2024年4月22日发(作者:google香港)
Designation:E1457
−
13
StandardTestMethodfor
MeasurementofCreepCrackGrowthTimesandRatesin
Metals
1
ThisstandardisissuedunderthefixeddesignationE1457;thenumberimmediatelyfollowingthedesignationindicatestheyearof
originaladoptionor,inthecaseofrevision,rinparenthesesindicatestheyearoflastreapproval.A
superscriptepsilon(´)indicatesaneditorialchangesincethelastrevisionorreapproval.
1.1Thistestmethodcoversthedeterminationoftimefora
creepcracktogrowoninitialload(CCI)anditssubsequent
creepcrackgrowth(CCG)ratesinmetalsatelevatedtempera-
turesusingpre-crackedspecimenssubjectedtoelevatedtem-
testsarevalidatedforeitherbasematerial(homogenous
properties)ormixedbase/weldmaterialwithinhomogeneous
thetime(CCI),
t
0.2
toaninitialcrackextensionδa
i
=0.2mmfromtheonsetof
firstappliedforceandCCGrate,a˙orda/dtareexpressedin
termsofthemagnitudeofcreepcrackgrowthrelating
parameters,C**definedasthesteadystate
determinationofthecracktipstressesderivedinprincipalfrom
C*(t)andC
t
(1-14).
2
Thecrackgrowthderivedinthismanner
isidentifiedasamaterialpropertywhichcanbeusedin
modelingandlifeassessmentmethods(15-25).
1.1.1Thechoiceofthecrackgrowthcorrelatingparameter
C*,C*(t),C
t
,orKdependsonthematerialcreepproperties,
esofmaterial
behavioraregenerallyobservedduringcreepcrackgrowth
tests;creep-ductile(
1-14)andcreep-brittle(26-37).Increep
ductilematerials,wherecreepstrainsdominateandcreepcrack
growthisaccompaniedbysubstantialtime-dependentcreep
strainsatthecracktip,thecrackgrowthrateiscorrelatedby
thesteadystatedefinitionsofC
t
orC*(t),definedasC*(see
1.1.4).Increep-brittlematerials,creepcrackgrowthoccursat
uently,thetime-dependentcreep
strainsarecomparabletoordominatedbyaccompanying
uchsteadystate
creep-brittleconditions,C
t
orKcouldbechosenasthe
correlatingparameter(8-14).
1.1.2Inanyonetest,tworegionsofcrackgrowthbehavior
maybepresent(9,10).Theinitialtransientregionwhere
ThistestmethodisunderthejurisdictionofASTMCommitteeE08onFatigue
andFractureandisthedirectresponsibilityofSubcommitteeE08.06onCrack
GrowthBehavior.
CurrenteditionapprovedFeb.1,ally
eviouseditionapprovedin2000asE1457–07
ε4
.DOI:
10.1520/E1457-13.
2
Theboldfacenumbersinparenthesesrefertothelistofreferencesattheendof
thisstandard.
1
elasticstrainsdominateandcreepdamagedevelopsandinthe
steadystateregionwherecrackgrowsproportionallytotime.
Steady-statecreepcrackgrowthratebehavioriscoveredby
tionspecificrecommendationsaremade
in
11.7astohowthetransientregionshouldbetreatedinterms
steadystate,aunique
correlationexistsbetweenda/dtandtheappropriatecrack
growthraterelatingparameter.
1.1.3Increepductilematerials,extensivecreepoccurs
whentheentireun-crackedligamentundergoescreepdefor-
nditionsaredistinctfromtheconditionsof
small-scalecreepandtransitioncreep(
1-7).Inthecaseof
extensivecreep,theregiondominatedbycreepdeformationis
significantinsizeincomparisontoboththecracklengthand
l-scale-creeponlyasmall
regionoftheun-crackedligamentlocaltothecracktip
experiencescreepdeformation.
1.1.4Thecreepcrackgrowthrateintheextensivecreep
regioniscorrelatedbytheC*(t)-
t
parameter
correlatesthecreepcrackgrowthrateinthesmall-scalecreep
andthetransitioncreepregionsandreduces,bydefinition,to
C*(t)intheextensivecreepregion(
5).Henceinthisdocument
thedefinitionC*isusedastherelevantparameterinthesteady
stateextensivecreepregimewhereasC*(t)and/orC
t
arethe
parameterswhichdescribetheinstantaneousstressstatefrom
thesmallscalecreep,transientandthesteadystateregimesin
ommendedfunctionstoderiveC*forthe
differentgeometriesisshownin
AnnexA1isdescribedin
AnnexA2.
1.1.5Anengineeringdefinitionofaninitialcrackextension
sizeδa
i
isusedinordertoquantifytheinitialperiodofcrack
een
shown(
38-40)thatthisinitialperiodwhichexistsatthestartof
thisearlyperiodthecracktipundergoesdamagedevelopment
aswellasredistributionofstressespriorreachingsteadystate.
Recommendationismadetocorrelatethisinitialcrackgrowth
perioddefinedast
0.2
atδa
i
=0.2mmwiththesteadystateC*
whenthecracktipisunderextensivecreepandwithKfor
uesforC*andKshouldbe
calculatedatthefinalspecifiedcracksizedefinedasa
o
+δa
i
wherea
o
initialsizeofthestartercrack.
Copyright©ASTMInternational,100BarrHarborDrive,POBoxC700,WestConshohocken,States
Copyright by ASTM Int'l (all rights reserved); Tue Jun 10 22:37:10 EDT 2014
1
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E1457−13
ingthe
tensileresidualstresseffectintoaccountwillproduceC*
valueslowerthanexpectedeffectivelyproducingafaster
crackingratewithrespecttoaconstantC*.Thiswouldproduce
conservativeestimatesforlifeassessmentandnon-
ldalsobe
notedthatdistortionduringspecimenmachiningcanalso
indicatethepresenceofresidualstresses.
1.1.9Stressrelaxationoftheresidualstressesduetocreep
andcrackextensionshouldalsobetakenintoconsideration.
Nospecificallowanceisincludedinthisstandardfordealing
rthemethodofcalculatingC*
presentedinthisdocumentwhichusedthespecimen’screep
displacementratetoestimateC*inherentlytakesintoaccount
theeffectsdescribedaboveasreflectedbytheinstantaneous
rextracaution
shouldstillbeobservedwiththeanalysisofthesetypesoftests
asthecorrelatingparametersKandC*shownin
AnnexA2
eventhoughitisexpectedthatstressrelaxationathigh
temperaturescouldinpartnegatetheeffectsduetoresidual
4presentsthecorrectcalculationsneededto
deriveJandC*forweldmenttestswhereamiss-matchfactor
needstobetakenintoaccount.
1.1.10Specimenconfigurationsandsizesotherthanthose
listedinTableA1.1whicharetestedunderconstantforcewill
donebycompar-
ingdatafromrecommendedtestconfiheless,
useofothergeometriesareapplicablebythismethodprovided
dataarecomparedtodataobtainedfromstandardspecimens
(asidentifiedinTableA1.1)andtheappropriatecorrelating
parametershavebeenvalidated.
1.2ThevaluesstatedinSIunitsaretoberegardedasthe
h-poundunitsgiveninparenthesesarefor
informationonly.
1.3Thisstandarddoesnotpurporttoaddressallofthe
safetyconcerns,ifany,e
responsibilityoftheuserofthisstandardtoestablishappro-
priatesafetyandhealthpracticesanddeterminetheapplica-
bilityofregulatorylimitationspriortouse.
ncedDocuments
2.1ASTMStandards:
3
E4PracticesforForceVerificationofTestingMachines
E74PracticeofCalibrationofForce-MeasuringInstruments
forVerifyingtheForceIndicationofTestingMachines
E83PracticeforVerificationandClassificationofExten-
someterSystems
E139TestMethodsforConductingCreep,Creep-Rupture,
andStress-RuptureTestsofMetallicMaterials
E220TestMethodforCalibrationofThermocouplesBy
ComparisonTechniques
E399TestMethodforLinear-ElasticPlane-StrainFracture
ToughnessK
Ic
ofMetallicMaterials
ForreferencedASTMstandards,visittheASTMwebsite,,or
contactASTMCustomerServiceatservice@ualBookofASTM
Standardsvolumeinformation,refertothestandard’sDocumentSummarypageon
theASTMwebsite.
3
1.1.6TherecommendedspecimensforCCIandCCGtest-
ingisthestandardcompacttensionspecimenC(T)(seeFig.
A1.1
)whichispin-loadedintensionunderconstantloading
vissetupisshownin
Fig.A1.2(see7.2.1for
details).Additionalgeometrieswhicharevalidfortestingin
thisprocedureareshownin
retheC-ringin
tensionCS(T),middletensionM(T),singlenotchtension
SEN(T),singlenotchbendSEN(B),anddoubleedgenotch
bendtensionDEN(T).In
Fig.A1.3,thespecimens’side-
grooving-positionformeasuringdisplacementattheforce-line
(FLD)crackmouthopeningdisplacement(CMOD)andalso
andpositionsforthepotentialdrop(PD)inputandoutputleads
endedloadingforthetensionspecimensis
figurations,sizerangeandinitialcrack
sizeandtheirextentofside-groovingaregivenin
TableA1.1
ofAnnexA1,(40-44).Specimenselectionwillbediscussedin
5.9.
1.1.7Thestate-of-stressatthecracktipmayhavean
influenceonthecreepcrackgrowthbehaviorandcancause
ensize,
geometry,cracklength,testdurationandcreeppropertieswill
affectthestate-of-stressatthecracktipandareimportant
mendedsize
rangeoftestspecimensandtheirside-groovingaregivenin
eenshownthatforthisrange
thecrackingratesdonotvaryforarangeofmaterialsand
loadingconditions(
40-44).Suggestingthatthelevelof
constraint,fortherelativelyshorttermtestdurations(lessthan
oneyear),doesnotvarywithintherangeofnormaldatascatter
ritisrecom-
mendedthat,withinthelimitationsimposedonthelaboratory,
thattestsareperformedondifferentgeometries,specimensize,
asesacomparisonof
thedatafromtheaboveshouldbemadebytestingthestandard
C(T)earthatincreased
confidenceinthematerialscrackgrowthdatacanbeproduced
bytestingawiderrangeofspecimentypesandconditionsas
describedabove.
1.1.8Materialinhomogeneities,residualstressesandmate-
rialdegradationattemperature,specimengeometryandlow-
forcelongdurationtests(mainlygreaterthatoneyear)can
influencetherateofcrackinitiationandgrowthproperties
(
39-47).Incaseswhereresidualstressesexist,theeffectcanbe
significantwhentestspecimensaretakenfrommaterialthat
characteristicallyembodiesresidualstressfieldsorthedam-
agedmaterial,mpleweldments,orthickcast,
forged,extruded,components,plasticallybentcomponentsand
complexcomponentshapes,oracombinationthereof,where
enstakenfromsuch
componentthatcontainresidualstressesmaylikewisecontain
residualstresseswhichmayhavealteredintheirextentand
tionofspeci-
mensinitselfpartiallyrelievesandredistributestheresidual
stresspattern;however,theremainingmagnitudecouldstill
causesignificanteffectsintheensuingtestunlesspost-weld
heattreatment(PWHT)iseresidual
stressesaresuperimposedonappliedstressandresultsin
crack-tipstressintensitythatisdifferentfromthatbasedsolely
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2
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