysis required

35

Type

35,50

Material

15,51

Nom. Thk.

Reinforcement Material

- - 7:-- No

No.

38

Location

36

16,52

Other

_--:-:_ _Legs

How Attached

AUached ----:D=-e-s-cr7.- - - ib e

Where and how

39 Describe contents or service

or

Remarks:

21,22,24,31,33,37,40,47

43

Vesse! made by I, the undersigned ,hOJdii~av8iiCfC(;rru~~~~;(f~ or Province of r-.and employed by of --J , have inspected the pressure vessel described in on , and state that, to the best of my knowledge and belief, the Manufacturer has constructed this pressure vessel in accordance with ASME Code, Section this certificate neither the nor his makes warranty, or implied, concerning the pressure VIII, Division 2. be liab!e in any manner for any personal vessel described Data neither nor employer or property damage or a !oss of kind from or connected with this in<:nA/~tinln 43 Authorized Inspector

construction of ali parts of this vessel conforms with the requirements of CODE. "U2" Certificate of Authorization No expires ---CC::-Date Signed o-.-na-m-e-------Assembler that certified and constructed field assembly

VIII, Division

of the ASME

Representative

45

I, the undersigned, holding

valid commission issued by the National Board of Boiler and Pressure Vesse! Inspectors and/or the State or Province of and emp!oyed by of .,.,---;_ _--:--; have compared the statements in this and state that parts referred to as data items

I-

---j

knowledge and be!ief, the Manufacturer has not included in the certificate of shop inspection, have been me and that, to the best of the constructed and assembled this vesse! in accordance Code, Section VIII, Division and subjected to hydrostatic test of. The described vessel was ·antv.-exoo;SS:edor~iDTIed~Or1i;eriliriQi:hepress ure vessel described in this certificate neither the !nspector nor his any personal injury or property Data Furthermore, neither damage or a loss of any fram or connected with Date Nat'!. Board (inel. Endorsements), State, Provo and No.

1.

Manufactured

by

Manufactured far 3.

Location of installation

4.

Type

5 Horiz. or vert. tank

6.

The chemical and physical properties of ali construction, and workmanship conform to 12 Year Constructed to:

7.

Shell

8.

Seams

5.

7

8

9

Mfr.'s Serial No.

CRN

Drawing No.

11 Nat'l.. Bd. No.

Year built

meet the requirements of material specifications of the ASME BOILER ANO PRESSURE VESSEL CODE. The design, Code, Section VIII, Division 2.

io 15 Material (Spec. No., Grade)

24

21 Heat treatment 24 Radiographic treatment

No. of Courses

Heads: (a) Matl.

10. If removable, bolts used (describe other fastenings):

27 Matl. Spec. No. Grade Size Number

11. Jacket closure _--::---:':' 2....,8_.,..,..-.,.--__:----lf bar, give dimensions Describe as ogee and weld, bar. etc

12.

MAWP

13. Tubesheets

15

to

31

16 Nom. thk.

17 Corro Allow.

Attach. (wid., bolted)

(Diam. )

16 Nom. thk.

17 Corr. Allow.

Attach. (wid., bolted)

15 incl.

15. Shell

18 diameter

Corr. allow. 16. Seams

20 Longitudinal

Girth

Heat treatment

17. Heads: (a) Matl.

at test tempo of

Radiographic treatmant

Radiographic treatment

No. of Courses

Matl.

29

tempo

__:___.,.~-~-~___.,.~-~___.,.----Matl. Spac. No. Grade Size Numbar 30

31

Charpy impact_ _-.,.-_3_1 metal tempo

hydro., or comb. pressure test 14) may

19 Length (overall)

21 Heat treatment

~remo~~e,~~~~~e~~eclh~fu~ooi~s~

19. Design presso

This

__3_2_ _ at __3_2_

18 Diam. (Subject to pressure)

15

14. Tubes

_ _ _ _ _ _ _ _ _ If bolted, describe or sketch.

30 Min. design metal tempo (external) At test temperature of 33

30 (internai)

Impact test Hydro., pneu.,

18.

19 Length (overall)

18 diameter

17 Corr. allow.

20 Longitudinal 21 Heat treatment

23 Girth

9.

16 Nom. thk.

obtained fram ASME,

_ Dept..

Drive.

2300, Fairfield. NJ

_

~

2007

VIII FORM

ltems below to be

DIVISION 2

(Back)

ali vessels where

20. Nozzles inspection a1d safet\ valve openinçls Purpose No IDiam or Size Type (Inlet, Outlet, Drain, etc) 34

35

35

Material

Nom. Thk.

35

15

16

50

51

52

Material How Attached

-'''''"

Location

36

36 48

21. Support Skirt _:-:--_37--:-:-_Lugs Ves or No

_-,,-,_ _ Legs No.

---,-,---

Other

No

Remarks:

Attached ---::::---::----

Describe

Where and how

21,22,24,31,33,37,40,47

41 We that the statements in this the Code for Pressure Vessels, "U2" Certificate of Authorization No Date

---------

are correct and that ali details of design, materiaI, construction, and workmanship of this vessel conforms to VIII, Division 2. 41 expires 41 41 Co. name Manllfactllrer

AlIthorized Inspector

Representative

1.

Manufactured and certified by

2.

Manufactured for

3.

Location of installation

4.

Type

5 Horiz. or vert. tank

7 Mfr.'s Serial No.

8 CRN

9

11

Drawing No.

Nat'!.. Bd. No.

This form (E00119) may be obtained fram the ASME, Order Dept., 22 Law Drive, Box 2300, Fairfield, NJ 07007-2300.

Year built

1.

Manufactured and certifted by

2.

Manufactured for

3.

Location cf installation

4.

Type

5 Horiz. or ver!o tank

Daim Hole

7

8

9

11

Mfr.'s Serial No.

CRN

Drawing No.

Nat'!. Bd. No.

Staggered Layers Or Radiai Thraugh

(a) Layered Shell (b) Layered Head

H

G

Item 24 (Remarks)

B

This form (E00119) may be obtained fram the ASME, Order Dept., 22 Law Drive, Box 2300, Fairfield, NJ 07007-2300.

Year built

wriUen Manufacturerls processes. the or information learned about wiii ali

Division 1.

the

shall

as

shall include

to

the Manufacturer's

c)

f"ì"\li"\f"irlolnt

MAWP

accordance with

built.

f)

ali

included.

the aPl=IIlCélble

1)

i)

follows: been

when t"r.It'V'IInlo'l'O

vessel

c)

Manufacturer's

.d and

.e

not

1)

C''I",",l'YIr,or!

with low stress Manufacturer in

ii) ...""n,,,",,,!:>.

of

am.i-WBIU

i)

ii)

far

• •

cantaur

N/mm (8

width

Minimum

1)

may

il.

an

Insoel~tIC~n

!:l\''''II''OOflY'lon'l'

with

c)

the apPllcant '''''''''''''\l'''t::- his

or

Manufacture of

location.

,th",,,·i"'':3h...,,,,,

not

does

I-rU"rUnf"1lC' •••••••••••••••••••••••••••••••

3-10 O 3-11 3-11

1 1

dissimilar

will not of Section Il, dissimilar

and

Manufacturer.

minimum nominai c)

filler

in

shall not be used in this '-"""""'.u,

~n~~I\lCIC

nor'I'''1i''''TTori li'l' .. ,,>e-""I"\."·~II"

ov-::,rni."\o.rl

in in

in nominai thickness

n~I·~nr~rln

"'f"i''''''''',/"I-::''''f''O

in nominai thickness shall

examined other

any

or

c)

If

vessel

c)

1)

i)

(

c)

c)

i)

ii)

of not

ii) (1 filler Number detemined

b)

c)

1.. ......,. .

,'1",,.. chromium

ct'::llnlo.~c

Martensitic chromium thinner.

1)

C't'::llnlo'~C'

1 or

and shall conform in ali resloects e-'I'~nrl'~11"n IL"'·-""'L.<:H (1

c)

1

c)

Annex

in

s

in

this

of

8

2~Cr-1Mo

Mo-~V

Plates

0.05-0.35

0.015 max

0.20-0.40

0.010-0.040

0.50-1.30

0.20-0.50

0.015 max

0.20-0.40

0.010-0.040

0,30-1.10

0.05-0.35

0.015 max

0.20-0.40

0.010-0.040

0.30-1.10

0.20-0.50

0.015 max

0.20-0.40

0.010-0.040

0.50-1.30

2.00-2.60

0.90-1

0.015 max

UNS

ND4400 N04405 N06600 N10001, N1D665 ND8800,ND8810 ND8825 ND6625

3

o o

o

o

o

1.000

0.0

0.0 4.6

3.0

8.9

5.0 0.831 0.781

0.648

36.5

0.610 36.8 0.539

40.9

0.447

53.6 95.2

0.395

58.1

35.0 68.1

0.349

40.9

0.309

48.0

Maximum : - - - Condition

Condition Minimum

Note: These satisfied.

0.50

1.00

1

o

36 38

4

,mm

1O -I---~~.,.........,~--'----r--+-.................,..........,.......+-...---.,............----t~---r-......,....--+-.....,......-r-~..j---.,..........,.......,~ O

6

80

,mm

Width

40

30

~

..

~

10

o O

4

Maximum Nominai

h'9"'VnL"'''''''''

of Materiai or

in.

~

0.6

~

~

~

0.0

o

40

Nominai

80

60

or

100

0.00

0.25

Not sut!IJect

-60

-+--r--,--,-+...,.......,F"""'T"'"'"~...,.....~~...,....+--.---r---r......,....,......,...~F"""'T"'"'".,.......,..~~.,--t...........".....-+-r--,--..-t-'

O

10

90

mm

00

fabricated

for D

1 of

Notes

Section

Welded

Welded

or without

or

or

or

Ihs::>,c:h,::>s::>t

with

Joint

Pressure

Int.:~nll",;}!hl I-'Olln1fr'I"t"'t:~n

Welded Connection

('nlntainir1'i"l

Part

40

60

100

0.0

+-..-...,...........,....~

........-r........,.-l----,.........,..,...........,.......--l--...,...........,......."...~-r........,.~~+-----".......,...,.........,........,4 60

O

in

o.o +--.......,....----,-..,...............j.............,.-..,..--,------+-.,....-...........---.--l-----...,.............,....----,--+---~.........,.-~~ o 00

3.13

o

10

30

50

Plate

Direction of

::l

Cl

lf)

N

ci + o

N

+

Cl lf) ('f)

+

8 Cr + Mo + O.7Nb

in this Division

forms

shown below.

c)

f)

3.A.6

for

forms

Table c)

Steel

Section Il, Table

f)

Nickel and Nickel Titanium and Titanium

shown this

this

c)

'tnllnuJann

tables

SA-335 SA-335 SA-336 SA-336 SA-336 SA-336 SA-336

SA-336 SA-336 SA-350 SA-350

Mn-%Mo

1Cr-1/5Mo 1Cr-1/5Mo %Cr-1/5Mo -

%Cr-1/5Mo

SA-372

1Cr-1/5Mo

1Cr-1/5Mo 9Ni SA-508

3%Ni-1%Cr-%Mo-V

SA-508

3%Ni-1%Cr-%Mo-V

----

%Cr-%Mo-Si %Cr-1/5Mo-V 1%Cr-%Mo-Ti

-

%Ni-%Cr-%Mo-V

-----

SA-517

J

C-%Mo

P

%Ni-1Cr-%Mo

I

K81340

9Ni

SA-533

Mn-%Mo-%Ni

SA-533

Mn-%Mo-%Ni

SA-543

Plate

3Ni-1%Cr-%Mo --_."~------

3Ni-1%Cr-%Mo 3Ni-1 %Cr-%Mo SA-543

%Cr-%Mo 2%Ni-1%Cr-%Mo 2%Ni-1 %Cr-%Mo

Plate

SA-268

SA-312

SA-312 SA-312

SA-4D3 SA-4D3 SA-4D3

SA-4D3 SA-4D3

SA-4D3

Wld. Wld. Wld. Wld. Wld. Wld. Wld. Wld. SA-814

Wid. 25Cr-20N i-Cb

Wld.

25Cr-20Ni

Wld.

21Cr-6Ni-9Mn 3Ni-5Mn 13Cr SA-965

18Cr-8Ni 18Cr-8Ni

SA-965

18Cr-8Ni

SA-965

18Cr-8Ni-N

SA-965 16Cr-12Ni-2Mo

.---\------=---=------1

SA-965 SA-965

SA-965

16Cr-12Ni-2Mo

58-366

Ti-O.3Mo-O.8Ni

S8-338

Ti

Smls.

Ti

Smls.

Ti

Smls. Tube Smls. Smls.

Ti S8-338

Ti-O.3Mo-O.8Ni

Smls.

S8-338

Ti

Wld. Wld. Tube Wld. Tube

3 Ti - Pd Pd Ti-O.3Mo-O.8Ni

S8-348

S8-381

Wld. billet

Ti

billet billet

R50550 Ti - Pd

billet

Ti

billet

Pd Ti

S8-381

Wld.

Ti

Ti-O.3Mo-O.8Ni

S8-381

Wld. Tube

billet

SA-449

3%Ni-1%Cr-%Mo-V 1Cr-%Mo-V 1Cr-%Mo-V

SA-54D

Cr-%Mo-V

SA-54D

1Cr-%Mo-V Cr-%Mo-V 2Ni-%Cr-~Mo

SA-54D 2Ni-%Cr-~Mo

SA-54D

2Ni-%Cr-~Mo

SA-54D

2Ni-%Cr-~Mo

2Ni-%Cr-1/3Mo 2Ni-%Cr-1/3Mo

Nuts

Nuts Nuts Nuts 7M

I-----------f----------+------f------------------+------------I

SA-540

Mn-%Mo Mn-%Mo Mn-%Mo Mn-%Mo Mn-%Mo SA-540

2Ni-%Cr-%Mo 2Ni-%Cr-%Mo 2Ni-%Cr-%Mo 2Ni-%Cr-%Mo 2Ni-%Cr-%Mo

SA-540

2Ni-%Cr-1/3Mo

SA-540

2Ni-%Cr-1/3Mo

in

function

be used in the stress-strain curve may

rl

=

.0-

+

U

the

'"'"..,'''''."''' in

+

+

+

-+

r

+

{l-

+-

for the rlO(~inrl~tt:~rI 1-'lI'tor'n~1

Pressure Chart Number strain

charts under in Tables 1A

on the abscissa and B

the

A

coefficient

in

t~nlnolnt

modulus.

t~n,nolnt

modulus.

t~nlnolnt

modulus.

stress-strain true total strain total strain range.

0.2%,

on'.,'n'oov·..... n

of of

true t':llnnolnt

stress-strain curve. stress-strain

modulus

of interest. Annex

modulus strain in true strain in

macro-strain

stress-strain curve. model.

curve strain

curve stress. model.

stress range.

R

to

ultimate

l Aluminum

Titanium and

in.

Carbon Steel

1Cr-1/2Mo

/2Mo

in.

390

/2Mo

70

/2Mo

(100 mm

200 300

0.101 0.1 0.1 0.100

O. 16 0.1 0.094

mm

mm

400

600

660 656

633 683

Values

function

are

function

function of 'l'ontU'''lOr~TI

function of tont"lnOrc':ltl

are

nrr'HIt"!On

in

Section

Section Il,

'l"nllnuJ .... "" ....... "'to .. ,j""'"


c)

Nickel-Chromium-I ron not

ex(~ee~alrlg

Nickel-Chromium-I ron not

ex(~ee~alrla

not

eX(~eeialrlg

not

ex(~eeialrlg

in for

Nickel-lron-Chromium

>1 Nickel-lron-Chromium

:::;1

f)

10 , which is

l

rlatOl"'n"'li"'L:J\rl

b)

c)

for follows.

=

ac(~onr1arìce

1)

.(1

.(1

q=

with

shall

c)

A

units cf in ksi.

mcdulus

minimum

cf

SPE~ClTlea

cf

7~

31

1 1 273165~~E-()4 -5.263661

6 8

0.0 0.0

0.0 0.0 0.0 0.0 0.0 0.0

<

3

6

0.0 0.0 0.0

0.0 0.0

0.0

0.0 0.0

1

3

8 10 1

=

0.0

8

0.0 0.0

<

3

0.0

0.0 0.0 0.0

0.0 0.0

0.0 0.0

l

<

6

0.0 0.0 9 O

11

0.0

0.0 0.0

lll"arnan,tc, 4-6 .............................................................................................................................4-6 Mìnìmum Thìckness

c)

to

1)

or (1

and

this Division

of the vessel and <:>n"",,...,.,.,, Manufacturer shall the to ali minimum mmlmum material thickness. The corrosion allowance then the corrosion or other metal loss do not ~D'eClnc(:ltICln that corrosion allowance is not

c)

1)

to the

in

c)

f)

construction for any combination ex~)ectea to occur

S

+

1.1) ~

not

ex(~ee~a

not

apl:lllcclble limit

ex(~ee~a

)

below:

in

+

-1

) constructed other than ambient dissimilar materials

te c)

te

use

c)

f)

60

s

L SPE~CltIC

definition

s

s s

s

Combination column

and/or

n1"\r\nl""~CCI

b)

c)

two

f)

h)

or

transition the

of

1)

No.

thickness of 1

c)

of 1. )

i)

mm (1

both

is not

1)

b

1)

b)

not connections to shells f"'''''.~n''',f"''I"II''\n'''''

Some

ac(~e[)ta[)!e

to

V'lJrelClea

rw'\c~nlrln

in

shell is

to NPS

or

mm

""'rn""iU~'"

wall The minimum

rn~tQrl~IC

not

Qln.nf'l'~tlr\n

not eXI::eEld 1

wall thickness, service

1)

Re:sjstan<~e \N'elcled

studs those included in Material stud bolts to the

"""''''''''''''''''''''1'<''''; minimum

for limitations,

shall

cornOémOle with

c)

is

"',""lib<;)lU"'"'

for IAlalrill"'lt'l to which the attachment is

COrnpé:ltlble insofar treated when

Part 6. is

1)

A

Attachments to n,", ..\nrt::'~~1 is suitable for IA/alriirlt'l

doser gross structural weld thickness

n a .., a t..·""ti?'\n

this is limited

not

ex(~eeidlrlq

fillet weld on each boss butt weld is examination. Heat

f)

= .0;

1)

weld

; the nominai

i)

weld.

ii)

exclusive

the

restriction,

i) j)

1)

in

1)

to

wall

8.

to

if

a b

c

or other

'"""'''''''''',f''I'''.'',",'''' with

or

this Division

Notes:

any

of the

4,

IV&

Taper Either Inside or Outside

Weld

limitations

8

B

a>

iimitations

Fillet Weld Buti Weld

ts >

(1.5

far

Tension Test Specimen

,19mm

>

(l

e;::::max

3

c Tension Test Specimen

1

10

C

1

mm Gasket \

Full Penetration Weld, Single Or Double. The Full Penetration Weld May Be Through The Lap (ti) Or Through The Wall (t n ). This Weld May Be Machined To A Corner Radius To Suit Standard Lap Joint Flanges

6

l

c c

tc > -

o.

r.l

A-A to

o.

'l

,6mm

Limited to DIN

,6mm

3

tg

the thickness of

1

3

Perpendicular Parallel to the Cylindrical Vessel Axis

9

3 mm (0.0625 in.) recess Section A-A

3

9

mm 1

4

>

B A

(a)

(d)

A

(b)

(c)

(e)

(f)

mm (0.25 in.) max.

I-I I I I I I I

: t-I I I I I I I I LI

Round Corners On

On Pads

around

mm(2 min.

(2 min. max.

Intt:u'n"Iittont

One

Weld

-I

I

Stiffener

~

AllI

( Shell

w

-ì

1.

2.

the

to

c)

and

internai

t

eone shall have n'!:lll",:::llloi of their minimum evaluated per noi'ano.n in .... '''l'JI<;;!I~IVI

r-ort\tor'lin":lI~

nitt,OI"Oil"'lr-O

;;:lYl.JIOI.. \

to external

and other

shall

heads

sheils and

.;;)U',JIV'''~

, and assume

in~,f'II,,'"I'''''''

the

to internai

L,

be

and

knuckle

L

-s c)

'l"Allt"1l\Mlr1n n.::lIAn1o'l"i"!f"

constants:

arccos

=

r

-----+

= =

t(- J(-ì+ \

<

s >

J

ex[)ectea to

elastic

knuckle,

in

. If the allowable is determined 1)

If

follows. is the material

is the '-"""',",U'CHe>

the value

ex~)ected

the knuckle.

to

1.0

l

=

the allClwaOle

on

Calculate the allClW81ble

on

'-"UlIIV,",,'''''''''''

maximum aIlC)W8IDle

k)

,nt~::Irn'<::!I1

of

of

crown.

SU[>lec:tea to

'1"11'0 ..",..,,1

substitutions

L

k=-

1.7

c)

+

wall

+

o

d"

( -I)

.\

[-IIJ)

_____ + __

--.:...-_~...:è

p

-----,=----=

+--------

cos

+ ----.::.........;:::.----

+

-,---------+ - - - - - - - - + --,-----~~-

+

+

+

shall be satisfied.

on

c)

meridional stress

is

r:ornO!FASsivA.

satisfied the allowable tr"lf"\ff'lf'lnrO~~'iHO f"nr'1ltrr\liin,n condition for this

1 tr""" ....

'''''''''1 transitions or circular cmlss··se,ctlCms

end Ac(~eptable

internai conical transition details the small end

details shown in that the ones shown in this

-;:;;...,;;;..-+

1 knuckle is

without

to f"ioe'f"r!l"\of"i

a,

the

s S

tL

tL

S

s2

section transition.

The thrust load

aPI:>ll€iO to

inciuded as

to

of

of

, is

Table

=

B=tan f)

other than

stresses allowable stress t""l"lt,ol"ir,n circumferential rnQrnh,r~rIQ shall be considered. is evaluated

O. 5. If

te' at

hOFlfill"'lf'l

transition.

moment ,

the axial

inciuded

v(;)llvUI(;)l~<ç,Vl

transition and

linear

int~:lIl"nl"ct,~tir\n

aPI:m€iO to the conical

cf

values of

other than , is

with

te'

knuckle Tnu·'Vn.""",,,, be ",.-.T"",,!",,.,,rl then

the

cannat

>

as

the

in If either the the

A=O.l ,

to

small

with

of

te' at the small

c)

, and flare cannot

- Determine the net section axial transition the

the location

the knuckle. The

hor'f1ll'"lrll

moment ,

load due to pressure shall not be included

conica! of

d

modulus

E

in in

G

,",~iP""n

.."" ..,h

f''''''~''''n .. ~ ..,h

knuckle conical transition

calculation when

nl"~.co!nt

knuckle is

the of consideration. on the resultant meridional

"""'''''''''''011'''\\'1'

resultant meridional moment

on the to

on

to

resultant meridional moment """',,:'",.. Une load. normalized resultant

""",o,"'ri""'I"'\\'3Ii

moment

net-section

nOl'"'Iri .... n

moment

end

net-section

nOI"'ilriu'".n

i'Yl,"'i'Yl,on'l'

end

net-section torsional moment

on

f"\Jlinrlll"if"''=l1

shell. shell.

shell section. eone,

Une resultant circumferential membrane force

on the eone, due to pressure

an

to pressure

an

the on

in failure ",n,,,,,"',,",, transition

to pressure

an

resultant meridional membrane force

due

Ani Hv;;m:~lm

pressure

crown

is

f"r\lnif",~1

transition

nI"CI~o!nt

vc:llvU!ilQU'UI

is conical transition

nI"Q,~olnt

vQIVU!IIQtl'UI

conical transition calculation when calculation. total total resultant the

f"\lIllnn,::h1"

internai

resultant pressure. resultant

radius to

for

radius

for

force

on

due

knuckle.

inside radius inside radius of the small

of

conical transition.

t", .. ,.f""'''''f'''5I!

transition.

1""'''' f"'" ' " 1f"'51 1 transition.

centroid

.d

of

the

the

shell.

thickness

conical transition. of a toriconical

at

n~r1'I~lhl

drilled hole. hole.

location

a

n~r1'l~ih!

drilled hole. location

stress

due moment. """"""',... Une load

on

due to

axial

and

hOI'H'11ff\rl

)

+

1.

)

n 1

1

10

Note: (1)

sN'

1

1

5

6 8 9 10

1 2

0.000020 0.001668 0.002986

0.003111

0.0011

0.008046

0.002508

0.000000

0.000000

0.000000

0.000001

-0.000007

-0.000008

8

-0.0001

-0.000120

-0.000118

9

-0.0001

-0.0001

0.000001

0.000001

6

-0.003618 Notes:

=

1

8 9

11

8 9

o

)

=

+--~-=--=

---=----± - - - - - = - -

]}

=

=

=

)

=

=

=

=

=

=

+

i ì i

i ì ,

ì

\i/

,

~--O.8

i

Within Conical Shell

"tl"'~CC':llC

without without

Knuckle at the

and

Cone without

of

with Knuckle

Small

<

l

=

based on

. For Axial

stress

follows:

to

e=

ec

ec

+

[~] =~

{~)r

n S; l

1)

(R)"'4,

c)

shall t is

follows: the corrosion allowance. n08rrniii:"ii:"ihlo

deviation is e +

rllff,croint t!"IIf"I<'no'~ct:IC

t

nominai shall be

or

across

maximum loeal deviation shall be

3 do not

(-J

(?zr,(?wnt{-~rpj'r1.tl,'11

shall loeal deviation fram true eireular e, shells and exeeed the shell thiekness. Measurements to determine the with with ehord the tnllnu/'inn

<

.5 <

=1.0

:::; 13 1.5

ìOA he

(F

STEP 4

)

<

Caiculate aliowabie external pressure,

<

n is an

=

11/11<7('701'"

<

use n =

The actual moment shell

+

=1. c}

and

+

L

ettE~ct"/e

where

2--·-:::--

f)

1)

i)

sut>lec:teCl to Qvt,Qrn~1 substitutions:

TnllnU/lnn

where

in

in

+)

+

)

+

If

= +rjJ arctan

+

<

lf

a=

-rjJ

fJ = arctan

In both

rk )

shown

rjJ=

conical transition and

other

te is

In~,""l'n"""

eone

shall

head

(-)

,6<

=0,1

<

,6

+

allClwa.Die external

(-J = f)

less

pressure,

InCf'ea~~e

~p.:np.;=it this process unti! the allowable external pressure is pressure.

to

"'U'JI"""'~ to external pressure

with this

and

=

+0.

+0.

""U""'lv..,t

to external

and other

ir."","!"·"'·"'"

wall

membrane stress of

1

=

<

= :::;;

c= c=

3.13

c=1.0 For

O. 5

.5

.5<

<15

15

/r

g

< 0.15 <

c)

1.

cornor'es~;tve nnorlfll'''\f',~no

stress , is

1 t

1

r

y<0.1

y , is

allowable

1.5

(1+

.5<

<

<

=

.0

+

(~J

1.7

+

-'---------'- -1.0

=

+ and

defined in ",,,,,.,,,,,,,,,..,,,,,,,,,h with the

'-''-i

.

in The

(1-

this reduction

, is

=

)+ n

o

5 , is

01)

combination of

1)

and

+

r

evaluated

=

.0

+ 0.15<

~

.0

~

1.0

~1

+

+

~

1.0

i)

fram

+

1 )

0.15 <

rnQirnh,~1" ;:)!uurO\J~

is determined

coefficient f:1 is

to cornoress,lve axial fnlln\Mlnn

interaction

O\.4~.u::;nIVI

vVo;;;lIUOllvY

LO

1.0 j)

maximum stress is less

<

e may ex(:;ee!(j shells

combinations ofaxial

1

value of

if the maximum axial

t'IIQ(~lnr'Qt'II !f'r.I"!i4lnl"o~c;·'r.n .. _I.".A..

~_,A\

,

is determined

1

)J

au;;:,vlru~o

number

of stress

k)

Jr

A == -'-----'-

4

s==-:..-__.. :. .

==

==

==

s A

A

value

te is substituted far is

c)

~YLJ~tltY

where

is

distance

is

allowable

f"('H"nnro~c~i\lO

the direction of

allowable , where is aDlolle~a

is the allowable

f"nrnnI"C~C!IHC

with

< t

0,

loads

shown below. , and is the value of

the cone at in

)

n~w'~nr~r,h

is the '"'''' •.'''.uv diameter

the

f"\lllnrlrlf"~1

shell at the

).

In these calculatl()nS

pressure

A

ho!nriinn'

and in this

v".,H.JlOLIVI

ends the consideration ( no,,.,,,,,,?,,,,,, when for ",,",,,,,,,,,,,,",,,,,,·.r-ir,,,,,

"""'1"\"""''''I''\'l'"'.r-

c or the inside

external corrosion,

outside outside

the

ri''''''''''I:'.to,"

"""""...,.If:j,1'Ol'"'

modulus '1'"""",,",""'''''+

modulus of nn"".r-+i,,,,'f\,

load.

,on aOI:>II€!O loads.

>:lU!JIl;#'vl

5,

to

in

=

of a

.0 in

with

,",,,unr,,,:,,!"

S:;0.15.

a

the

0.15.

r a

Une of a

to the next of

",ul i nrll .. i",,,",i

rv'on"h"~..

that is

to

;:'U&Jlv'",t

vessel under external

absence of other the

niIl"C\r'Tlr'\n

of

aplDIIEld shear

radius inside radius of of

s

section minimum

cru:~r'l'tlorl

v

4-1

the distance

shell

distance from

shellto

centroid

65

150

480

900

31

600

315

600

h

h

I
l

cf

18

Caiculation

Weld In

Butt Weld

ullnf"l/f',ro'''OAi

Shells-

Conical Shells

r'HlinrU::llr

the

and

'l'Allt'\\IIIIV"Irl

is the outside

""''-11'''''''''''''-1''

for any cross section

are the eone f"An,If"~1

rli~n'1lQ,tQI"

and small end outside EoOroi!',,,,,,,,,

under vVC;i\lUCHIVI

t

with without a

Knuckle at the Small

Cane with a Knuckle at with at Small End

""n~"'ni."n"" that in accordance with

1"1"""'"'710

rio(~inl'''ori

shell or

Studded Connections shall have a Drilled holes to inside surface of the

, l

vessel

1tf"\11f"\\ll/inn

methods.

follows.

c)

1)

=

]

=

= = Calculate

the

of

+te +

+ =8(t+te ) 1)

= reinforcement

c)

the

wall

v'''·'''''''?'ir,nn

inside

] ).

+

=

A=

+

+

A)0'85

).max[(

+

+

+t

the 1)

For ...

" I I ... rIIW'" ... ",1

shells:

of the conical shell of the

"""""''1,''''''511

conical

shell as follows:

STEP 8in

=-'------'-

= the

i)

), j)

k)

=

=

(-J

]

t)+

=

)

shall

] =

)

e-

l-

in

shall

= -_.'----------'-

t)

=

+---'------------'--

+

then

pressure of

=

+

J

wall.

and ellH)SOldal

1)

=

]

]

=

For

=

=

=

c)

reinforcement

+ ellu)sOICial and

tf""lì~nl"ol"i.... ~1

]

[-~]

O'35

.. +te

[(

tn

J

,l

4

the

] the

::::

+

+

+

+

+

+

::::

+t)+

+ +

::::

-t)

=f

""""'Y1I<:'>,,., membrane I

i)

11,o't,ol"lnil"1l,o

the maximum local

},

n ....TIl'="eH

ml,orrlhr'!:~n,o

stress

] then the allowable

is sutllec:ted

=

(-J

external

then

the

intersection.

+-~-----'-

)

=

=

1)

]1

+

xt =

(t+te +

+

)

1

local

"ruTlI"".ru

r\ruY'l '::l\ 1M. I

i"Y1,ol'Ylhr-:~no

stress in

stress at Int~:lIl"n'!:I1 pressure, then

l'Ylon'\hr~:lIno

intersection.

intersection allowable

SU[)lec:tea to external pressure, then the allowable stress is

):

A

B

c

= c)

for

oV'\l',Orn'5li

no~~ZIE~S

1

in

<::"tr<:~nn'th of attachment forces and moments from

1)

=

31

to =

Te

2

+tn +

= 3

c)

are acc:eot:ame. 1)

)

s +

= ------''-------

max

=---'---

=---'--~

1r\~t'!lnn

The nl"'r\t"'orl! is shown below.

1

to weld throat

attachment welds of r1;I"'I"'.on'E'it"\v~~

as aptlilCélble

in

max

shear stress in is If and return

s method I\lO;i::ZIE~S

in

f"\Jllnrjl ..if""::\1

NO;2:Zle~S

in

'1""" ....1"1""1"'1

calculations shall calCUlatlcmS shall

in

"::\f"f"'"" ..,f"!':Ir"'lf"O

6.5" c)

follows: two

c)

f)

400 mm (1

in. x 1

but should

shall

in which the internai pressure width mm

hQ~:ll"lnll'l

=0

+

is

8

walL wall.

weld.

distance

center Une.

Une..

weld

minimum

the

h

fillet weld. weld

weld.

fillet weld.

throat

weld. weld.

of the vessel walL inside of the vessei outside weld

p

internai maximum

to shell weld.

pressure. allowable pressure. membrane

the

s

the vessel

of pressure stress wall.

a pressure. minimum

corrosion

due to pressure of distance

as

11

1

1 mm

The

fram

1.

a

a

Axis

Modified Limits of

Reinforcement

Initial Calculated Limits of Reinforcement

The minimum that results in an

attaehed

moment arm this deseribed in t

tg

=

shall rV::H'~nr-:ln,h

6.

the

t=

cover, shall , and this described in

moment arm of rIl"='''''V'''''''

l"'1I"C:II""C:If"ii""C:Ir\h

t=

tg =

thickness

in n;::\i""C:If"\Ii";::\nl'\C allowable stress limits in Table

).

material as

2 , V,

f

on

the

'I;;I'-'I'''<;;II''V'

in

on rlOC~lnn'::lto

f)

in

4.1

the

6 - Calculate

Y, T,

, L, e, and d

in

on

an

attached

with

= t Where

is

vVCUUClI~ç;U

h)

i)

9

=-----'------"j)

in Table

or hub attached with

nnl4._int'oru"o:5\l

welds:

k)

A

shell VUI.vIUv ri,i:::lfYlot,::.r inside rh~n"Io,to ..

c for

or covers measured as indicated in

d

and other weided cover stress for such

pel"penOICulal to short span. shown in Table

e hub

QDI~nìina-tQ-tlat

for

head

hub stress correction factor

E stress factor for thickness at the hub thickness hub thickness

end of the

sm~II-Io-naI

smail end of the the shell-to-f1at

hub thickness at

hub hub

shell-to-f1at head measured

condition.

allowable or

t tg to ti

nominai

bolt

the

dimension of

OOI::mlina-·tQ-TI:::lt

nn"""""1·,nn

head

condition. "''''''':>T'M,n

condition. the

z

that

times

of head with interaction of the

i nt.::.1"'1l l"'o:lI I

rlCUf'\OI'\rlc

shell

on

Une of ratio of short span to

modulus of elastl(~lty

outside diameter of

head.

rli"'I"""I'I"" ..rili ... 1'I

the

Une

• c=o. for

Y=[l.l-

used

O.

for circular and noncircular with or butt welded to where thickness not than two times thi,,'vn,oC'l::' the corner on than three times the intt::>r'll·,~1

r =

minimum shall be used

ts

mm (1.5

6

c=

far circular

an inside used

8

bolted with

d

the case of an '" ,..ar'''"·~

h

~-t--------------A---------------+--~

dimensions in

corroded condition and the uncorroded

shall be rI ....i,............. i ..'ori listed in "''''''L''''','!''",rI therein shall be f"nrlClrllorClf"I ""1'.."nrl.., ..ri'"

in construction

in

""",T"""1"o ...,,,,,

the

TI"\!li"\UJlnn '-''VI'''' ..... '"'.

]

T=

A

used

both

n~IF~nr~r\h

the

4.7.2.3

satisfied.

shall

Head determined thickness shall be the

for

max

]

rlotorn"lin~:lIrl

thickness shall be determined in

]

=

=

= +

c)

thickness

heads with round

holes

+ is thickness for full-face

for heads with

holes slotted

of the head

+

- the head thickness shall

thickness

=

]

in

+

moment lI'nllf"\U/lnn

modifications shall

). to

6

be

in this

orientation of

where

is

p

R to the

of location

the

the

= A

B

[-] e=q-..!JT-

2l

kj

t cot

1_(_1)cOl =1 (~)cot

e

=

+1

·cot

=

---I

+ --'----'-

J

-------='---=-

and moment for the

ctl";::~CC~:::'C

nnt:llIF~1'inn

in the and the ne;30-IQ-'narme If the stress criteria

and

conditions.

A

c

the for the

e

head

D head alternative moment arm of the

head alternative

6.

n

v p

r

from rnornhl"''5lr,o

local

rnornh,I"''5lI'''IO

local

rnornh,l"''5lrr,o

"""'...'t,"".....

condition.

stress.

on

inside

the on the outside the allC)walble stress from

the head evaluated at the

minimum

SDE~citìed

"'t...,., .......'.""

from Annex 3.0.

T

* nn":ll1"'~1'1r"\n

condition.

t CO~::Iltinln n"''''''1'''~1'I ... n

bolt load for bolt load

C'O~:ltin,n

condition.

condition.

condition.

of

=

3

with

t

5GO/o above

c)

it

c)

aDl:~ilCEIDle to

t= the

c

c)

1. weld weld

c)

not

ex(~ee~a

13

mm

f)

(1 ) with C = 2. or

C

for

other

if thicknesses.

thickness

less

c

S t

the

0.1 ),

minimum maximum allowable mm

d

p* ()

n

in

Une

14

1

in

1 1

mm mm

1

mm

=

100 95 90 85 80 75 70 65 ~

>. (.) c (l) 't3

lE LU (ii

60 55

c::

'6

il

50

'Cl c::

o

..J

C

45

(l)

(ii

>

'5 O'"

LU

40 35 30 25 20 15 10 5 O

Angle of Diagonal with Longitudinal, Theta, deg

this

c) J">\!linrll"lr'~1

shell

full

both

1 not

c)

full

laCI(etE~d V~3ss;eIS

in

b)

1.6 in this section su[>!ec:tea to internai .6.1 to Consideration should be In adejjticm

4.11

1'1"'\"'·,v..... ,~e-'"

to

of a half

additional condition that

must also be satisfied.

1

pressure

, shall

1

), +

+

+ 1

+

+

j

nominai thickness

nominai thickness of nominai • CALI"''" ":iU

shell minimum thickness of

wall.

minimum thickness of

inside radius at vessel.

allowable

the at

allowable stress

Annex 3.0,

limited to a of 6 mm

When this

y

max.

t

'c

(b)

Backing Strip May Be Used

y

(c)

(d)

Saa

Sae min.

(a)

(b)

See paragraph 4.2

Backing MayBe

(c)

(d) min. Throat Dimension :::: tj

max.

j (e)

(f)

Detai! (h-1)

(0.625 in) max

(0.625 in) max (b) far A

(a) far A> B

=1.5 tj min.

(c) far A <: B

B

a=

=/.}

~==±I~~==l:d Jacket Wall

Attachment

Attachment

under with thickness of , shall

not exist Attachment

When a between

exist

00

t -

1

t "

R

1

shown 4.1.2.13,

In noncircular vessel have .different thicknesses. the

rules of this ,,,,.. ,,.,,,,,,,..,,,,,,,,.l''l at locations cross section. or ..""iv,"'n"",,,,,,,,,,,,,,,,,,,t the outermost surface of the shell obtain two values of stress. stress.

be stress at both of the shell to the allowable

l"\""l'\rilfl"''''

"'n.""'n"" ..~,rI

at the

section of a vessel with and without the inside and V""'.""IYI"" aIlC)W8IDle stress as the cross r-nrnn''''C'11'o section and outside surfaces

c)

1)

in the

follows.

sum

one-half the distances to

rOU"I'I'nlrf'U"II"'l

member on

p

p

+---

---+---

1)

=

=

+---

---+---

= =

c)

CIT,g:U'T!\/C

t""""IOtl-',OI'"

moments shall

oerweem 1.0

If

E there is not

If 1)

weld

is

then:

calculation loc,8ticm then: if there were no

If

Iln~lnnJC.ntc

in the J

which would

if

were no

1 non-welded locations results in of the for which '-''4'....... v. the weld occurs at some it to the weld location and J

1

=

+

+

+

+

) with multi-diameter holes

(t

C,l

= -

c)

to

c)

is

the

and

f)

in the

and

+

~l

where

+ +--~---

.0

=---'-----..:.---:.-_--'--

=-=--------------'=---

>

the apl:lllcélbie

this

sat:istleCl, fabrication

.."",i."'!'""""""i,,,,,,,

1'V'l""'l'V'lh""'..

on the

with uniform this

I"oir,fru"t"'inlt\l

member on with of

OIT<::~t"'Tl\/O

width coefficient

hole diameter

factor

location.

aDI)li€~d

IlrI'.:lnt'lant

or weld

factor.

Modulus from

)

inside

of

moment of moment

w

w

vessel.

the end of

",t>"'"ird.. t

side

the

indicates

~~

p

vessel where ~ ~ width of

distance

>"oi ... tnier>i",,"n

distance between inside radius. radius of

S

radius to allowable stress stress

t

thickness.

tI

of

t3

or

t4

or

t5

of

v

w y

3.D.

members

ali

4.1 1. and

f)

the

f"l"\rnnrocc,iuo

stress calculations

1 and

Table

9

10

=

(;J =

=

=

=

--=-'::"'1

(~J=~l -

+

+

+

+

+

+

1

inside and outside inside

in the short

outside on

in

the

and

V"""v',",',,-,

inside

and outside

=

(;J (;J=

)+ )+ +

= =

(~J=

=

(~J=

+ )+

N}

)+

-

)+ +

= =

) kI

-

)+k1

+ )-

)+

)+

} }

s +

1

+

1

+

1

+

1

+

1

+

1

+

~l

+

1

+

1

1

on on

on membrane

inside and outside

=

(;:l

+

(~J

+

+

-

+

=

(~J

(~J=

+

]

+

=

+

-

-

+

)]

l 1--

= =

is

+

cosO

maximum al B = arctan (

+

2

~J s

~s

+

~l

+

+

+

+

l

+

+

l

l

+

~l

in

(~)=--=-......:.­ =

(

~) = ----'-

=----

=

=

=

S biIY

-

-

---=--

+

+

1

+

+

::::;1

+

+

in

inside and

short

in the short side

inside and outside on the inside and outside

short

and outside

on

outside

y

and outside

= (~)=

+

= (~)=

+

-'----'--+

(~)

=

(~)=

+

(;J

+~

+

)

-

)}]

+}] )

(~)

=

+

+

)2}]

+

)-

+

+

+

} ( 1. ,

l;lll j+ +

is a maXlm!Um

+

--:::---=-=-

=

+

e) + (I e

+

)

+

l

+

l

+

::;;

+

::;;1

+

::;;1

+

::;;1

+

::;;1

+

::;;1

+

+

l

+

+

::;;1

l

membrane inside and

in the short side in

on

in

on

and inside on

membrane

circular resnA(~tlVAlv

outside inside and outside

+

+

-

} ~+

+

+

}

+

2

}

(~)= =

=

+

(~)

l]]

+

t· cos 5

)

}2 +

-

+

-

}

} + -

+t1 +

}2

+ -

}J]

=

(~)=

=

(~)

=

(;J= (;J=

]

+

]

+

2

+

+

O~y

~y~

)

+

+ +

+~)}

O

~

+ +

+

~)}

+

)

=

=

+RcosOI -cosOI ) cos

tI

)

cosOI tI COS

°

tI COS

1)

arctan

=

COS

+

arctan

+

+

COS

+

sI

+

sS

I

+

+

sI

+

sS I

+ +

+

S

sS I

+ +

S

S

+

sI

+

S

sS

sS

+

I

+

I

+

sI

+

I

+

I

+

I

S sI I sS +

I

M.

the

N. inside

and outside

=

(~J=

=

(~)=

+

=

(~) (~)= A

= - - ---'----'-

=

+

+

+

+

+

+

in

short

inside and outside

short

inside on

short side

outside inside and outside

side. in

outside

on the

outside

the side stress in the

Y on

outside

h

+

+

l

+

+

sI

+

+

1'V'iIe:>.l'V'iIh,,,,,,,,,,,e:>.

stress in the

=

(2)=

A

=

(2)

+

=

nt:llt'inQt1

A

+

+

locations

+

~1

+

+

~1

+

~s

+

+ 1

+

~l

on the inside

stress in the circular membrane stress in the

at

membrane

c. and outside

C on the

in

outside

in the the

at

inside

outside outside

in the

Y on

inside

outside

==

==

+

==

(:i] (:i]

=

+

S

+

l

+

+

l

+

S

+

+

l

+

l

l

membrane stress in the circular in

membrane

in

on

(2)

=

---=-...:-

(2)=~

(2)=_ (2) _

-

+A

)- 3 +

]

3

A

=

(

2

A

R[ (

~

)

+ff (

~;

)]

-

[(L,)\ (~)(~;)+2(~;)J =

[2(~)\ (~)(r)+

(r)J

L,

12 (

J+ (L J(~;)+ 2

~ ~; )(

)+

G;)

+ (~J(~;)+ - 24(%)(r)+ (r)

8

8

+

l

+

+

1

+

5:.8

+

l

+

+

l

are at are at

C on

inside and

side. in the stress in the in the

B on

side at side at

A on defined

inside and and outside

Y on the inside

outside

= =

=

(~J

s

(~J=

>

Il

)

)3 =

S

sS

+

l

+ l

+

+

S

S

+ +

l

Il

t

l

)2 +

(x

h

(x=-J due to externa! pressure external pressure

---+---

---+---

x

= in

for If the thicknesses

Note

function

not

the above

evaluated at x

=

to vessels

+

the

h/2

---- -----I---.-----:f------------i------------------j

h/2

j-----;[--··---4-------------··-I..---------

A

I

--i--

Distance to Next

h/2

A

-------- ---t---------r---.----.-------.-------.--t- -t--'---

y

h

I I I I -

-----------

~ I

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

I I I I I I I

I I

- -------~---j----~--*--I I I I I I I

I I

I

-----------+----------I I I I I

i I I I

___________

~---------I I I I I I I I

I I I !

I I I I

-----------+----------I I I I I I

- . -

o

c)

Inner

for

wiii

not

thickness

",,,,,,,.nnr,oC'C',;,,,,,,,,,

shall

calculated

accordance with

shell or

n~:ìlI'~nr~n,h

the

inner heads of ."",,,,,,,,,re'n! sections shall

1~\lQrC,n

sections shail

mm

weld.

No,1

follows.

1 or sections

1

in

c)

4.13.9 Sketch 3.9 Sketch

of the finished is

thickness of

3.9 Sketch

solid hub section c)

boundaries

IU'Oi"Y'lOnTe-

of r",::u·'::lnr'::ll".h

in accordance with

IIrOi"Y'lO,nt~

shall

of

3.6.

4.16. 3.6.

l''"Irr'\\IIr'lorl

to

the

shell and

in

on

holes obstructed.

it shall be

rlO(~INr"lorl

to that the distance c)

the

the five

materials circumferential

section of Maximum gap

N

DerWeE~n

3

+

o. total

(-J

shall

exceed the

of

limited

b C

3.

h

v p

Note (1) Note

Coil Wound Note (1)

Note

Note

Note Note (1)

Shrink

!

Note (1)

Notes: 1.

Sketch

3:1

For

16

Or Less

In Thickness

Note:

3:1

Min.-

lnside Or Outside Or

Min.

16 In

Less

Tack

tL Chamfered

In

Less In

Welds

In

Removed

(i)

(I)

Notes: into

annulus

Skirt

o

the results in the vessel ac(~epltarlce criteria in 5.

for structural

vessel within

c)

+ () ()1--( ) + -

considered

Moment and Shear If the vessel is "'"",V'l"'''''',''''''',",,rl at , then the

T,

+ ---='-----

1 3

=

+

= +

=

A

4.

1)

c) not

S.

shear stress in

"'''1 , nrl"',"'''l

shell without

"'i','I"i'""n,nN

below. 1)

is

5.. 15.1

T3 --

=

16)

as

+

+ =0

is

not

not

ali

1

the saddle location. saddle and shall

Width of

i"\llinf1I'"Ii"~1

i"\ll!nf1I'"Ii"~1

shell

contributes

the

of the If

as

c)

Circumferential 1)

~tr~~~~&~~

i"\JIII"H'iI"'I""~1

shell without

width Xl

width Xl shall

~tll'tQninn

""\lllnrll'"li"~1

shell

coefficient

shall

i)

shall

=----'---

1"""">'1''''·''''

, and be that is welded to the (,,\ll!nnrl("~i can

reinforcement or wear

=_--::.._-

)

where

the circumferential

t'nrnnrOCC!I\/O

rnornh,r~rIO

f"'\/li nrl ril"'::;) I

shell with

1)

A

stress Points and of the shell are determined as follows.

l''\O ..'t'iI ....,n

with

e-ti't'to .... i .... n

A Points I and J rlotorn'ilIn"~rl

ap[)IlC,801IB, shall

saddle is

low

=

of \lonrU"!:lI1

ve~;sels

the when

in

as follows.

on

Division. b)

f)

Number 1

a

neutral

Cl'

saddle

1"\ 1""\ 1"1 7 ('U"",, 1" ":l 1

o

k

inside

s

side

l+cosa

=-------

3cos 4

4

(-)

~ l

e p Note:

I I

I

i

--------

--------

I

I

~i~

,-L

~I--

~

...

,-

t


Cl

-

I

T

I I

(b)

(a)

4.1

Without

~ti'iI1'A!l'lIinn

e

(b)

c

a=

Maximum Shell without stiffeners in the

Co ... r!i ..,,., ctirtonol"C'

tt2,r-hlfnll:ll~llt

Location

Vertical

V~~~IAR~

of

.,."..""\0""",

b)

L,;aiICulatl()nS shall

two

1)

has no substantial Int':u·u·'~l connections InU::llnr~1 attachment. 6.5 shown in 1)

apIPIIE!O

to

liL'::~nnO-:::lillnn

1-;:a1'';I''If''';:att:~f1 tl'~nr1oc

rQ\/'QrC::Q

heat treatment

wìth hub shall

or

c)

either

4a 1

"" .....,..".1'..,:>'" in

or

in the

no less

recommended

The minimum width in Table

conditions. be considered.

C'o~:lltir"1.rI

bolt and

2

'-'CA"''''''!:>'

3

tQl"Ifu,\Qr<:ltl

and f"lot,orrriino width should r'nl"lf'\nnl

width of the

conditions

and y from Table , or other QUll:leliineS detailed in Table 4.16.2.

'-IC4,;;:o",y~.

, the

eTTE~ctl\'e

, based on the and shown below. Note that for see 6.6 and

b

::;;6mm

16.1 )

6mm

nn<::lII">::iIf'lnn

+

condition.

is

G

=max[[ =

that

is

)

} (W

g ,

~

J]

non

=

H/O."!"", ... ""

is shown below. the , If the pressure is

c)

c A

nCrl~TI\/Q

action

this

1)

=

i)

c)

dimensions of to n,.n"",,01 a

rh:::'l"'rQ~ct:~rI

, shall smaller hub

the small

, shall

in

f is

+

to

nor'l"'nlttorl

for

intot''U''''ò:}!

1..0. b

c

circle diameter.

= 1..0

for US

Ictt"l,l"'n!:lnl

Units and

=

for

Units. r'nrH/crCit''\n

factor

= "O for

Ictt"ll"'n!:lnl

Units

=

Metric Units. stress stress Modulus Modulus

e

to

=

moment hub

G

of

hub

1..0 for

nnr, .. "''','"

hub

the

CQ~:ltll"ln

condition.

trom

section

hOi'"lrlll"ln rnnrnQnt

m

not less than

mm

on with nut trom Annex 3.A for bolt allowable

allowable stress from

T

Annex

the

Annex

the

tx

v

w

y

J:

o

o Il

1.00

Il

Elastomers with cotton Elastomers without wire

Il

insertion or

r&::àlrnnWY'&::àim&::àlnt

Il

(1,1

nickel-base

3.00

Il

69 (1 (1

il

Il

(1

Il

•

•

4%-6% Stainless Metal: Soft aluminum Soft brass Iron

Il

6.00 6.50

(1 (1

2 b

w N 1I--------ji-----------------------1

max

w+T w+ 4

max

w+

w+


1

w+N w

w+ 8

O.4mm

3

N/2

4

8

8

4

w 8 Notes:

8

A

1

+

1

(~Jl -1

-1)

te+

[3

=--+T

d

e

= d

a

=_'----C-

v

h

)

0.1 ~

+

----l

V

+ +

l

---+

v

ì

+

I

j

o.

--+ =--

f

l

5

c- -

C 2

c-

G

2

2

-B

C-G

c+

c C-

2

C-

~(c

C-G

)[3I

v

=

{3 +

Hub

Hub

I=----=.~

6

--e:rJJ --l

)

,

t,

=

{DDG

f]J

~-----~

Wt::IU'lJu

to b this section.

LO

J =

----=---'''--

~

•

O

.0

=

---'::o.-

.0 Notes: 1. Far an

I

=

nt':lIf"l l'''!:li

loose

with

without

LO

l

user. the

A

HT

Without A Hub

w

w

Where Hub to Flange L;.AI..CCI.J<::l Use Hub

Hub

excE~eds

1:3

Weld

I

r

6 mm (0.25 in) :

mm

4~umm

(1

Note:

Hub

c

Use 90

91

r I

l I I i I I I

I I I

I

I : l

l __ L

B*

c

Reverse

I I I I I

--T I l ! I I l I I I !

\ _ _ ...L

Shell

1-1~lnrl!O

6mm

mm

Taken At

I\Jlll"llnf"\!,nt

Between I nrl~::InQlnrlQnt Of Gasket Location

in uncorroded

the

i"f'\,,,,rI'i·;,,,,,,",

with

if

13

is

into an

P.ITì=~r:TI\'P.

y from Table c)

i"'r. ... t"",...t

forces

load

face minus

\JOI\.AAi(;IUVI

non

a

+

)

minimum

+

) ':l~c~orrlhhi

condition.

2 bolts that is selected

is

=max

1-"""'1"."",,,,,

is also

r"nrl~irloi".:::~rl

factor used shall

is shown below. pressure and ton"'lnO,I"':ltl

r>nv'''',,",r>1"I''''''

c)

Determine

)

+

+

=

=

c

(--

2

=

2

f)

c-O;::'ltu'V'I

+

+--_....:..:.....--

condition

i)

=

j)

eb =

)/; =

+

=

+ +

)

k)

11

Determine the hub stress

f"n.ff''f'Of'''~i?\ ...

f, based on

, h,

the

in

I)

stresses conditions If the

UlL"J"">JL "'"0'-'''''''''''''

ofthe

a

maximum the hub. connection

b

line to the

of

bolts.

contact width. ~O~::ltlnln width. diameter

reaction

inside diameter of

Tnllnu.!lnn

condition

width. radiai distance from

centroid

the bolts to

the

cross section

hub stress correction factor. factor

total

thickness thickness

moment

neck

the reaction moment

the hub neck

small end.

hub neck at intersection with hub shoulder.

of hub shoulder.

g

radiai distance from location of

hub inside diameter

to

hub shoulder

centroid.

reaction. 1"0 "'::l r-tir, n

circle to

hub

sum

total

on of l'1t1\nl'1t1\Olnt

of

of

h\!ril"n(~t~tif"

for

y

condition.

for

~o.~~'fln,n

for

condition.

0.25 in. min. radius

Hub

Hub

or Hm

or Hm

B

Neutral Axis

(f)

bolt

to tac1111tate the

c)

this

c)

f)

Rules

in

or oet'weEm

and

=

two

the

of

S

and

18.1 )

c)

max

-C t ) ,

backsicje of

=

+d

Jt=

max

-ct ),

the shell shell c)

',",O,e>!n,..,.oll" in't""""I"''''''O

InCll~nQOT

with shell and

extended not

aa~)Keted

ov1'onr'1ot'1

QiaSI<:etEld with

f)

8.4

1)

the

considered:

i)

=

ii)

=

3

Tube

shell side

When

vacuum.

,ho(~ho,ot

in

thickness within the

-a,

=

c

e,j

=

18.1

8.1

c,d

=

U'\'::lf'1,nn

case, calculate

rni"\lr'no,l"'l'll'

to pressures

8.1

and ~

on the

8.1

c)

+

(1 +

+

)

==-----=---

+

(l+h

+

) the coeifficiient

A

nn1'iu1j rntinn 1

a

8.31)

E*

d

f f)

+-'-----'----

=

=

'V'''H''",'' -e

+

+

+ -'------'-----

-I on the

= ------:;:;;..;=----

=

+---'-----'--'----'-

1J case,

i)

If

acc:eO'table for

increase the

For

d, the calculation

shell and/or channel

j) shall have

uniform thickness

IntQnl"~1

with the

ts for a minimum

of

, the

l to the

+

+

nOO'\rI ...',,,..

i)

ii)

In

:::;

c)

. In

i)

=

ii)

without differential thermal

and with

v)

Shell

pressure

=

riiti'or,e"nti''5l!

t!".orrV\~1

with differential

tho,rl'Vl~i

shell

without

vacuum. side the

c)

, Jl,

=

-a

c,d

2

=

=

xt

6,

2

=

=

*, and

= -

-a,

c

the

The ... 'l'.Ti'n"",<' ... factors.

=

J

= ---::;..-

and

+

2

=

+

+

o.

2

=0

v

c)

=

8.6

of

=(l+v

2

r

3,

r=

)*

r

O.

=

)

=

+)

=

=0

2

-a

-b

c

d f)

6

=

=--------="'---

= +

2

for acoepté~Ole

for

Cases

5,6,

hon,rI!nn

1)

f"nnCQn./'!:Iti1.10i\l

calculated

8.1

more

1. i)

8.1

4,

if

6,

>""",,",""""",rI to "",,,,,, ..,,,,,,,,,..,,.,,,,,,1'\

10.

1 )

8.11

is acc:ep1:able.

be

j)

the tubesheet.

----.:=--------=:...- +----"--'----

=

(

+

8.11

uniform

thi .... lrno""C'

te for minimum , the

to

l

i)

11. ii)

l

1"\'::'I"\,'''unn

1)

1.

1. i)

te'

ii) rlo'll-in;::,rl

i)

in

18.8.6.

used when and 3_

ii)

may

different

I"\,""'II-'",,,",'"7'51'11-'I"\n

may result in smaller of the tubesheet thickness or

A010lic:abiilitv - This calculation b,and c)

Calculation calculation with the T1'"\IIi'"\U/.nl"l1 modifications.

is •n t'::1 1"11 I" '!:l I with the

l'"\l'"r.t''o,n.

nl'"r.t"o,f'II.

1)

for

outlined in

n""o·-:>I"I1I'"-:>".n

minimum

In

and

J, the

with

r

)

, and

with.

) r

Il

r *-

l~) +

( +1;)]

of 1)

Conditions the tlmle-demmdent

1)

nff'nnOff'tIQC

and

limit

a,

c

govern

G,

C

cf =

G,

*= In

18.1

G

with

*

C

*

and

with

b,c

*

of

= shell

T:

to the

below.

Ts * =-"--"'-

a,

c

8.1

-a

* of

*

maybe

* -a,

*

c

8.1

=---='-------------= -

=

c

8.1

8.1

In

v V j ..AUU'V.

for

with:

8.1

= -----------------=::.::...-...... In

+---:.----'-

+

+

8.1

+

1l"'::Il1'!f"l.I"IC

1)

ah.:u::!ha,at In,tof"U"<:1I1

with

in,tOf"""~!

with

11'"\0':;>1'"\0.0"

Iha,;!hoot •

Iho.;!hoot

""'l'"",.......",, 1 with

shown

8.11.

and aa;:;Keted with ... h-:u"'U"ol extended as a 1'1,.,..,.""""· Qa~)KeteO

with

not ovto .....,·'1of'i

Q;aSK:etElO with 8.

c) 1)

two

have

1)

i)

ii)

=

v)

=

shell

with

1)

o. or

o.vr-h~nlno.l"

is

6,

=

18.

b,c

=

=

l

+

+

8.1

= and

o.

=

=

=.:::::.--_---=---

8.1

+

b, c,

8.1

+

==

o.

*

=

=-'--_.:..-...:..-_--_-:-

=(1+v

8.1

= -"------=-

8.1

1)

)

=

=

8.1

)

G,

8.

-c,

1

)

e

-f 6-

o Sketch

8.1

an

)-~ For

)(1-

)

1)

=-----_--=.:~

i)

ii)

=

+

2

If

1>-18.1

ACCisptalnce crieteria aCCisptémle for

i)

1) 2

+

) + ---=----'18.1

I

I>

4,

defined

8.1 ii)

limit

J

l

=

=

>

),

8.1

=

=

8.1

be

the tube

o. and/or

j)

uniform thickness

b

, in the

its

l'''n'::~nnol i n'ton r"'::31

t s for

with

of

is

+

8.1

=

l

i)

l

and

3, if

ii)

is

ac(~ep'table

3,

l

the

,and

acc;epitabile and

, the channel 1. k)

a combination

1. i) ii)

1)

, and for

ygl\",U!ICHiUi

c) 1)

-a

T= r

T= r

8.1

+

+

the

-a,e,

A

=

o

A

e,

o

A

is

with

=

+

+

=

o 4.1 full

and

c)

full

1)

=

~trc~nrl'th

i)

ii)

1)

i)

the

ii)

to

wall

nominai

in

i)

ii)

full

ii)

,

in i)

minimum

t] . 18.13

to

]

2

combined " . .""'''\/=

filiet

shall

shown in

8.1

follows:

i)

minimum C:;"',AI' "-:;u

), 2

1

)

).

is not

=

+

considerations

in c)

f)

locate~d

in

of

1)

Axial

rnr"KlC>rrT'lC>rn

life in

rules of this

n'!:li"'!:Inl"'!:Il"\h

is

c)

be su[)!ec:tea

Int~:JInrIQn

the

of the bolts to

to

).

from

hole.

p

h

Poisson's ratio

8.8

for outside

rli'5ln"l",.tor

tube limit

c inside channel

rli'5ln"lta,tor

its convolution inside shell

rl'''''n''I~,?or

E modulus of ela.stl<:my for

at

tubesheet at

modulus modulus of n41lrllnnint

J:

for tube

of contact oet1>Neem

h

consideration

at

s

material

to

the

tubesheets at

thermal """".",., .... "';r'''''

a """L"'iH"""",",''''T

of therma! """"'''''''''''''''r,,,,,

r v

Poisson's tube-tin-tljh~!~hl~et r-nr""hi,,,,,,,,rl

welds

weld

axis

under consideration nominai ratio

on tube the

is

welCle~Cl

the

its

p 0.10

h

1.00 Notes:

E

=

+

* +

+

valid for 0.1::;

=0.1.

S

O. S

S. O is

nrn'llirU:l>rl

p

o 0.1

1.

3.

E

=

+

o.

0.1

)

calculate

is

of the absolute

x

o

such that

o

x

4

6 (a) U-Tube

3

5

7

Exchanger

15

I

/ 9

(b) Fixed Tubesheet Heat Exchanger

(c) Floating

Exchanger

Joint

000 000·.00 -.-+--11-1-+

OOO

Do

C) O

~LL1~-~1

[1------

0000 00000 000

LL1

-7"'---_1

00 O

Two

~ - LL3 ---+---~

0000000

oooc)loc)oo OOC)O

Ilh~"c:hPAl

Integrai with Shell and Channel

b: Tubesheet Integrai with Shell and Gaskelted with Channel,

",.,nfi,"" I"",f',,,.. d: UbE~sneet

Integrai with Shell

Channel

Tubesheet Integrai With Shell And Channel

Configuration b: integrai With Shell And Gasketed With Channel, Extended As A Flange

,h""",hooi

(not extended) (d)

Notes: curves

, and

valid

curves

values

>

8.3.

for other

Notes: 1.

for and

for ne",,,,,,,.,,,,,

the values in the curves,

,n'I',.""."'I"I" accurate for

values

18.3.

Notes:

1.

curves and

valid for values

. These the

for other

of

l ~l

I ~

*-

!..-

I

ti -

I

ts

"

!

~

/ . . e"

.-h---..

ts ,1 ~

IDQ)

'"

l l

US,m Es

t

/'

1/

tS '1-1

'\

.....

.-h---.. IDQ)

.c II)

.c II)

Q)

Q)

..c

..c

I--

I--

::l

::l

4.1

\

(

~

!

lmmersed

I-In'::!tir,n

Head

Tubesheet

Configuration with Shetl and Channel

(b) Configuration b: Tubesheet Integrai with Shell and Gasketed with Channel, Extended as Flange

A

Tubesheet

(e) Ga:ske,ted with Shell and Integrai with Channel, Extended a

ahl"<::hl"'At

(f) TubesheetGaske:ted

c)

i) ii)

=

or

for

LO

m,

notexceea

or

in

aocmlCm root convolution

c)

avoid

b)

insitabilitv is

5= of OellOVlfS

is ~nY',c,"::Ilori

.."..",.,+0,..;.... 1

condition. If

= c)

shall

+w+

1)

c)

= O,

l

c) ant:lCI~)atE~a

bellows.

N a1w ' shall i)

in

calculated

UNS

and UNS

number

in

aUclwable internai

avoid column lnsltablllltv is 9.1

9.1

pressure caClacltv as '''' .....'l'V ..'.''-''-' to vacuum, the pressure stress

vY'AO"V'

roirltr.r,r"orl

4.1

c)

bellows shall

torus of

4.1

The

=_.:0--__

OISI)laC;errlem of

>

axial dls!)lac:ement

> c)

b)

>

aDI)IIE~d to

of

bellows

8

p.mHV~~Ip.ll1

+

+

axial diSDIaCernel1t

in

IJ c)

+

+

+

IJ

Position Number 1:

+

=

[

+

IJ

in

c) "'''1''-'''&''''''''''''''''''"' with

dimension

ovro·,","~'1""

thickness

us units.

moduius

k

'iI

s

P.

w

-. - - - = : = - . . . - _ - - - _ . . = : .

=

, 1.0J

k

A=

s

s

1.5

o

1)

o

l

in

in

)

2

)

2

!I:-----------------.---.---J---------------------------'I

Notes: 1)

A

b

---

=

s sS

)

1

?:

<

Notes: 1)

is

C'tI"L,",,, .... ,th

reduction

s s s

3.8

6.4

--

---------~--_-----::._--------'::-..------=-

that accounts

w

f

Displa(:::emlem: y

e

e

(1 )

(1

or

Manufacturer:

1. ltem Number: Drawing/Tag/Serial/Job Number:

_

____IDmm

VesseIOwner:

_

Installation Location:

_ Length:

Expansion Joint

Design

MPa

Design

MPa Internai

Design Movements: :Splscl1"ied number

Design

DC

MAWP

MPa

Compression: (-) Cycles:

MDMT

Shell Corrosion AlIowance:

installed Position:

Vert.

mm Angular:

deg

_"

mm

lnterna!:

_ mm

External:

mm

Spot / Full Square Cut

Outside

lnside

Double Bevel

16. Heat Exchanger Tube Length Between lnner Tubesheet Faces: No

18. Internai Liner:

No

19.

No

Holes in Liner: ID:

if special)

N/mm - Materia! Ves

_

Quantity/Size:

_

No

- Telescoping Liners? No Ves

No

- Material:

oV"lnin<:ll~;rm

_

I Bellows

No ultrasonic

(Describe in Une

mm

17. Maximum Bellows Sprìng

20. Liner Flush with

DC

mm Axial Extension: (+)

DC

Upset

_

mm

14. Shell Radiography:

_ _ _ _ MPa

DC

Bellows Materia!:

13. Shell thickness

mm

MPa

Operating

12. Shell Material:

End Preparation:

_

etc.)

VO'vUIO,"VI

DrawinglTag/Serial/Job Number:

Owner:

_

_

Installation Location: _ _ _ _ OD

5. internai

6.

_____10 in.

Design

psig

Pressure: Design

psig

EXloarlsicm Joint Overall Length:

Internai

7. Vessel Manufacturer Hydrotest Pressure

8. Temperature 9.

o

Design

_

MAWP

rating

_ o

External

psig

psig

Operating

°F

Upset

MDMT

°F

installed Position: Horz.

_ psig

10. Design Movements: Axial Compression: (-}

in.

in. Axiai Extension: (+}

in.

Lateral:

°F

in. Angular:

deg

11. Spedfied number of Shell Material:

Bellows Material:

13. Shell thickness

in.

14. Shell Radiography: 15. End Preparation:

Shell Corrosion AHowance:

Internai:

_ in.

External:

in.

Spot / Full Square

16.

Outside Bevel

Inside Bevel

Double

Length Between Inner Tubesheet Faces:

17. Maximum Bellows Spring Rate:

(Describe in Une

if spedal)

in. No

Ves

Ibs/in

No

Yes-

Drain Holes in Uner:

No

- Quantity/Size:

Uner Flush with Shell

No

- Telescoping Liners? No Ves

No

- Material:

ultrasonic examination,

SOE~ClrIC

to the

and

the

c)

low pressures.

oV'':lmnio

aOIDilc:able to

function.

the

a

InSDe~:tlcln

program,

and that

the

construction.

nor

e h i,

k

1)

constitute value of

test. . In

.0.

=

e

in

for

/

s

), l

1)

(1 )

(3)

(2)

(4)

Test Block Support

Plunger

Stiffening Ring

TestBlock

Snap Ring

l I

O-Ring (typical)

N.P.T.

Test Block

Cylinder

~'- - Snap Ring

c)

c)

limit c)

structural

intr-,,..,,ri,hl

) 1)

in

5.6.

)

5.6.

)

1)

and

c)

, or

1) .

~s ~l

+

c)

on of a The material small displacell1elnt

iimits

limit-Ioad

c)

If applilcable,

User's

f'laicarrY1lln,o

c)

the acc:epltabiilitv cf

cf

=

~Jl

=

+

,0

1 )

=

c)

c)

1)

c)

f)

c)

on

c)

N

construction

is

)

(

) ) +

+

=

J'

,o

used

, in ), In

f)

the

h)

s1.0 i)

+

+

J'

+

J5

i) j)

S .0 k=l

k)

c)

o

+

), (

+

+

), (

+

for

).

+ ela:stica!ly calculated

, fram

ela:stlcally calculated

structural

are

+2 and

= =16 mm

16 mm l

t

l

l

(1-

LO

=

mm

= i)

6

8

ali

j)

location

.0 i=l

k)

the

shown

range

=

+3

r J

in

r

=

minimum

POSjSlbie

=

is

In

l

=

+

---------~~--------~.:--...---_--::.--'-

+7.

(-)

thermal

c)

C'n"',f"''t'~:>rl

minimum

c)

(~)

o

< .0

=

<

(1

5

LO

of

in

in

whether

not

1)

'LlULULlI""

to

minimum c)

of

than

w=

6.

a

a

under

sm~citjed

full range of

two adH:iCelnt normal

normal

normal

two adiiac!ent

stress

direction.

evaluation for under rc:::"'fl:=lIUaUIJI

m,k

nominai

and evaluation.

the .""".....""''-' or

)

as~;oclatE~a

number

with as~;oCllatE!d

with

the shell to

axis of

the maximum stress in

L

s

L

at at

OIUell.IVI

far

m

the

w

s

s s s s Notes 1)

+ +

1)

+ +1

+

+

+

+

1++ l

+

+

+

+

/"lotlno/"l

in

Junction with

Notes:

1. to hov.,rlIlru'"l

1'Y'l~"n'l"-:un

is classified

POEiSibilìtv of thermal stress ratchet. ''\l'~IO'''''I"

linear stress is defined as the linear stress distribution stress distribution. moment as the

the

Material

Steel and Nickel

',.a':lllnl,=>c>~

Stainless Steel

Aluminum

1

(1

Titanium and Zirconium Notes: not reduction in

the

spe~ClTlea, nt"I<:l"Int"l1

in

Notes: differential is unknown or cannot be

On

o

est:abllsnE~C1

a

Number Of Thermal

1000

is:

shall

construction

4

knuckle construction

=4

Weld Condition

1.5

NA

1.6

NA NA NA NA

acc~ordlan<~e

with

Notes:

satisfied:

Stress Local Membrane \l,n ..",,,,,,,, stress across any solid section. Considers discontinuities but not concentrations. Produced mechloads. il

Increment

j I I

....

_

....

-- :~~

I

)

l

">

<:

W

Wall

EClILJIVl:Uei1Ce

results

In the finite distribution distribution If

OlloirrlOlnt

an

rrlon''''n

c)

continuum

Structurai Stress Method but l''Octl''lf''tc

b)

c)

1)

i)

ii)

When the

stress distribution

1)

1)

c)

of the iinear "'=I,-".nl"

stress is the the stress classification

of

2 c)

ìs the tensor whose

The

+

)

f"nrrVH'", ..."non'il'C"

-l)

continuum or shell alorrno,nte mesh-insensitive structurai

c)

j, j , normal to the

nodal

CcOf"tir'\,n

.,,-'''''''''.., nodal moment nodal force

""il"'>'I"!f'l"",n'l'

iocation ,,,,,,,,,,,'1'.,,,,,,,, used

."n_u,~~"

nodal

element

lY\t'\ilY\Olnt

iiJii~UYlçp

or

thickness direction. Inf"':!lti""n

plOSI1t1on

under

stress tensor

inside surface shell. OiOll"!f'lo'n'l'

radiai

f"t'\tf'W'niln':!l'to

locai f"tr>,,, ..r!liln':!l,ro

of node

x

j for

.... "" .."''''''''.

t'\rl,cnj~an

w

iocation pmmlC>n

normal to

classification

stress claissITlcl:3t!e>n

defines

location

nodal

=---"-----=-----'=-

=-~------_---:-

=

=---'----------'-

---:;;....--,~---=--

w w

w w

SCl

IVlIU··Dlarle \

!

l

with

-

See Datai! A

1)

Note

should

Thick '---~~~--~4L:.L..----,~Plate

-+--r--+- Thin

User.

in this Annex

f)

shown

c)

stress-stra in

c)

8. ranges "'nt'Il,",~,·o

the absolute

of ranges

Y

Y.

3

f)

h)

c)

the counted

which

the three most

J5

mn

f)

- Determine and

8-

maximum von n

t

of

9

and

the event or

number of i)

and

Determine

t

as number of

<

trom those considered in n

>

n

and

the number

t considered

and reduce the number of

reversais k)

nt mn

nt

mn

.

.

with and nt .

mn

stress nt

nt

in

with

normal

in the

.

mn

mn

normal

.

mn nt

with

with the

in the 1-direction

with

in the

with

in the

.

stress

time

and nt . mn

and nt . under consideration with the n

t

under consideration that number nt

.

Rainflow Method.

y

absolute

the Method.

range

stress in ovr,,\;:I!I"1,C!i"I,n different """il""''''''''''''! stresses that """"'1"'1'01,,",'11'

J5 +

1)

i)

ii)

The non-linear =

distribution

/t) the assoeiated loeal below:

= =0

2

i=

3

=1

+ .0

>

) .6

) non-Ioeal

strain

rorli~trihi

1)

loeal therma! and

TnO,rnf'\~1

the

m

in

=1.0

1)

1J l

noteh

1)

In

pla~)tleltv

1 and

i)

)s

= 1.0

»

l.0} = +1.0

ii)

results that are <.4U''''''''''-',""

=

.0

= =

]

(l(

SCF)

>

c::Ll.O}---'---:---'---:--

=

1)

Poisson's i)

=

=

+

-l).

+1.0

J

+ non-Ioeal

strain redistribution

i)

ii)

with

results that eoneentration

f)

6

oe1N11Elen time

+

+

+

+

as

below.

stress

a

and OeltwElen time

to thermal

nt

hOI"\rlu"in

non-thermal

non-Ioeal

redistribution

noteh Dlastll:;ltv

n

nrUl_'r1,r''=3'

for

strain redistribution

loeation and

time

for

effeets for

for the

wall thickness. distribution. distribution T. x

z

distribution,

true. wall. lf the axis on obtained fram

(l +

the

c)

~

1

l

shall 1)

shell thickness t"

max

cf in "'''''''''''',1'"1'''''''''0 with

c)

aOI:lIIc:aOle rules

satisfied.

nnonnh,,.,,,,,,o

stress

with the

l

indices

the

'l r2

local

r3

local the

stress ""''''''''''''''''''''',,''''''''1' ''''''''l''I'V'l'' I

!t:'~"""t.""n

of the section under consideration and stress

normal to

around the hole in shell. minimum thickness in thickness of pel1or'ateld axis of

of the section

nrrrilin~lrrihl

n~II'~II,ol

the circumferential stress

under r'nrH:~if'iorr~::Iltir.n or the thickness or the thickness and

the normal to

to the

nnrr'tlnn

of

vessel.

the as aPt)IIC;aOI!e.

R

3.1

1.2

1.0

1.0 t

R

3.3

l

l

2.1

0.3

NA

NA

NA

NA

NA

NA

Notes:

1.

fillet Maximum stress/stress moment.

3

in

of occurs

as from

e

contains method trom structural interaction with lI''''III1"\\AlI''''''' conditions:

aOI:>ile~d

1"'I'::l1"'::lnr'::ll"".n

c)

adlac~3nt rno.rnho.rc-

loads

function of

rla1rarl'Y'lil'"lari

1)

based on the the ~n~~I\lCIC

"'.".''"''"''''''''' Poison's

the out-of-

strain

for

i)

ii)

E

= v,

of

modulus

modulus the ç:;1.4~.AaUUI

i)

-*

-*

<

in

stress

:::ln':H\lCIC

can

evaluate the mechanical thickness

b)

l

distribution

=

=

- sfJsl

evaluation.

1)

1)

)

)

)

)

c)

I

and

6

+

+

At

)

+

)

ofthe

of

HA'rwj:~An

the

of (

v

)+\

"

v

+

+

= = =

of

)+

+

)]

and

Tables

information

LO =

=1.0

=1

=

with

A

d*

direction

coefficient

coefficient of

G

(1+

r!1-:::lnnn~1

direction

J1

*

v direction for

p

normal

the rim

the

normal

normal

normal

for

in

"""",,,,,",,,r_Tl"._,,,,,,,,nH;;>r

rilC't~~nr'a

between aetllaClsnt in

rows, but not to exceed

l''O'ft::lI''O,nf''<::ln

to the local

coordinate

1.

E LO,

=

-6.193608E+01 -7.869233E+00 1.094078E+02

7.097756E+00 0.0

8.368412E+01

0.0

0.0

0.0

0.0

0.0

0.0

0.0

Note:

if

< O, l, then

0.1.

0,1,

O,

,O,

=

::;;1.0, If

=

-5.969066E+01 -1.407781 E+01 1.921504E+03

2.363003E+05

6.022030E+01

6.108286E-01

-1.346693E+02

5.674145E+04

1.627461E+01

0.0

0.0

0.0

0.0

-1.056089E+01

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

5.916208E+00

-1

Note:

:s; 1.0 ,

far

is

nV'r'\lIf'~o.f"I

far infarmatian

=

+

*2

+

-*

E

+

~_-:-.-_+

E --*

G

=

1

=

v =

=

Notes:

LO.

-*

=

---'---+-+

v

E

+

-*

G Notes:

l.0.

=

=---"'---

in

shown

*t t *t

o o o

=

)a

o o

t t

o o o

o o o

o o o o o

o o

o o

o

]+4 =

=

+

e

+

= cos

=

-4

e

v rllf'Q{"'tlnn

1

in

Notes:

l''\rn'ulru::>rl

for information

3.

Valid

Notes: 1.

O.OOOOOE+OO Notes:

Os()

and () (() is Valid range is 0.1

s

nl"n'l/ln<:~n

for information

Notes: 1. rlotiniti""n

3.

Valid

~

of

l.0 , data

o~e~

information

Notes:

Notes: 1.

information

Pt - Ph * Pt

Ps*

Ps

Pt

Pt

1.

=

=

y

a* x

a* x

x

Uniaxial

Loading along Y-direction

/Il*

, I

I 'xy

8 *

Pure

'ez

*

* *

*

*

*

With

the

of

=

=

of

c)

NT =

=

the shall follows:

max ), 1

max =

),

1 )

),

finish. stress. an

results.

minimum number

far the

) ) )

)

C'nL:>,...i'i"iori

)

I I I I I I I I I I I I I I I I I I I

I I I I I I I I I I I I I I I I I I I I I I

N

6.3 6.3.1

6.4.1

c)

1) if Ali

any

wiii

thickness

1)

c)

1)

c)

b) c)

b)

c)

1) mm

and to

in

c)

shall

this

shown

iX.

in

i)

datail such

1)

on

ii) c)

Examination

c)

Joints

b)

cf base cf weld

1)

wiii


the

if

shall not

',","Jl'U,",U

in

in

1)

c)

or

f)

weld. Materials

closed

1)

the

c)

f)

c)

weld

nU';:'r!;:;;lIU

UU'CllI.ilICiU

and

in

located

located

1.6

(1/16

ii)

i)

i)

i) ii)

8, resloect!veN

fram

are

1, 3 maximum.

has

b)

=

=p

=----'-----'---

4

=

+

t

hollow such

tro':otnf1lo.nt

shall

to

c)

follows.

b)

or

ovtan(~lnrH::>

c)

shall not exc:;ee!(1

in

without

SU[)OIE~m~::mt

and

c)

at least

c)

and

Section IX shall be

Nondestructive

aV":~l'Y'iIln':lt'l?'\n

11.

3.1

Rules

1.

formed

c)

d

modulus

g

p r

to

to

S

t tA tE ti

e

of

0.04 hr/mm,

b) minimum

1)

c)

15

tn >5 in: minutes in.

3)

4)

d)

1100°F,

1)

3) b)

i) ii)

tn > 5 minutes for in.

2)

i)

ii)

c)

maximum throat 'iI''"'''''I/.''1'''''''''''''

3 is

hr additional inch

a)

i)

a

ii)

a

i)

n4\<:::iVII4\"'li

tn > minutes in

3)

b)

c)

15

the minimum

C 30

mm

:

c)

1) minimum. Far tn >

aver

1)

and

in: 1350°F F max., 5 minutes far additianal inch inches.

a) 0.04 hr/mm, minimum

b)

1 hr/in,

hr

a)

3)

or

b)

the

i) ii)

maximum thickness

tubes

c) d)

e)

f)

3)

b)

Postweld heat

direct conditions SOl3ci1fied

thickness

min/mm (1 1,

of thickness for 1 and

SA-353

9Ni

1/4

SA-517 11

1/4

4

1/4 1/4

SA-51

1/4 1/4

11 3

% %

1/2

NA

NA

CI. 3

1& 5Ni-1/4Mo

C

Notes: 1.

air.

3.

--- ! --- ---

'---+------'---

These !tems

Test

Reinforcement Machined With Metal

mm

(a) Originai Configuration

(b) Flare

Upset (O.D. Match)

Swage

(e)

(LD. Match)

(f)

the

c)

b) c)

ali

thickness

ru'c''::llt""r

than

mm (1

location of nondestructive

1) shall group

c)

butt

or

1 shall

nn-"71t::lIC' e:x.CE~edls

orweld.

1)

pressure test of the test fluid

seeipa~~e

b)

b)

3, oV':HY\l!nofi

c)

in

'='f"r>r","fil,=,nf"O

b)

that

random ....... ~ru''',"'tit''

minimum unit of shall be t"nrnnlotolu examined

b)

v.

1)

i) ii)

i)

ii)

rounded indications that the

mm (1/8

to 6

c)

mm

c)

f)

i) j)

" .... rno.",,'!'

UT

III

in

1) FlU"'""">hl",,

flaw

aC(~el:ltarlce

or

O, internai on the

t"1"':I1':'1':'111'\I

an indication

similar m;::ltol"i;::ll it has been """t"'I'~nnlo that

shall

c)

in

c)

1)

width. than or

1)

mm

or

c)

not

mm like indications detected.

or

,,,,,.,,,,<:'1"\,61"'1'''/0

f'ioc~f'ril"lOf'i in

this section: until

c)

such

c)

or

c)

25

include

notch

1)

show the entire weld aelreC'[S disclosed the e:.V""i'Y1I""e:.r!

Unlimited

process this Division

Notes: 1.

maximum extent PO!:;SI[)le.

that differ

6.

thickness.

I

I~","::-"'''~'~'"'"'-''

~,.

'-' I

~"

". '-'. I

100% 10% (4) 100% 10% (4) 100% 10%

100% 10% 100% 10%

NA NA

100% 10%(4 100% 10% (• 25% 10%

100% 10% (4)

100% 10%

100% 10% (4)

10% 10%

100% 10%

NA NA

25% 10%

NA NA

25% 10%

100%

10%

100%

10%

10%

10%

100% 10%

100% 10% (4)

100% 10%

100% 10%

25% 10%

10% 10%

l ' U V IV .Jl"""n.1

100% 10%

I

10% 10%

100% 10%

I

100% 10% (4)

100% 10%

100% 10% (4)

10% 10%

10% 10% (4)

100% 10%

l

100% 10% (4)

100% 10%

100% 10% (4)

25% 10%

10% 10% (4)

100% 10%)

9 1-"

I"

...,.

~~

I

100% 10% (4)

I

10%

10% 10% 10% 10%

!\ 10%

10%

NA

10%

(4)

10%

10%

100% 10%

100% 10% (4)

25% 10%

10% 10%

NA NA

NA

NA

10%

10%

NA

NA

10%

10%

10%

NA 100%

25% 10% 25% 10%

100% 100%

NA 00% 10% 100% 100%

A

NA 100%

NA 00%

10%

D

Not

Lack of nOlnofr>::lfu'1In

Undercut

ner'l'Y'Iit'fef"'!

far

/

~

Notes:

3) 4)

o.

al 0.00

al

al t

0.020

0.031

0.022

0.033 0.033

0.038

0.038

0.40

0.058 0.067

any allowable reinforcement, and the two members thickness ne:,.,oh,"O>tir\n weld indudes weld, then

n""i'"""m<:::ItQi'"

1) of the dimension 3) 4)

al 0.00 0.10 1 0.20 0.30

0.50 Notes:

a

Not Indication Wash

.5

IU'

n'...' ....-

Possible Condition

of

in

t in

The

L

= 6 mm (1/4 / /4

(1 )]

1

(1 )]

Notes:

in any

mm

o

(1 )]

. . . .. .. ,

'

(1

(1

150

10

19

(1 )]

mm

mm (1

Notes:

mm

for

(1 )]

mm (1

mm (1

Notes:

1

Il

(1 )]

•

(1

(1

1

Surface Flaw #1

#2

Unclad Surface

Surface Flaw #3

S

Surface

or is greater) Pressure Surface Of Unclad Component L;i~~rl-IK~!~I" Metal In+<:,rf<:l;~'" Component

Surface

#4

,

S

/ ( \

\

\

) I

/

1/2 in.

Parallel Planes

Ciad Surfaee Pressure Retaining Surfaee Of Unelad Component Or Ciad-Base Metallnterfaee Of Ciad Component

Seelion T-T

Surfaee Flaws Note (1)

Surface Flaws Nole (2) C'

D'

Surfaee Flaws Note (3)

E

E'

+

1)

1)

cf this

InS!pec:tor shall

u"Tn""<:',,,

The Certificate Of Authorization Boiler And Pressure Vesse! Committee

Obtain the Certificate and maintain Ouality Contro! System

Manufacturers Ouality Control System

Applic:able Drawings Documents

Before Fabrication

CorTIpljan(~e

Of AH Materia! The Fabrication Of The Vessel Or Part unf'IIUt1unn Sample Test

Maintain and Quality ControI System

Annex

NA

that applicable Report, User Specification, dra,wir1Qs and related available docùments

7.3.1.1 Fabrication

Before Fabrication

6.1.1.3

7.3.1

Traceclbility Of The Material

NA material identification numbers have been properly tr<::llr"lcf,,,rr,,r!

Proper Thickness And Dimensionai Check Vessel Components

Qualifiical:ion Of Welding Procedure

Welders

Before Welding

Make examinations to confirm that the material identification numbers been

7.4.2 through 7.4.6 ControI For Required Treatments

7.3.3 7.A.3.2.5

Impact Tests For Welds As Production

Welding

Certification of Qualification of Nondestructive Kadiogn:lphic Ultrasonic,

After Welding

3.11

7,5,4

7.5.6 7.5.7

Nondestructive Examinations

Visual Examinations

Manufacturer's

After Welding

Welding

After

3.11

8.3 8.3.1

................................................................................................. 8-7 ........................................................................................ 8-7 8.5 8.6

Nomenclature

8-8 8-8

1)

examinations

pressure UV'"'''''''','V

c)

r;:;lFlricr!

b)

c)

d)

out

OlrrliC'Clr,n

examination in accordance

1 of

c) but

8.1

c)

b)

at

in

=1 or

=1 for

shall but

8.1

1)

b) if distortion.

on

for

c)

b)

test closures those shall visible of nOI'"rrn<::lnolnt

ton"I""""~If'''

;:)ultaumt)

of

c)

Position of f)

Test fluid

lf

is TOlloweo.

written

minimum

s

l''OT<:::>I''Ot"\f''O

shall

9.3

1 9.3.3

9.6.1 9.6.4

c)

VIII,

shall follow

1.

in Section flow ",,,,,,,,,.,,,,,,,·r,,

f"I""1-''''''',f''I

, and shall meet Division .

combination certiticaticm tests shall

Cal)a(~itV

defined Section certification and tolerance of

'O.'"''II"I",.n

or

1.

in

CUC1tOl'Yìl

that is used to limit redundancies n!::lI"!::lnr!::lfl"'lh

shall state shall be noted on the Data

VP'~,~p.I~

9.7.1

another flow

administrative

,..rw\trf"\lc

of

i)

Outside

and/or

in

ii)

i) ii)

c)

f)

pressure relief considerations maximum allowable \Alf"\l"vir.n

Process Conditions

fluido

f)

wiii

and

c)

consideration must also to nO'"1"'''','''

nTn .. n .. ,ot~lhr...":' Volumes 54 the Volume 57 is the first 2007 Edition.

Section

I II-A 11-8 II-C II-D (Customary) 11-0 (Metri c) 11I-NCA

111-3 IV V VI VII VllI-l V!II-2 VIII-3 IX

X XI XII

56 were included with the volume to be

service to the 2004 Edition of with the service to the

Intl:> ......nt''''lti,-w,,'

Val. 57 7/07 7/07

7/07 7/07 7/07 7/07 7/07

7/07 7/07 7/07 7/07 7/07

Val. 58

Val. 59

ENGINEERS

2006

issued between the indicated dates This includes aH written on behalf of the ASME Boiler and Pressure Vessel Committee response to mqlUlI1es COltlCé~rnJmg mtl::;rpret
matter or present

n ....

'-l"'+",-l

of technical

,,,,,,,n ..',",,,,,,,

to the ASME Boiler

Pressure 'lessel

pré~paJred to assist the user in lOC;atlng mtenJretatiOlJlS cover issued from Volume with each volume.

269

File No. AD-lOO(c). . . . . . . . . . . . . . . . .. .

VIII-2-04-12

270

BC04-650

VOLo 57

Division Issued: lune

.L;UJlUUU,

2003

2006

File: BC04-6S0 the

JlJ'v"H/<.U'vL

to

stress

instead of any

of AD-IOl and AD-420. the to use stress in accordance lieu of the rules in AD-210 for transition sections? Yes. of the Appel1Cl.l!ces 4 and S in lieu of the rules

nrrnTH'l"tH:O

A-JVC'"'F,HV'"

to use stress "'n""~T<"L' in accordance Article D-S for other

Yes. the to use stress in accordance in lieu of the rules in Article D-7 for flat heads and bolted and Yes. the to use stress in lieu of the rules in Articles for AD-9lI,

and AD-940.

271

272

SECTION

Location Table ABM-l Table ABM-1.2 Table ACS-1 Table ACS-2 AD-100 AD-100(b) AD-lOO(c) AD-102 AD-llO(a) AD-132.2 AD-140 AD-140.1 Table AD-150.1

AD-151.1 AD-160 AD-160.2 AD-200 AD-204 AD-21O AD-340 AD-400 AD-451 AD-510(c) AD-520

Fig. AD-540.1 AD-540.1(b) AD-540.2(a) AD-550 AD-550(f) AD-610.1 Fig. AD-613.1 Fig. AD-701.1 sketch (b) AD-702 AD-900 AD-900(c)(I) AD-I101(b) AF-111

CUMULATIVE INDEX

No.

Page No.

VOLS.

Location AF-1l2.1 AF-135(a) AF-140.1 AF-145(a) AF-200(b)

VIII-81-49R VIII-2-S3-08 VIII-2-S3-29 VIII-2-S3-19 VIII-2-S3-19 VIII-2-S6-17 VIII-2-S9-01 VIII-2-04-12 VIII-2-95-03 VIII-2-83-18 VIII-2-83-22 VIII-2-83-15 VIII-2-S3-35R VIII-2-83-35R-2 VIII-2-83-26 VIII-2-9S-02 VIII-2-01-12 VIII-2-04-07 VIII-2-83-35R VIII-2-83-35R-2 VIII-2-83-38 VIII-2-89-02 VIII-2-92-12 VIII-2-83-20 VIII-2-98-02 VIII-2-83-33 VIII-2-89-05 VIII-2-83-15 VIII-2-86-18 VIII-2-89-17 VIII-2-92-11 VIII-2-83-39 VIII-2-92-13 VIII-2-89-07 VIII-2-S3-39 VIII-2-83-39 VIII-2-S3-09 VIII-2-S3-33 VIII-2-98-05 VIII-2-86-06

BCSO-725* BCSO-725 BCS3-385 BCS3-135 BC83-135 BC87-427 BC87-198 BC04-650 BC94-617 BCS2-652 BCS3-245 BCS2-296 BC83-653* BC83-653** BC83-221 BC97-511 BCOl-822 BC04-1553 BC83-653* BCS3-653** BC83-644 BC87-298 BC93-347 BC83-169 BC97-511 BC80-606 BCS9-00S BC82-296 BC88-079 BC90-654 BC92-384 BC84-138 BC93-416 BC89-227 BCS4-138 BC84-138 BC82-861 BCSO-606 BC98-051 BCS6-377

5 13 28 23 23 85 91 271 165 23 25 16 45 45 27 202 243 267 45 45 3S 91 147 24 202 35 97 16 85 115 147 39 153 103 39 39 13 35 207 71

VIII-2-S9-14 VIII-2-04-01 VIII-2-S3-14 VIII-2-04-03 VIII-2-S9-16 VIII-2-89-16R VIII-2-S9-13

BC90-436 BC03-1249 BC82-20S BC04-271 BC90-533

110 259 16 263 115

AG-110 AG-120(a) AG-120(a)(3) AG-121(a)(l) AG-121(c)

BC90-344

110

AG-121.1

AF-2lO AF-2lO.l (b)(2) AF-220 AF-221.2 AF-222.3 AF-223.2 Table AF-226.1 AF-229.1 AF-234 Table AF-241.1 AF-320 AF-334 AF-402 Table AF-402.1 AF-402.2 AF-415(e) AF-420 AF-540 AF-551 AF-563 AF-572.2 AF-605 AF-630 AF-635 AF-S05.1(a)(2) Fig. AF-SlO.l AF-8lO.20(b) AF-810.20(d) AF-SI5.1 AF-S20

(a)

No. VIII-2-S3-06 VIII-2-92-06 VIII-2-92-09 VIII-2-92-03 VIII-2-83-30 VIII-2-83-30R VIII-2-89-12 VIII-2-92-17 VIII-2-98-01 VIII-2-9S-07 VIII-2-98-07 VIII-2-9S-06 VIII-2-95-11 VIII-2-S3-34 VIII-2-83-36 VIII-2-83-03 VIII-2-S9-04 VIII-2-01-11 VIII-2-83-31 VIII-2-01-07 VIII-2-92-18 VIII-2-83-24 VIII-2-83-43 VIII-2-83-06 VIII-2-83-30 VIII-2-83-30R VIII-2-S3-28 VIII-2-83-28 VIII-2-89-10 VIII-2-86-10 VIII-2-95-05 VIII-2-83-31 VIII-2-89-03 VIII-2-92-10 VIII-2-04-02 VIII-2-86-02 VIII-2-04-02 VIII-2-04-05 VIII-2-S3-31 VIII-2-83-45 VIII-2-S9-1S VIII-2-S3-26 VIII-2-86-11 VIII-2-9S-13 VIII-2-S9-19 VIII-2-04-04 VIII-2-9S-14 VIII-2-01-10

BC81-656 BC92-150 BC92-349 BC91-465 BC83-540 BC83-540* BC8S-426C BC94-107 BC97-264 BC98-228 BC98-228 BC9S-053 BC94-422 BC83-652A BCS3-683 BCS2-513 BCSS-213 BC01-792 BC83-341 BCOI-316 BC94-278 BC82-736 BCS4-371 BCSI-656 BC83-540 BC83-540* BCSI-531 BC89-399 BC87-066 BC95-049 BC83-341 BC88-126 BC92-109 BC03-1646 BCS5-330 BC03-1646 BC04-060 BC83-341 BCS4-003 BC90-729 BCS3-221 BCS6-073 BC99-275 BC90-652 BC03-1277 BC99-273 BC01-404

Page No. 7 136 141 130 29 51 109 159 201 213 213 20S 189 36 37 6 92 243 35 237 160 26 52 7 29 51 28 28 109 72 171 35 91 142 259 59 259 263 35 53 116 27 73 220 121 263 243

SECTION

VOLS.

Location AG-130 AG-140 AG-301.1 AG-301.2 AG-303 Tahle AHA-l AI-Wl AI-101(h)(6) AI-I02(h)(12) AI-IlO AM-I00 AM-101 AM-105.1(a) AM-201.4 AM-201.4(c) AM-202 AM-203.2

AM-203.2(b)(2) AM-204 AM-213 Tahle AM-214.1 Tahle AM-214.2 Fig. AM-218.l AM-218.2(a)(2) AM-31 1.2 AM-600 Tahle AMG-l Appendix I, Tahle 1-220 Appendix 3, 3-320 Appendix 4, 4-112 Appendix 4, 4-112(a) Appendix 4, 4-112(m) Appendix 4, Tab1e 4-120.1 Appendix 4, Fig. 4-130.1

Appendix 4, 4-134 Appendix 4, 4-136.7 Appendix 4, 4-136.7(a) Appendix 4, 4-136.7(b) Appendix 4, 4-140 Appendix 5, 5-110.3(a) Appendix 8, 8-120(b)

VIII-2-83-04 Vl1I-2-89-21 VIII-2-86-04 VIII-2-89-09 VIII-2-01-14 VIII-2-98-08 VIII-2-86-03 VIII-2-83-04 VIII-2-98-16 VIII-2-92-14 VIII-2-86-05 VIII-2-92-14 VIII-2-95-15 VIII-2-98-17 VIII-2-83-27 VIII-2-86-12 Vl1I-2-98-05 VIII-2-92-18 VIII-2-83-37 VIII-2-86-09 VIII-2-86-10 VIII-2-89-11 VIII-2-98-04 VIII-2-01-06 VIII-2-83-41 VIII-2-83-0l VIII-2-86-03 VIII-2-83-10 VIII-2-83-10 Vl1I-2-83-34 VIII-2-98-11 VIII-2-98-18 VIII-2-95-15 VIII-2-83-09 VIII-2-95-04 VIII-2-01-04 VIII-2-01-08 VIII-2-83-07 VIII-2-83-38 VIII-2-04-10 VIII-2-83-35R Vl1I-2-83-35R-2 VIII-2-83-13 VIII-2-83-16 VIII-2-86-15 VIII-2-83-35 VIII-2-04-09 VIII-2-01-0S VIII-2-04-06 VIII-2-86-01 VIII-2-86-01R VIII-2-01-04 VIII-2-83-07 VIII-2-98-10

BC82-548 BC90-775

BC02-3285 BC98-229 BC85-145 BC82-548 BC99-496 BC93-590 BC86-230 BC96-306 BCOO-288 BC83-266 BC87-026 BC98-051 BC94-278 BC83-687A BC87-065 BC87-066 BC89-412 BC98-052 BCOl-217 BC84-339 BC81-362 BC85-145 BC83-0n BC83-0n BC83-652A BC98-086 BC98-366 BC96-306 BC82-861 BC94-S02 BCOl-195 BC01-380 BC82-680 BC83-644 BCOS-680 BC83-653* BC83-653** BC81-717 BC82-584 BC85-288 BC83-653 BC05-678 BCOI-206 BC03-773 BC85-218 BC85-218* BCOl-195 BC82-680 BC98-049

6 122 66 103 251 213 65 6 231 153 66 153 190 231 27 79 207 160 38 n n 109 207 237 46 5 65 14 14 36 219 231 190 13 171 236 238 8 38 268 45 45 15 16 80 36 267 236 264 59 65 236 8 214

Appendix 9, 9-103 Appendix 9, 9-320 11 Appendix 18

Appendix 20,20-230 Tahle AQT-l AR-200(b) AR-230(d) Artiele 4-3 Alticle D-Il Article F-8 Artiele T AS-I00 AS-110 AS-120 AS-130 AS-130(a) AS-201

AS-204 AS-310(a) AS-320(a) AT-1l2 AT-l13 AT-l AT-200(b) AT-201(a), (h) AT-202(a) AT-202(h) AT-202.3(h) AT-203

AT-203(a) AT-203(b) AT-300 AT-355 AT-51O Code Case 1961 Code Case 1986-2 Code Case 2211 Code Case 2235 Foreword Interpretation statement

(b)

No. Vl1I-2-83-02 VIII-2-89-24 VIII-2-83-44R VIII-2-86-07 VIII-2-83-25 VIII-2-92-16 VIII-2-98-12 VIII-2-86-06 Vl1I-2-86-08 Vl1I-2-83-23 VIII-2-83-12 VIII-2-95-08 VIII-2-83-11 Vl1I-2-83-42 VIII-2-83-32 VIII-2-83-34 VIII-2-04-08 VIII-2-95-02 VIII-2-95-16 VIII-2-95-16 VIII-2-95-02 VIII-2-95-12 VIII-2-95-13 VIII-2-95-13R VIII-2-92-16 VIII-2-92-08 VIII-2-01-02 VIII-2-86-16 VIII-2-92-18 VIII-2-95-07 VIII-2-95-06 VIII-2-01-03 VIII-2-95-10 VIII-2-83-34 VIII-2-89-22 VIII-2-01-0l VIII-2-89-08 VIII-2-92-04 VIII-2-92-17 VIII-2-89-20 VIII-2-92-07 VIII-2-92-15 VIII-2-83-10 VIII-2-92-02 VIII-2-01-15 VIII-2-95-14 VIII-2-86-14 VIII-2-89-06 VIII-2-01-13 VIII-2-98-09 VIII-2-95-04 VIII-2-95-17

BC82-409 BC91-106 BC77-70l* BC86-082 BC82-754B BC94-059 BC98-307 BC86-377 BC86-376 BC81-576 BC81-583 BC91-445 BC80-526 BC84-334 BC83-641 BC83-652A BC03-1819 BC92-382A BC96-537 BC96-537 BC92-382A BC95-465B BC96-128 BC96-128* BC94-059 BC92-295 BCOI-I02 BC86-105 BC94-278 BC95-316 BC95-217 BCOl-190 BC96-127 BC83-6S2A BC90-341 BCOI-097 BCOl-190 BC89-288 BCn-050 BC94-107 BC90-862 BC92-221 BC93-629 BC83-0n BC91-514 BCOl-774 BC96-377 BC87-195 BC89-112 BC99-084 BC98-327 BC94-502 BC96-134

No. 5 123 53 71 26 159 219 71 71 25 15 183 14 51 35 36 267 165 195 195 165 189 189 201 159 141 235 85 160 177 177 235 184 36 122 235 103 135 159 122 141 14 129 255 190 79 97 247 213 171 201

SECTION

INTERPRETATIONS

No, use of ASME marking field fabrication restamping Stresses categories design stress intensity

limits

thermal bending stress Stress Theory, Maximum Shear operating loads

primary p1us secondary principa1 stresses

Test Gages Calibration

VIII-2-92-05 VIII-2-95-16 VIII-2-83-04 VIII-2-86-13

BC92-152 BC96-537 BC82-548 BC87-199

File

No. 135 195 6 79

VIII-2-83-26 VIII-2-83-16 VIII-2-S3-09 VIII-2-86-01R VIII-2-86-14 VIII-2-89-02 VIII-2-89-05 VIII-2-98-02 VIII-2-01-04 VIII-2-01-12 VIII-2-83-22 VIII-2-83-35R VIII-2-83-35R-2 VIII-2-04-06

BC83-221 BC82-584 BCS2-861 BC85-218 BC87-195 BC87-298 BC89-008 BC97-511 BCOI-195 BCOl-822 BC83-245 BC83-653* BC83-653** BC03-773

VIII-2-83-07

BC82-680

VIII-2-83-13 VIII-2-83-26 VIII-2-S3-35R VIII-2-S3-35R-2 VIII-2-01-0S VIII-2-04-10 VIII-2-01-05

BC81-717 BC83-221 BC83-653* BCS3-653** BCOl-380 BC05-680 BC80-526 BCOl-206

15 27 45 45 238 268 14 236

VIII-2-95-14

BC96-377

190

VIII-2-95-07

BC95-316

177

VIII-2-83-37

BC83-687A

flame cut flat heads forgings in lieu of radiography

27 16 13 65 79 91 97 202 236 243 25 45 45 264

straight beam Vessel

Weld Categories Welding buttering continuous electroslag equipment calibration nozzles packed joints procedures

8

repair strength of weld metal testing tube-to-tubesheet joints

BC84-339 BC87-065 BC87-066 BC89-412 BC86-376 BCOl-217 BC82-513 BC98-327 BCS6-377

46 72 72 109 7l 237 6 213 71

VIII-2-89-19

BC90-652

121

VIII-2-89-24

BC91-106

123

VIII-2-83-33

BC80-606

35

VIII-2-83-21 VIII-2-83-14 VIII-2-83-30R VIII-2-83-17 VIII-2-01-15 VIII-2-83-46 VIII-2-83-34 VIII-2-89-10 VIII-2-92-09 VIII-2-92-10 VIII-2-92-17 VIII-2-01-03 VIII-2-83-06 VIII-2-83-23 VIII-2-89-12 VIII-2-89-04 VIII-2-98-07 VIII-2-01-11

BC83-197 BC82-208 BC83-540* BCSO-038C BCOI-774 BC85-194 BCS3-652A BCS9-399 BC92-349 BC92-109 BC94-107 BCOl-190 BC81-656 BC81-576 BC88-426C BC88-213 BC98-228 BCOl-792 BC83-540* BC83-652

weld overlay ang1e beam

VIII-2-83-34

38

(e)

No,

(Cont'd) VIII-2-S3-41 VIII-2-86-09 VIII-2-86-10 VIII-2-89-11 VIII-2-86-08 VIII-2-01-06 VIII-2-83-03 VIII-2-98-09 VIII-2-S6-06

24 16 51 17 255 54 36 109 141 142 159 235 7 25 109 92 213 243 36

ISBN-13: 978-0-7918-3069-7 ISBN-10: 0-7918-3069-1

9 780791 830697

U00082