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Quian Lippold 2003 Liquation Phenomena in the Simulated

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Liquation Phenomena in the Simulated Heat- Affected Zone of Alloy 71 8 after Multiple Postweld HeIat Treatment Cycles Delta-phase formation increases liquation cracking susceptibility BY M. QIAN AND J. C. LIPPOLD ABSTRACT. Long-term isothermal solu- tion heat treatments were conducted to simulate multiple weld repair/postweld heat treatment cycles in Alloy 718 wrought plate. These heat treatments re- sulted in extensive precipitation of needle- and plate-shaped 8 phase in the y-nickel matrix. 8-phase accumulation represents the principal metallurgical damage from simulated multiple repair/postweld heat treatment cycles in Alloy 718. Grain size did not increase during this exposure due to the grain boundary pinning effect of the 8 phase. Simulated weld heat-affected zone thermal cycles resulted in a variety of microstructural changes to the heat treated material, including 5-phase disso- lution-promoted liquation, boron carbide constitutional liquation, and segregation- induced grain boundary liquation. The ef- fect of these liquation phenomena on the weldability degradation of Alloy 718 is dis- cussed. Introduction Weld repair of aircraft gas turbine en- gine components has become increasingly prevalent as a means of extending engine life and reducing the costs associated with component replacement. As part of the repair welding process, the precipitation- hardened superalloys must undergo post- weld heat treatment (PWI-IT) to restore their mechanical properties. Because components are subject to multiple re- pairs over their lifetimes, they will also be exposed to multiple cycles of PWHT. It has been observed that the weldability of some superalloys degrades after an accu- mulation of repair/PWHT cycles (Refs. 1-5), making further repair difficult. Heat-affected zone (HAZ) liquation cracking is the root cause of this difficulty, which occurs in the partially melted region of the HAZ. Such cracking has been M QlANandJ. C LIPPOLD are wvith thle Weld- ing and Joining Metallurg Group at The Ohlio State University Coluimbus, Oltio. shown to be associated with local or par- tial melting of grain boundaries, causing a short time high temperature grain bound- ary (GB) weakening (Ref. 6). Preliminary investigations on the effect of multiple PWHT cycles on repair weldability have been conducted for Alloy 718 (Refs. 2-5, 7). A direct result of the multiple PWHT is the accumulated, abundant 8-phase (Ni 3 Nb, orthorhombic) precipitation in the nickel matrix, constituting the metal- lurgical "damage" that degrades the weld- ability of Alloy 718. The 8-phase dissolu- tion during weld thermal cycles was reported to be a factor resulting in grain boundary liquation (Ref 7) by promoting GB segregation of Nb, a melting point de- pressant (Ref 1). The purpose of this paper is to elucidate the effect of liquation phenomena on the weldability degrada- tion in the Alloy 718 due to multiple re- pair/PWHT cycles. Experimental Procedure The material used in this study was Alloy 718 in the form of wrought plate. The composition of this material, based upon an independent analysis, is shown in Table 1. The plate microstructure in the as-received condition is shown in Fig. 1. There are fine deformed grains surround- ing the "normal" grains and some 8 phase is present in the y-nickel matrix. Simula- tion of multiple PWHT cycles was accom- plished through metallurgical-equivalent long-term isothermal heat treatments. This technique had previously been shown to yield microstructures and properties similar to those achieved through multiple thermal cycles for equivalent times (Ref 6). A normal PWHT for Alloy 718 would be 954°C for 0.5-2 h. wvo isothermal treatments were performed to simulate multiple PWHT cycles: 954°C/40 h and 954°C/100 h. The isothermal treatments were conducted in air in a box furnace with air cooling. Subsequently, Gleeble hot ductility specimens were machined from the bulk materials after heat treatment. Gleeble hot ductility testing was con- ducted to evaluate and compare the sus- ceptibility of Alloy 718 to HAZ liquation cracking in three different conditions: 1) as-received, 2) 954°C/40 h, and 3) 954°C/100 h. The specimens are 6.35 mm in diameter, 100 mm in length, taken lon- gitudinally along the rolling direction in the plate. The hot ductility testing follows conventional procedures as have been re- ported previously (Refs. 2-7). A heating rate of 111°C/s, hold time at test tempera- ture of 0.5 s, cooling rate of 43°C/s (for on- cooling tests), and stroke rate of 25 mm/s were used. All testing was conducted under an argon atmosphere. Figure 2 schematically shows the procedure for de- termining critical values of nil-strength temperature (NST), nil-ductility tempera- ture (NDT), and ductility-recovery tem- perature (DRT). Initially, the nil-strength temperature (NST) was determined by heating the specimen under a small static load (approximate 10 kg) until failure oc- curred. On-heating hot ductility tests were conducted by heating samples to various test temperatures, and pulling them to failure at the stroke rate reported, until NDT was achieved. On-cooling tests were performed after heating to a peak tem- perature (Tp) between the NDT and NST, and then cooling to a desired temperature, and pulling to failure to identify the DRT Metallographic samples were exam- ined using both an optical microscope and a Phillips XL-30 scanning electron micro- scope (SEM) equipped with an energy- dispersive spectrometer (EDS). Elec- trolytic etching with 10% aqueous chromic acid was generally used to reveal I WELDING JOURNAL KEYWORDS Alloy 718 Weld Repair , 5-Phase Precipitation Boron Carbide Constitutional Liquation Liquation Cracking Intergranular Fracture
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LiquationPhenomenainthe SimulatedHeat-AffectedZone of Alloy 71 8after MultiplePostweldHeIatTreatmentCyclesDelta-phaseformation increases liquation cracking susceptibilityBYM. QIANANDJ. C.LIPPOLDABSTRACT.Long-termisothermalsolu-tionheattreatmentswereconductedtosimulatemultipleweldrepair/postweldheattreatmentcyclesinAlloy718wroughtplate.Theseheattreatmentsre-sulted in extensive precipitationof needle-andplate-shaped8 phaseinthey-nickelmatrix.8-phaseaccumulationrepresentstheprincipalmetallurgicaldamagefromsimulatedmultiplerepair/postweldheattreatmentcyclesinAlloy718.Grainsizedid notincreaseduring thisexposuredueto the grain boundary pinning effectof the8phase.Simulatedweldheat-affectedzonethermal cycles resultedin a varietyofmicrostructuralchangestotheheattreatedmaterial,including5-phasedisso-lution-promotedliquation,boroncarbideconstitutionalliquation,andsegregation-induced grainboundary liquation.Theef-fect of these liquationphenomenaontheweldability degradationof Alloy 718 is dis-cussed.IntroductionWeldrepair of aircraftgasturbineen-ginecomponentshasbecome increasinglyprevalentasa meansof extendingenginelifeand reducing the costsassociatedwithcomponentreplacement.Aspartof therepairweldingprocess,the precipitation-hardenedsuperalloysmustundergopost-weldheattreatment(PWI-IT)torestoretheirmechanicalproperties.Becausecomponentsaresubjecttomultiplere-pairs over their lifetimes,they willalso beexposedtomultiplecyclesof PWHT.Ithas beenobservedthat theweldabilityofsomesuperalloysdegradesafteranaccu-mulationof repair/PWHTcycles(Refs.1-5),makingfurtherrepairdifficult.Heat-affectedzone(HAZ)liquationcrackingis the rootcause of thisdifficulty,which occursin the partially melted regionoftheHAZ.SuchcrackinghasbeenM QlANandJ. C LIPPOLD arewviththleWeld-ingand Joining MetallurgGroup atTheOhlioState UniversityColuimbus, Oltio.shownto beassociatedwithlocalorpar-tial melting of grainboundaries,causing ashort time hightemperaturegrain bound-ary(GB) weakening(Ref.6). Preliminaryinvestigationsontheeffectof multiplePWHTcyclesonrepairweldabilityhavebeenconductedfor Alloy 718(Refs.2-5,7).Adirectresultof themultiple PWHTistheaccumulated,abundant8-phase(Ni3Nb,orthorhombic)precipitationinthenickelmatrix,constitutingthemetal-lurgical "damage"that degrades the weld-abilityof Alloy718.The8-phasedissolu-tionduringweldthermalcycleswasreportedto beafactorresultingingrainboundaryliquation(Ref7) by promotingGB segregationof Nb,a melting point de-pressant(Ref1).Thepurposeofthispaper is to elucidate the effectof liquationphenomenaontheweldabilitydegrada-tioninthe Alloy718duetomultiplere-pair/PWHTcycles.ExperimentalProcedureThematerialusedinthisstudywasAlloy718intheformof wroughtplate.Thecompositionofthismaterial,baseduponanindependentanalysis, is shown inTable1. Theplatemicrostructureintheas-receivedconditionisshowninFig.1.There arefinedeformedgrains surround-ing the "normal"grainsand some 8 phaseispresentinthey-nickelmatrix.Simula-tion of multiplePWHT cycles was accom-plishedthroughmetallurgical-equivalentlong-termisothermalheattreatments.This techniquehad previouslybeen showntoyieldmicrostructuresandpropertiessimilar to those achievedthrough multiplethermalcyclesforequivalenttimes(Ref6).A normalPWHT for Alloy718 wouldbe954Cfor0.5-2h.wvoisothermaltreatmentswereperformedtosimulatemultiplePWHTcycles:954C/40hand954C/100h.The isothermaltreatmentswere conductedin air in a box furnace withaircooling.Subsequently,Gleeblehotductilityspecimensweremachinedfromthebulk materialsafter heat treatment.Gleeblehotductilitytestingwascon-ductedto evaluateandcomparethesus-ceptibilityof Alloy 718toHAZ liquationcrackinginthreedifferentconditions:1)as-received,2)954C/40h,and3)954C/100h.The specimensare6.35mmindiameter,100 mm inlength,takenlon-gitudinallyalongtherollingdirectioninthe plate.The hotductilitytesting followsconventionalproceduresashavebeenre-portedpreviously(Refs.2-7).Aheatingrate of 111C/s,hold time attest tempera-ture of 0.5s, coolingrate of 43C/s (for on-coolingtests),andstroke rateof 25mm/swereused.Alltestingwasconductedunderanargonatmosphere.Figure2schematicallyshows the procedure for de-terminingcriticalvaluesof nil-strengthtemperature(NST), nil-ductilitytempera-ture(NDT),andductility-recoverytem-perature(DRT).Initially,thenil-strengthtemperature(NST)wasdeterminedbyheatingthespecimenundera small staticload(approximate10kg)untilfailureoc-curred.On-heating hot ductility tests wereconductedbyheatingsamplestovarioustesttemperatures,andpullingthemtofailureatthestrokeratereported,untilNDT was achieved.On-coolingtests wereperformedafterheatingtoa peaktem-perature(Tp)betweenthe NDT and NST,and then cooling to a desired temperature,and pulling to failure to identifythe DRTMetallographicsampleswereexam-inedusing bothan optical microscopeanda Phillips XL-30 scanningelectronmicro-scope(SEM)equippedwithanenergy-dispersivespectrometer(EDS).Elec-trolyticetchingwith10%aqueouschromic acidwas generallyusedto revealIWELDINGJOURNALKEYWORDSAlloy 718WeldRepair,5-PhasePrecipitationBoronCarbideConstitutionalLiquationLiquationCrackingIntergranularFractureFig. I -Microstructure of as-received Alloy718 base metal:A -distributionoffine deformed grains at grain boundaries;B-short bar-shlapedintra- andiutergranzularSphlase.lhble 1-ChemicalCompositionof Alloy718WroughtPlateElementCrMnCoVAlCTiBMoSiNbSFepWMgCuTaNiwt-%18.420.090.20.0220.50.0331.030.00183.030.15.040.000517.580.0120.0290.0110.150.006BalanceNSTTpNDTDRT'M.-Pull tofailureG)l.DeterminingNST2.On-heating test3.On-coolingtestTimeFig. 2-Schematic of Gleeble hot ductilioy test procedutre.Table 2-The Effectof HeatrreatmentonGrainSizeof Alloy718HT ConditionGrainSize(df)As-received954CC(1750F)/40h954C(1750F)/100h7940.6 lim8327 1tm8331pmmicrostructuresof interest. Grain size wasmeasuredin Feretdiameter(df),ondigi-tally recordedoptical images usingimage-Tool 2.0(Ref.8).Fracturemorphologywasevaluatedonselectedhotductilitysamples by usingSEM.Resultsand DiscussionsThe principalmicrostructuralfeatureinlong-termisothermallytreatedAlloy718isthehighfractionof precipitated8 phaserelativeto thatof theas-receivedmaterial.Theas-receivedbasemetalhadrelativelylittle5 phaseandthesizeofintra-andintergranularbar-shapedophase is comparable-Fig.1. In contrast,thefractionof bothintra-and intergranu-lar(IG)o phase inthe long-term,isother-mally treatedmaterialincreaseddramnati-cally,as shown in Fig. 3. Theintergranularo phase becomesessentiallycontinuousasa resultof the long-termisothermaltreat-ment,and somebar-shapedo phase alongtwin boundariesalso becamecontinuous.Themorphologyoftheintragranularo phase appearsas fine needles that inter-crossedcompactly- Fig.3B.Therewasno evidenceof gammadouble-prime(Y')observedinthisstructuresincetheheattreatmenttemperatureisabovethepre-cipitationrangefor Y' and none wouldbeexpectedtoformuponrapidcoolingtoroomtemperature.Inaddition,therapidformationof the ophase depletesthe ma-trixof niobium,furtherreducingthepos-sibilityof Y'.Thegrainsizeremainedessentiallyconstantafterthelong-termisothermalheat treatmentat 954C, as shown in Table2. Thisis duetothepinning effectof theo phaseongrainboundaries.Thebulkyangularphasesinthenickelmatrix(Fig.3B)arecarbidesthataredistributedasstringersintherollingdirectionof thewrought plate.GleeblehotductilitytestingrevealedHAZliquationcrackingsusceptibilityin-creaseswiththeincreaseinholdtimeat954C,asdeterminedbytheliquationtemperaturerange (LTR), which is the dif-ferencebetween NST and DRT (Table 3).Noticeably,the increaseof LTR is consis-=JUNE 2003- --->beTXtFig. 3-Higl fraction of needle-shiaped intragranularand bulky continuous, intergramnara phasefrom long-temnisothiemial treatment.A-9540C/40 h;B - 954C/100 hi.Fig. 4-8-phase dissolution during simulated HAZtihennal cycles in Alloy718.A- 8-phase "thickening" at NDT of thle as-received material; B-dis-solving s-phase nenvork atNDT of 954'C140 h treated material; C - 8phlase"rounding"at NST of thie as-received material (liquatedboron carbide is indi-cated);D - interconnected cluster of B- and Nb-rich eutectic constituentsfromdissolved 8-phase along grain bounidaries atNST of 954C/100 1h-treatedmaterial.tent with the densityincrease of 8 phase asafunctionof hold timeat 954C.Microstructuralevaluationrevealedthat8-phasedissolution-promotedliqua-tion occursduring the on-heatingthermalcycleandpersists tothe NST8phase hasanorthorhombicstructurewithcomposi-tionof Ni3Nb.In Alloy718, itsprecipita-tiontemperaturerangeisfrom650to1050C(Refs.9,10).6 phase willdissolveabovethe uppertemperaturelimit.Upondissolution,thesurroundingy-nickelma-trix isenrichedinNb,bothintra-andin-tergranularlydependingonthe6-phasedistribution. Since Nb forms two eutecticswithNias(Ni+Ni3Nb)at12820C(23 wt-% Nb)and(Ni3Nb+Ni6Nb7)at1175C(52 wt-% Nb),Nbactsas amelting pointdepressantelementin=Ni(Refs.11,12).WithregardtoAlloy718,itis expectedthatthe dissolutionof5 phase willresultIWELDINGJOURNALAXLJDJItLt7lt;ffi~~Ni 4I__________________Fig. 5-5-phase dissolution gradientin DRTspecimens.A -As-received;B - 954'C1100 h:treated condition (arrowvs indicateeutectic constituentsformedin the cores of original Spitase).Fig.6-Fractograplzyof NDTsamples of as-receivedAlloy718.A -Intergranularfracture;B-detail of Fig.6Ashoving evidence of liquid films and li-quated boron carbides.TIble 3-Resultsof Gleeble HotDuctilityTestingfor Alloy718HT ConditionNDTNSTDRTPeak temp(Tp)LTRT;DRTAs-received1199C1274C1171C1240'C103C- 69C954C/40hl191'C12720C1158C1240*C114C82'C954C/IOh1190'C1276C1149C1240C127C91CinformationofNb-richeutecticcon-stituents,as has beenobservedin thecur-rent research.Figure4showsmicrostructuralevi-denceof8-phasedissolutionandassoci-atedliquation.Thedissolutionof theophaseresultsinNbenrichmentatthegrainboundarythatgivesrisetothedif-ferentetching characteristicof the bound-ary.TheNb-enrichedboundaryvariedasafunctionofthepeaktemperaturereached during the hot ductilitytest and ismanifestedmicrostructurallybydifferentmorphologies.AttheNDT,themi-crostructureappearsas5-phaseneedle"thickening,"asshownintheas-receivedmaterial- Fig.4A. Notethat the "holes"alongtheGBsaresitesof eutectic,5-phasedissolutionproductsthathaveetchedout of the structure.Fracturesur-faceanalysisintheSEMrevealedaddi-tionaldetailsof theliquationprocess,in-cludingapparentconstitutionalliquationof boroncarbides.TypicalintergranularfeaturesareshowninFig.6,whereliquatedparticlesandevidenceofliquidfilmsonthefrac-ture surface canbe seen. Note the angularbutslightlyroundedparticlesandholeswhereparticleshavedroppedoutofthefracturesurface- Fig.6AandB.EDSanalysisrevealedthattheparticlesarecomplex boron carbidescontaining Cr, Ti,andsomeNb.Thepresenceofroundholesaccommodatingtheroundedboroncarbidessuggeststhatboroncarbide-relatedconstitutionalliquationhasoc-curredalongtheGBs.Heatingofthedenselydistributed8phasein954C-treatedsamplestotheNDTproducedmoreextensive,dissolving8 phasenet-works- Fig.4B.As thetesttemperature,wasraised to the NST,5-phasedissolutionbecamemorepronounced.Theonce-thickened,intragranular8-phaseneedlesbegan"rounding"(Fig.4Cand D),indi-catingamoreacceleratedNbdissolutionrate.Someadjacentdissolved5phasenear or alongGBs interconnectedto formB-andNb-richeutecticconstituents-Fig.4D.Theselow-meltingeutecticliq-uidsalongGBswillresultinGBweaken-':JUNE2003lIAT4~~~~k-k'Xtw:~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~tCl;~~~~'Fig.7-Fractograplzyof954C140 1:-treated specimensA-IGfeatulrc at NDT;B -detailof Fig. 7Ashlowing terraced nipple pattemnwitht particles dis-persed at NDT;C-detailoft/ice liquated bomntcarbide; D-terracedripplepattern of liquiadflowv trace atDRT:ing and potentialfailure (cracking)duringthe weldthermalcycle.At the DRT,the microstructuresof as-received718(Fig.5A)didnotchangemuchcomparedwiththatoftheNDTsample(Fig. 4A). However,the Nb disso-lution is more extensive(Fig. 5B) than thatattheNDTsincethissamplehasbeenheatedthroughthepeaktemperature(Tp) during the on-coolingtest. It can alsobeobservedthattinybutdistinguishableeutecticconstituentsformin the center ofthe original 5 phase - Fig. 5B. This is dueto the Nb enrichmentassociatedwiththedissolved5 phase.The center has ahigherconcentrationof Nb,whiletheperipheryhasalowerconcentrationof Nb.Asthehighconcentrationof Nbcorrespondstotheeutecticwithalowermeltingpoint(1175C),liquationstartedpreferentiallyatthecenterwhentemperaturesbecamefavorable.Figure7showsintergranularfractureofthe954C-treatedsamples,butwithmore liquid presentthan seenin Fig. 6fortheas-receivedmaterial.Therearemoreparticlesonthesefracturesurfacesandthe flow pattern of the liquid films is muchmoreevident,appearingasterracedrip-plepatterns.Atthecenterofconcentricripples,aliquatedparticleinaholewasidentifiedasaNb-richboroncarbide,asshowninFig.7BandC.Similarbutsmaller particlescan also be differentiatedinthe samemicrograph.The angularpar-ticleatthe upperrighthasnotliquatedandwasidentifiedasTiC.MoreGBli-quationassociatedwithripplepatternscanbe seen inFig. 7D.Figure8presentssecondaryelectron(SE)andback-scattered-electron(BSE)micrographsthatclearlyshowthe mor-phologyof boroncarbides(lighterbulkyphase)andMCcarbides(darkphases),whereboroncarbidehasapparentlyde-composedfromitsperiphery.Asimilarcasecan beseen in Fig.4C(arrow)andisprobably due to constitutionalliquation.Basedontheaboveresults,itcanbeconcludedthat8-phasedissolution-promotedliquationplaysamajorroleininfluencingthesusceptibilityto liquationcrackinginAlloy718subjectedtolong-termheattreatmentsat954C.Segrega-tion of Band Nb as well asother melting-pointdepressantsalsocontributetothelocalizedmelting of theGB.Interstitialelements,suchasboron,arewellknownto havethepropensitytosegregate to GBs. Nb fromthe dissolutionof 8 phases couldpreferentiallysegregatetoGBthrougheitherdiffusion(Refs.13,14)ora segregationmechanism(Ref.7),by which Nb couldbe swept by mobile GBsoncethe pinning effectof5 phase wasre-ducedbydissolution.Nb-containingboroncarbide liquationalsocontributedto the Nb segregationtoGBs,thoughthisisexpectedtoaccountforonly a small fractionof the liquidpre-sent,sincethefractionof boroncarbidesis much less thanthe 8 phase.In addition,boroncarbideliquationproducesalow-meltingeutectic,anextralowmeltingpointconstituentthatfurtheraggravatestheliquation.Insummary,theeffectofliquationphenomenaon the susceptibilityto liqua-tioncrackingof Alloy718thathasbeenexposedto multiple PWHT cycles that re-sult in a high fractionof 5 phase can be ex-plainedas follows.As thenumber of weldrepaircycles accumulates,8-phase precip-itationbecomes more extensive.Uponre-IWELDINGJOURNAL=YA4L DkkFig. 8-Morphology of boron carbidesand MC carbidesin a DRTspecimen.A-SEMsho)ving rounded 8 phase and associated liquation; B-BSE imagedifferentiatingphasesindle y-nickelmatrix.heatingintheweldHAZ,rapid5-phasedissolutionoccurs.8-phasedissolution-promotedliquation,possiblycombinedwithboroncarbideconstitutionalliqua-tion,results in extensivegrain boundary li-quationthatthenleadstocrackingif re-straintlevelsaresufficient.Thisexplainswhy the buildup of 8 phase in Alloy 718 in-creasesthesusceptibilitytoHIAZliqua-tion as the number of repair/PWHTcyclesincreases.Conclusions1)SimulatedmultiplePWHTcyclesusingequivalentlong-termisothermalheattreatments(954C/40-100h)re-sultedin extensive precipitationof needle-andplate-shapedophaseinthey-nickelmatrix,whichisthemajormetallurgicalchangerelativeto thestarting plate mate-rial.Grain sizedid not change appreciablyduring these heat treatmentsdueto grainboundarypinning by the8phase.2)Gleeblehot ductilitytesting showedweldability(resistancetoI-IAZliquationcracking)of Alloy718 degradedasacon-sequenceofthesimulatedmultiplePWI-ITcycles.3)Thedegradationof weldabilityre-sultsfromgrainboundaryliquationre-sulting primarilyfromthe 8-phase dissolu-tion andassociated Nbenrichmentof thegrainboundary.Constitutionalliquationof boron-richcarbideswasalsoobservedand maycontributeto the grain boundaryliquation.AcknowledgmentTheauthorswishtothankEdisonWeldingInstituteforsupportingthisre-search.References1. Chou, C. P.,andChao,C. H. 1988. Repairweldabilitystudiesof Alloy718 using versatilevarestrainttest.Superalloys 1988.Champion,Pa.:TheMetallurgicalSociety/AIME,18-22Sept.,pp.785-794.2.Lippold,J.C.,Mehl,M., Lu,Q.,Lin,W,and Kelly,T J.1996.Effect of composition,mi-crostructure,andthermaltreatmentonthere-pair weldabilityof Alloy 718.American WeldingSociety77th AnnuialA WSConventionAbstracts(USA).pp.124-125.3. Hooijmans,J.W, Lippold.J.C., and Lin,W1997. Effectof multiple postweldheat treat-mentonthe weldabilityofAlloy718.Superal-loys 718, 625,706 and Various Derivatives. Pitts-burgh,Pa.:Minerals,MetalsandMaterialsSociety/AIME(USA).pp.721-730.4. Mehl,M.E.,and Lippold,J.C. 1997.Ef-fectof 8-phaseprecipitationon therepair weld-abilityofAlloy718.Superalloys718,625,706and VariousDerivatives. Pittsburgh, Pa.:Miner-als,MetalsandMaterialsSociety/AIME(USA), June15-18, pp.731-741.5. Bowers,R. J.,and Lippold, J.C. 1997.Ef-fectof compositionandheattreatmentcyclesonthe repairweldabilityof Alloy718.Joiningand Repair of Gas Turbine Components.Indi-anapolis,Ind.:ASMInternational(USA),Sept.,pp. 41-50.J6. Qian,M.,2001.AnInvestigationoftheRepairWeldability of Waspaloyand Alloy718.Ph.D.dissertation, TheOhio State University.7.Lu,Q.1999.HIAZMicrostructrualEvo-lutionin Alloy 718 MultipleRepair andPWHTCycles.Ph.D. dissertation, The Ohio State Uni-versity.8. lmageTool programdeveloped at the Uni-versityof TexasHealthScienceCenteratSanAntonio,Tex.,andavailablefromtheInternetbyanonymousFTPfromftp:llinaxrad6.uth-scsa.edu.9.Brown,E.E.,andMuzyka,D.R.1997.Nickel-ironalloys.SuperalloyslL.Ed. C.T. Sims,N. S. Stoloff,and W. C. H-Iagel.New York,N.Y.:John Wiley& Sons,pp.165-188.10.Liu,W.C.,Yao,M.,Chen,Z.L.,andWang,S. G.1999.NiobiumsegregationinIn-conel718.Joumal of Materials Science(UK).Vol.34,No.11,pp.2583-86.11.Duerden,1. J.,andHume-Rothery,W.1966.Theequilibriumdiagramofthesystemniobium-nickel.Jourmal of theLess-CommonMetals.Vol. 11,p.381.12. Zeng, K.,Zeng, X. Z., and Jin, Z. P. 1992.AthermodynamiccalculationoftheNi-Nbphasediagram.Journal of Alloysand Comn-pounds.Vol.179,pp.177-185.13. Boucher,C., Varela, D., Dadian, M., andGranjon,H.1976.HotcrackingandrecentprogressintheweldabilityofthenickelalloysInconel 718 and Waspaloy. Revue de Metallurge.Vol.73,pp.817-831.14.Vincent,R.1985.Precipitationaroundweldsin the nickel-basesuperalloy Inconel 718.Acta Metalllurgica. Vol.33,pp.1205-16.MJUNE2003IREPRINTSREPRINTSToorder custom reprintsofarticlesinWelding JournalContact DenisMulliganat(800)259-0470FAX:(717)481-7677or viae-mailatinfo @reprintdept.comREPRINTSREPRINTSCOPYRIGHTINFORMATIONTITLE: LiquationPhenomenaintheSimulatedHeat-AffectedZoneofAlloy718afterMultiplePostweldHeatTreatmentCyclesSOURCE: WeldJ82no6Je2003WN: 0315200146016Themagazinepublisheristhecopyrightholderofthisarticleanditisreproducedwithpermission.Furtherreproductionofthisarticleinviolationofthecopyrightisprohibited.Copyright1982-2003TheH.W.WilsonCompany.Allrightsreserved.


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