Asme Viii d Table 2a - Rectifie

7/24/2019 Asme Viii d Table 2a - Rectifie

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Product FormSelect first TABLE2Athe ProductForm before FERROUS MATERIALS AT DESIGN TEMPERATUlooking for (Materials Permitted on ASME Sec !III"2 Onl#$

the materialspecification. ASME 2%%& Allowab

Design TemperaturePlate 60 140 Stress

Nominal Composition " 1#" Ni

TensileSpec No T$pe#%rade Allo$ Design # &NS 'ieldSA("0) A *"1+0)AS , -ocator Applic.

Addenda Page -ine Class # Cond # Tempe -imits on Sect"36 1 -imits on Sec.

Applicable Notes ,/t.C!art.No. CS("

SC5 -- D 7N to 8iew Notes or use 9F2ND9 :Ctrl.;F< command in 9,D2T9 menu.%eneral Notes

(a) The following abbreviations are used: Applic., Applicability; Cond., Condition; Desig., Designati

MA'IMUM ALLO ABLE STRESS !ALUES S FO

oC oF

PlateForgingsPipe

Tube

FittingBar

Cast


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5emar=s>

RE

le Stress at Design Temp.=si pa

"0.?6 14).?"46 1466.61

in. Strengt!=si pa6@ 44?.1@3" 4 @+0)+ "@@.106 " 601

a/. Temp. deg.F # NPion 222 NP

222(" )00Tic= in P(No. %(No.

3A 1

on; Smls., Seamless; and ld., elded.

=g#cm "

=g#cm "


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Notes Group Addenda note_abrv note_textGeneral Note (a) The following abbreviations are usGeneral *e+uire ents G, -aterial that !onfor s to Class ,.#General *e+uire ents G0 -aterial that !onfor s to Class ,,General *e+uire ents G/ -aterial that !onfor s to Class ,,General *e+uire ents G1 -aterial that !onfor s to Class ,,

General *e+uire ents ., G2 """General *e+uire ents G5General *e+uire ents G6 &ue to the relativel$ low $ield streGeneral *e+uire ents G>General *e+uire ents G8General *e+uire ents G,.General *e+uire ents G,,General *e+uire ents G,0General *e+uire ents G,/ The '$ values of this aterial var$General *e+uire ents G,1 A +ualit$ fa!tor of .">2 has been aGeneral *e+uire ents G,2 ? pa!t testing in a!!ordan!e withGeneral *e+uire ents G,5 G=0,,.(b) of 'e!tion ??? is andatGeneral *e+uire ents G,6 These stress intensit$ values shallGeneral *e+uire ents G,>General *e+uire ents G,8 The tensile strength shall not be inGeneral *e+uire ents G0. All forgings shall have a axi uGeneral *e+uire ents G0, For 'e!tion D??? appli!ations# 'A=60General *e+uire ents G00 Fabri!ated fro 'A=/>6 Grade ,0General *e+uire ents G0/ Fabri!ated fro 'A=/>6 Grade ,0General *e+uire ents G01 'ee Appendix 05 of 'e!tion D???# &iEeat Treat ent *e+uire ents E, Annealed"Eeat Treat ent *e+uire ents E0 Nor ali ed and te pered"

Eeat Treat ent *e+uire ents E/ uen!hed and te pered"Eeat Treat ent *e+uire ents E1 i+uid +uen!hed and te pered"Eeat Treat ent *e+uire ents E2 Nor ali ed# nor ali ed and te pEeat Treat ent *e+uire ents E5Eeat Treat ent *e+uire ents E6'i e *e+uire ents ', The axi u thi!3ness of forging'i e *e+uire ents '0 The axi u se!tion thi!3ness s'i e *e+uire ents '/ Both NP' > and larger# and s!hedu'i e *e+uire ents '1 The ini u thi!3ness of pressur

elding *e+uire ents , Not for welded !onstru!tion"elding *e+uire ents 0 For 'e!tion D??? appli!ations# weldielding *e+uire ents / Nonwelded# or welded if the tensilelding *e+uire ents 1 elded# with the tensile strengthelding *e+uire ents 2elding *e+uire ents 5 For 'e!tion D??? appli!ations# 'e!ti

'A=60/ shall not be used for ini

This aterial has redu!ed toughne The stress=rupture test is not re+uiAt te peratures over ,... oF# thesFor te peratures above ,... oF# t

These stress intensit$ values at te

This steel a$ be expe!ted to dev

Nor ali ed at ,8..=0... oF and teFor 'e!tion ??? appli!ations (if an$)#

?n welded !onstru!tion# for te per


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erature% and ld"# elded"

he short ti e tensile properties govern to per it the use of these allo$s where slightl$ grea

i e of the steel"

rdness nu bers shall not be ore than ,.7 below or 027 above the nu ber !orresponding

te pered forgings"

es of welding# as allowed in Part AF"

his aterial" These variables shall be applied in a!!ordan!e with the rules for welding of Par

pends on !o position# heat treat ent# ti e# and te perature" The lowest te perature of !

le onl$ when stresses above >.. oF are published"g to a ini u te perature of ,8.. oF and +uen!hing in water or rapidl$ !ooling b$ othereel has a predo inant grain si e not ner than A'T- No" 5" This note is appli!able onl$ whe

No" ,.E Gr" , aterials# exposure to te peratures in the range of ,,.. oF to ,6.. oF for relat

2. oF for a period of ti e not to ex!eed ,. in at te perature# followed b$ rapid !ooling" For


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er defor ation is a!!eptable" The stress values in this range ex!eed 55 04/7 but do not ex!

to the tensile strength"

AF"

n!ern is about 2.. oF" 'ee Appendix 5# 5=/5."

eans" This note is appli!able onl$ when stresses above >.. oF are published"stresses above >.. oF are published"

ivel$ short periods of ti e a$ result in severe loss of du!tilit$ due to sig a for ation% see

'e!tion D??? appli!ations involving !onsideration of heat treat ent after for ing or welding#


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ed 8.7 of the $ield strength at te perature" 9se of these stresses a$ result in di ensional

5=/1. and 5=/5."

ee Table AF=1.0", for P=No" ,.I# Group No" , aterials"


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l !hanges due to per anent strain" These stress values are not re!o ended for the :ange


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of gas3et ;oints or other appli!ations where slight a ounts of distortion !an !ause lea3age


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r alfun!tion" Table


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lues shown in Table


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anent strain"

Asme Viii d Table 2a - Rectifie

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