Oxidation Resistant Porous Material For Transpiration Cooled Vanes

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N A S A C O N T R A C T O OR TRANSPIRATION COOLED VANESby Per Mddsen and Robert M. RusnakPrepared byTHE BENDIX CORPORATIONMadison Heights,Mich.48071for Lewis Research HINGTON,D.C.M A Y 1972

I.Government1. 2.Rsput No.Accession No.3. Recipient's Catalog No.4. Title and Subtitle5. Report DateMay 1972OXIDATION RESISTANT POROUS MATERIAL FORTRANSPIRATION COOLED VANES" " " 6. PerformingOrganization Code8. Performing Organization Report No.NonePer Madsen and Robert M. Rusnak1 . 10. Work Unit No.9. PerformingOrganizationNameand AddressThe Bendix ctorGrantNo.NAS .3-1047713. Type of Report andPeriodCovered12. SponsoringAgencyNameandAddressContractor ReportNational Aeronautics and Space AdministrationWashington, D. C. 2054614. SponsoringAgencyCode- " 15. SupplementaryNotes Project Manager, Edward L. Warren, Technical Advisor, Albert Kaufman, both of AirbreathingEngines Division, NASA Lewis Research Center, Cleveland, Ohio16. AbstractPorous metal sheetwith controlled permeability was made by space winding and diffusionbonding fine wire. Two iron-chromium-aluminum alloys and three nickel-chromium alloyswere used: GE 1541 (Fe-Cr-A1-Y); -H 875 (Fe-Cr-Al-Si), TD Ni Cr, DH 245 (Ni-C,r-Al-Si)and DH 242 (Ni-Cr-Si-Cb). GE 1541 and H 875 were shown in initial tests to have greateroxidation resistance than the other candidate alloys and were therefore testedmore extensively.These two materials were cyclic furnace oxidation tested in air at 1800 and 2000' F (982 and1093' C) for accumulated exposure times of 4, 16, 64,100, 200, 300, 400, 500, and 600 hours.Oxidation weight gain, permeability change and mechanical properties were determined afterexposure. Metallographic examination w a s performed to determine effects of exposure on theporous metal and electron beam weld joints of porous sheet to IN 100 strut material. Hundredhour stress rupture life and tensile tests were performed at 1800 F (982' C). Both alloys hadexcellent oxidation resistance and retention of mechanical properties and appear suitable foruse as transpiration cooling materials in high temperature gas turbine engines. In particular,the GE 1541 alloy extends the useable temperature range by more than 300' F (149' C) as compared to the most common alloy in use today (DH 242).17. Key Words(SuggestedbyIAuthor(s))Turbine coolingOxidation resistancePoroloyWire cloth19. SecurityClassif. (of this report)Unclassified18. Distribution StatementFiltersUnclassified- unlimitedI20. Security Classif. (of this page)21. No. of PagesUnclassified*For sale by thP National Technical Information Service, Springfield, Virginia1 .10222. Rice' 3.0022151,

TABLEO F CONTENTSPageSECTION 1SECTION pose2.3SECTION3.13-WPi rreo c u r e m e n t3.1.13.1.23.1.33.2WIRE PROCUREMENT AND POROLOY PROCESS DEVELOPMENTAnalysis of AcceleratedOxidationRod a n dWireSpecificationW iPr erocessingPo ro 1 o y P roces s Deve 1 opmen t3 . 2P.o1r o Pl oryo c e s s3.2.2D i f f u s i oBno n d i nDge v e l o p m e n tSECTION4.14.24.34.44.55.1-EXPERIMENTAL PROCEDURE12Specimen P r e p a r a t i o .4O x i d a t i o n Specimens4.1.5P o r o l o yS t r e s sR u p t u r ea n d12121212Hot T e n s i l e Specimens13Oxi d a t i o n134.2.1ApparatusSchedule4.2.2O x i d a t i o nS p e c i m e nE x a m i n a t i o na n dT e s t i n g1313144.3.1WeightGain4P. e3 r. 2meability4.3.3T h i c k n e s s Change4.3.4M e c h a n i cPar lo p e r t i e s4.3.5M e t a l l o g r a p hEi cx a m i n a t i o n1414141415S t r e s sR u p t u r ea n dW e l dE x a m i n a t i o nSECTION5.245-Hot T e n s i l e T e s t s151516RESULTS AND D I S C U S S I O NS t a t iOc x i d a t i oTne s t sC y c lOi cx i d a t i o n16165.2.15.2.21617WeightGainPermeabilityiii

TABLE OF CONTENTS ( C o n t i n u e d )Page5.35.45.55.2.3T h i c k n e s s Change5.2.4BendTests5 . 2T. 5e n s iSl et r e n g t h5.2.6J o i n t T e n s i lSet r e n g t h5.2.7M e t al ol g r a p h iEc xamination1717171818S t r eRssuptureWeldinTgests191919-21Hot T e n s i lTee s t sSECTION6CONCLUSIONSAPPENDIX A-NUMERICALDATAAPPENDIX B-POROLOY OXIDATION WEIGHT GAIN AND PERMEABILITY PLOTS43METALLOGRAPHIC EXAMINATION -CYCLIC5137TABULATIONAPPENDIX E-WELDINGTESTS88APPENDIX F-STATIC 0x1 DATIONTESTS94APPENDIX CAPPENDIX DSTRESSRUPTURE,HOTOXIDATIONTENSILE AND STRESS OXIDATION TESTSREFERENCES7698iv

LIST OF TABLESTitleT a b l e No.1234PageA1 loy C h e m i c a l A n a l y s i sW i r eM e c h a n i c a lP r o p e r t i e sMetal lographi c Etchant SchedulePoroloyTensileProperties23232424L I S T OF ILLUSTRATIONSF i g u r e No.12.345678910111213TitleWi r eS u r f a c e-PageGE 1541W i r eM i c r o s t r u c t u r e- GE 1541 exposed t o n i t r o g e n- GE 1541 o x i d i z e dW i r eC r o s s - S e c t i o n sP o r o l o yP h o t o m a c r o g r a p hP o t o l o yW i n d i n gM a c h i n eP o r o l o y O x i d a t i o n SpecimensSpecimenandThermocoupleArrangementS t r e s sR u p t u r ea n dO x i d a t i o nA p p a r a t u sO x i d a t i o nW e i g h tG a i nP e r m e a b i l i t y Change A f t e r O x i d a t i o n E x p o s u r ePermeabi 1 i t y Change ComparisonWi reStressRuptureLifeP o r o l o yS t r e s sR u p t u r eL i f e"25262728293031323334353636

OXIDATION RESISTANT POROUS MATERIALFOR TRANSPIRATION COOLED VANESM.byPerMadsenlandRobertRusnak2THE BENDIX CORPORATION1SUMMARYThe o b j e c t i v e o f t h i s w o r kwas t o f a b r i c a t e and t e s t po.rous m e t a ls h e e t so fo x i d a t i o nr e s i s t a n ta l l o y si no r d e rt od e t e r m i n et h e i rs u i t a b i l i t yf o ru s ei nt r a n s p i r a t i o nc o o l i n go fgas t u r b i n ev a n e s .F o u ra i l o y s , w e r ee v a l u a t e da n dcompared t o a n a l l o ycommonlyusedintranspirationcooling- DH 242.GE 1541H 875TD N i CrDH 24520Cr-1Si-1Cb-NiDH 24215Cr-bAl-lY-Fe23Cr-6Al-1Si-Fe20C r-2Th02-N i20Cr-lSi-5Al-NiThe f i r s t t h r e e a l l o y s w e r e s e l e c t e d o n t h e b a s i s o f p r e v i o u s s h e e tand1 and 2. The DH 245w i r es p e c i m e ns c r e e n i n gt e s t sas r e p o r t e di nr e f e r e n c e sDH 242because o f i t s aluminuma l l o y was s e l e c t e d a sa ni m p r o v e dv e r s i o no faddition.The a l l o y sw e r eo b t a i n e da s0 . 0 0 5i n c h( 0 . 1 3mm) d i a m e t e rw i r ea n dm a n u f a c t u r e di n t oP o r o l o y 3p o r o u sm e t a lw i t ha w a l lt h i c k n e s so f0.023 i n c h(0.58 mm).I no r d e rt omake t h eP o r o l o y ,a new f a b r i c a t i o np r o c e s swas d e v e l o p e dt oovercomethed i f f i c u l t yi nd i f f u s i o nb o n d i n gt h ea l u m i n u mc o n t a i n i n ga l l o y s .G E 1541 a l l o y was d e v e l o p e di nc o o p e r a t i o nw i t haA l s ow i r ep r o c e s s i n go ft h ec o m m e r c i a lw i r ed r a w e r .I np r e l i m i n a r ys t a t i co x i d a t i o nt e s t sa t180OoFGE 1541 and(982 C) DH 245 P o r o l o ye x h i b i t e dl e s so x i d a t i o nr e s i s t a n c et h a nH 875 P o r o l o ya n dwas e x c l u d e df r o ma d d i t i o n a lt e s t s .The TD N i C r P o r o l o yshowed a p r o n o u n c e d d e c r e a s e i n p e r m e a b i l i t y f o l l o w i n g c y c l i c o x i d a t i o n a t1800 F ( 9 8 2 " ) f o r 600 h o u r s .T h i sc o u p l e dw i t ht h ed i f f i c u l t yi np r o c e s s i n gf i n ew i r ec a u s e dt h ea l l o yt ob ed r o p p e df r o mt h ea d d i t i o n a lt e s t sg i v e nt h et w om o s tp r o m i s i n ga l l o y s- GE 1541 and H 875.F o rt h e GE 1541 and H 875 a l l o y s c y c l i c f u r n a c e o x i d a t i o n t e s t s w e r emadeonPoroloysheetcouponsat1800and2000 F(982and1093 C)inairforaccumul a t e de x p o s u r et i m e so f4, 16, 64, 100,200,300,400,500 and 600 hours.Thel S e n i o rE n g i n e e r ,F i l t e rD i v i s i o n2 P r o j e c tM e t a l l u r g i s t ,R e s e a r c hL a b o r a t o r i e s3 P o r o l o y i s a r e g i s t e r e d t r a d e name d e s c r i b i n g space-wound w i r ep o r o u sm e t a lm a t e r i a lm a n u f a c t u r e db yT h eB e n d i xC o r p o r a t i o n ,F i l t e rD i v i s i o n1

specimenswerecooledt o room t e m p e r a t u r ea f t e re a c he x p o s u r et i m e .The s p e c i change,mens weremeasured t o d e t e r m i n e o x i d a t i o n w e i g h t g a i n , p e r m e a b i l i t yt h i c k n e s s changeandroom t e m p e r a t u r em e c h a n i c a lp r o p e r t i e sa f t e re x p o s u r e .M e t a l l o g r a p h i ce x a m i n a t i o no fP o r o l o yandPoroloy/lN100 weldsamples was p e r formed t o show s i g n i f i c a n t changesduet o o x i d a t i o n and h e a t i n g .S t r e s s r u p t u r e and t e n s i l e t e s t i n g a t1800 F(982 C)b o t h 0.005 i n c h (0.13 mm) d i a m e t e r w i r e and P o r o l o y .wereperformedonB o t ha l l o y se x h i b i t e dgood o x i d a t i o n r e s i s t a n c e w i t h n o a p p a r e n t s p a l l .A f t e r 600 h o u r sc y c l i co x i d a t i o ne x p o s u r e ,t h eGE 1541 P o r o l o yw e i g h tg a i nwas85 p e rc e n th i g h e ra t1800 F(982 C)and56 p e rc e n th i g h e ra t2000 F(1093 C)t h a nt h a to ft h eH 875 P o r o l o y . However, t h ep e r m e a b i l i t yd e c r e a s ewas t h esame f o r b o t h a1 l o y s a f t e r 1800 F (982 C)exposure(20percent)andafter2000 F(1093 C)exposure,theGE 1541 Poroloypermeabil i t y decreasedlessthant h e H 875 P o r o l o y( 2 2p e rc e n tv e r s u s44 p e rc e n t ) .The GE 1541 o x i d a t i o n r e s i s t a n c e was found t o be s e n s i t i v e t o p r o c e s s i n gc o n d i t i o n s and c o n t a c t w i t h o t h e r a l l o y s a t e l e v a t e d t e m p e r a t u r e s .R e t e n t i o n o f room t e m p e r a t u r e t e n s i l e p r o p e r t i e s f o l l o w i n g600 hours o fo x i d a t i o n was good f o rP o r o l o y made from b o t ha l l o y s .I np a r t i c u l a r ,t h et e n s i l e e l o n g a t i o n was equal t o o r g r e a t e r t h a n t h a t p r i o r t o o x i d a t i o nand H 875 - 15 p e rc e n te l o n g a t i o n ) .The(GE 1541 - 10 p e rc e n te l o n g a t i o n15 p e rc e n t .The1800 Fdecrease i n t e n s i l e and y i e l ds t r e n g t h was l e s st h a n(982 C) t e n s i l e and s t r e s sr u p t u r ep r o p e r t i e sw e r ec o m p a r a b l ef o rb o t ha l l o y sw i t h an u l t i m a t e t e n s i l e s t r e n g t h o f a b o u t2500 p s i b l 7 . 2 x l o 6 N/m2) and a100 h o u rr u p t u r es t r e s so fa b o u t1500 p s i (10.3 x 10N/m2).Sound welds made betweenPoroloyand I N 100 s t r u t a l l o y .The weldzonesw e r es t r o n g e rt h a nt h eP o r o l o yand werenotdegradedby1800 F(982 C)cyclico x i d a t i o n , however,exposureat'2000"F(1093 C) r e s u l t e di ns e v e r eo x i d a t i o nofthestrutalloyand consequentlytheweldzone.Thegoodo x i d a t i o nr e s i s t a n c e ,p e r m e a b i l i t yr e t e n t i o nand r e t e n t i o n o fm e c h a n i c a lp r o p e r t i e sa tt e m p e r a t u r e sup t o 2000 F(1093 C)makes t h e GE 1541and H 875 a l l o y s a t t r a c t i v e f o r a p p l i c a t i o nas t r a n s p i r a t i o n c o o l i n g m a t e r i a l sf o r gas t u r b i n ev a n e s .I np a r t i c u l a r ,t h eGE 1541 a l l o y a t 2000 F(1093 C)hasg r e a t e rp e r m e a b i l i t yr e t e n t i o na f t e ro x i d a t i o nt h a nt h eDH 242 s t a n d a r d a l l o ya t 1700 F(927 C).2

2INTRODUCTIONT h i sr e s e a r c h and developmentworkwas c o n d u c t e d w i t h t h e u l t i m a t e g o a l o fp r o d u c i n gp o r o u sm e t a ls h e e tm a t e r i a lw i t hg o o dh i g ht e m p e r a t u r eo x i d a t i o nr e s i s t a n c ef o ra p p l i c a t i o ni nt h et r a n s p i r a t i o nc o o l i n go fgas t u r b i n ee n g i n e s .2.1BackgroundAs r e p o r t e di nr e f e r e n c e3 , t h et r e n di nb o t hm i l i t a r yand commercialgast u r b i n ee n g i n e si st o w a r d st u r b o f a ne n g i n e sh a v i n ga compact, h i g ht e m p e r a t u r egas g e n e r a t o r .To make suchenginescompact,lightweight,and w i t hs u p e r i o rs p e c i f i cf u e lc o n s u m p t i o n ,t h e r ei st h eneed t os i m u l t a n e o u s l yi n c r e a s eb o t hcompressorpressurer a t i o and t u r b i n ei n l e tt e m p e r a t u r e .T u r b i n ei n l e tt e m p e r ifa t u r e s may go t o t h o s e c o r r e s p o n d i n g t o s t o i c h i o m e t r i c f u e l - a i r m i x t u r em a t e r i a l s and c o o l i n gd e s i g n sc a nbe developedthatwill t o l e r a t e suchtemperatures re1 iably.Up t o t h e p r e s e n t t i m e , c o n v e c t i o n c o o l i n ghasbeent h ep r i m a r y means o fc o o l i n g gas t u r b i n ee n g i n e s ,w i t h some film c o o l i n g a u g m e n t a t i o n i n c r i t i c a lit i sr e g i o n s . A t t h es e v e r ec o o l i n gc o n d i t i o n se x p e c t e di nf u t u r ee n g i n e s ,will beinadequate,andmoreadvanced c o o l i n gl i k e l yt h a tc o n v e c t i o nc o o l i n gf i l m and t r a n s p i r a t i o n c o o l i n g will have t o be u t i l i z e d .schemes suchasT h e o r e t i c a l l yt r a n s p i r a t i o nc o o l i n gi s s u p e r i o r t o film c o o l i n g as showni n r e f e r e n c e 4, p r o v i d e dt h eo x i d a t i o np r o b l e m sd e s c r i b e db e l o wc a nb eo v e r come. A l s o good creep l i f e canbeaccomplishedw i t ht r a n s p i r a t i o nc o o l e db l a d e5.designs compared w i t h o t h e r c o o l i n g d e s i g n sas d e s c r i b e di nr e f e r e n c es,shroud1 inersand s i m i l a r componentshave been f a b r i c a t e df r o mf i n ew i r ea b o u t0.005 i n c hspace wound i n a g e o m e t r i cp a t t e r n and(0.13 mn) i nd i a m e t e r ,f l a t t e n e d ,f i n a l l y d i f f u s i o n bonded t o p r o v i d e a p o r o u ss t r u c t u r e - Poroloy" (See r e f e r ence 6 ) . The c h a r a c t e r i s t i c so fh i g hs u r f a c ea r e at ovolume r a t i o and smallp o r es i z e enhance c o o l i n ge f f i c i e n c yb u ta g g r a v a t eo x i d a t i o np r o b l e m s .O x i d a t i o nc o r r o s i o nw h i c hmay be c o n s i d e r e dm i n o rf o rs o l i do rs h e e tm e t a lcompon e n t sm i g h ts e r i o u s l ya f f e c tp o r o u sw a l lc o o l i n ga i r f l o w p e r m e a b i l i t y ands t r e n g t h .T h e r e f o r e ,o x i d a t i o nr e s i s t a n c ei sa p r i m a r yd e s i g nc r i t e r i o nf o rt r a n s p i r a t i o nc o o l i n gm a t e r i a ls p e c i f i c a t i o n .R e t e n t i o no fgood mechanicalp r o p e r t i e s ,e s p e c i a l l yd u c t i l i t y ,a f t e rc y c l i ch e a t i n gand a g i n g i s a l s oi m p o r t a n t as w e l l as t h eh i g ht e m p e r a t u r es t r e n g t ho ft h em a t e r i a l .A c c o r d i n g l y ,t h e s ep r o p e r t i e sa r ed e t e r m i n e di nt h i sw o r k .E a r l i e r workasdescribedi nr e f e r e n c e s 1 and 2 was d i r e c t e d t o w a r d1, s o l i df o r mI.rne f e r e n c eselectionofalloysfortestinginporousmetao x i d a t i o n r e s i s t a n c e ands h e e ts p e c i m e n sw e r ee v a l u a t e do nt h eb a s i so f-I." P o r o l o yi sa r e g i s t e r e dt r a d e name d e s c r i b i n g space-wound w i r ep o r o u sm e t a lon, F i l t e r D i v i s i o n .m a t e r i a l ,m a n u f a c t u r e db yTheBendixCorporat3

m e c h a n i c apl r o p e r t i e s .F o u rc a n d i d a t ea l l o y s(N 155, TD nickel-chromium, DH 242and H a s t e l l o y X ) w e r es e l e c t e do nt h eb a s i so ft h er e s u l t so ft h e s et e s t sforf u r t h e re v a l u a t i o n .As r e p o r t e di nr e f e r e n c e2 ,t h e s ea l l o y sw e r emade i n t o f i n emm) d i a m e t e r )a n dt e s t e df o ro x i d a t i o nr e s i s t a n c eandw i r e (0.005 inch(0.13m e c h a n i c a lp r o p e r t i e s .The t e s t i n go ft h ea l l o y si nw i r ef o r mwas a necessaryp r e l u d et of a b r i c a t i o no fp o r o u sm a t e r i a l sf r o mt h e s ea l l o y sb e c a u s et h eo x i d a t i o nb e h a v i o r a n dm e c h a n i c a lp r o p e r t i e sc o u l dd i f f e rs i g n i f i c a n t l ybetween ag i v e na l l o yi ns h e e tand w i r ef o r m .I na d d i t i o n ,t h ed i f f i c u l t yi nf a b r i c a t i o no f good q u a l i t y f i n e w i r e f r o m e a c h a l l o ywas assessed.I t was c o n c l u d e dt h a tTD nickel-chromium showed themostpromiseandshouldbeconsideredforevalua t i o n i n p o r o u sm e t a fl o r m .I na d d i t i o n ,i t was n o t e dt h a ta l l o yGE 1541 w h i c hhadbeent e s t e di ns h e e tb u tn o tw i r ef o r ms h o u l dbeconsideredbecauseof i t ss u p e r i o ro x i d a t i o np r o p e r t i e s .2.2ScopeBased on t h e e a r l i e r a l l o y s e l e c t i o nwork, t h i s i n v e s t i g a t i o n was i n i t i a t e dt oe v a l u a t eP o r o l o ymade from GE 1541, TD N i Cr and DH 242and t o s u p p l y NASA w i t hs h e e t so ft h etwobesto f t h e s em a t e r i a l s .D i f f i c u l t ywas e n c o u n t e r e di np r o c u r i n g good q u a l i t y TD N i Cr w i r e i n s u f f i c i e n t q u a n t i t y f o r f a b r i c a t i n gP o r o l o y and i n i t i a l o x i d a t i o n p e r m e a b i l i t y t e s tshowed l e s sp e r m e a b i l i t yr e t e n t i o nt h a nGE 1541. C o n s e q u e n t l yt h i sm a t e r i a lwas d r o p p e df r o mc o n s i d e r a t i o nDH 245 and H 875.B o t hw e r es e l e c t e df o ri nf a v o ro ft w oo t h e rc a n d i d a t ea l l o y s ,b e i n gr e a d i l ya v a i l a b l ei nf i n ew i r eformandf o rt h e i re x p e c t e dgood o x i d a t i o nr e s i s t a n c e ; DH 245, a n i c k e l - c h r o m i u mt y p ea l l o ys i m i l a rt oDH 242 e x c e p tf o rt h ea d d i t i o n o f aluminumandH 875, a n i r o n chromiumaluminum a l l o y w h i c h was showni n e a r l i e r w o r k( r e f e r e n c e1 ) t o havegoodo x i d a t i o nr e s i s t a n c e .P r e l i m i n a r ye v a l u a t i o no ft h ea l l o y si nw i r eand F'oroloy f o r ml e dt ot h ec o n c l u s i o nt h a to n l y t h e GE 1541 and H 875 a l l o y ss h o u l db ee v a l u a t e de x t e n s i v e l yi np o r o u smetalform.The reason f o rt h i sc o n c l u s i o nwas t h a tt h e s ea l l o y sw e r et h eo n l yones t h a t showed anypromise o f b e i n g a b l e t o o p e r a t e a t t e m p e r a t u r e s o f 1 8 0 0 " (982 C)andabove,w i t h o u to x i d a t i o ns u f f i c i e n tt ocause a s i g n i f i c a n t loss o fs h e e tp e r m e a b i l i t y .However, t h et e n a c i o u so x i d el a y e rf o r m e db yt h ea l l o y smade d i f f u s i o n b o n d i n g d i f f i c u l tand n e c e s s i t a t e d a processdevelopmentforf a b r i c a t i n g them i n t oP o r o l o y .I t was d i s c o v e r e dd u r i n gt h i sp r o c e s sd e v e l o p ment t h a tt h e GE 1541 a l l o ys u f f e r e da c c e l e r a t e do x i d a t i o na tt e m p e r a t u r el e v e l swhere o x i d a t i o ni sn o r m a l l ys l i g h ti nt h eb u l ka l l o y .T h i sp o o ro x i d a t i o nr e s i s t a n c ea p p e a r e dt ob ei n t r o d u c e dt ot h ea l l o yd u r i n gp r o c e s s i n gi n t ow i r ef o r m .An i n v e s t i g a t i o n was conducted t o d e t e r m i n e t h e c a u s e o f t h e l o s s o f o x i d a t i o nr e s i s t a n c e and s p e c i f i c a t i o n s w e r e a d o p t e d f o r t h e a l l o y i n w i r eand rodformtopreventsucha l o s sf r o mo c c u r r i n gi nt h ef u t u r e .E v a l u a t i o no ft h eG E 1541 and H 875 i n p o r o u sm e t a lf o r mc o n s i s t e do fc y c l i cf u r n a c eo x i d a t i o nt e s t sa t1800 and 2000 F(982and1093 C) f o re x p o s u r et i m e so f 4, 16, 64, 100, 200, 300, 400, 500 and 600 h o u r s .A f t e reachexposurec y c l e , specimenswereremoved f r o mt h ef u r n a c eand a i rc o o l e d .T e m p e r a t u r e sand t i m e sa sw e l la sg e n e r a lt e s tp r o c e d u r e sw e r et h esame as t h o s er e p o r t e di nreferences 1 and 2.The o x i d a t i o ne f f e c t s wereevaluatedbymeasurement o fw e i g h tg a i n ,p e r m e a b i l i t ychange, t h i c k n e s s change and room temperaturem e c h a n i c a lp r o p e r t i e sa f t e re x p o s u r e .E l e c t r o nbeam w e l dj o i n t sbetweenPoroloyand I N 100 s t r u tm a t e r i a lw e r ea l s oe v a l u a t e di nt h e s et e s t s .I na d d i t i o n ,4

t e n s i l e and s t r e s sr u p t u r ep r o p e r t i e sweredetermineda t 1800 F(982 C).Testsf o rp e r m e a b i l i t yf o l l o w i n go x i d a t i o na t1700and1800 F(927and982 C)ande l e c t r o n beam w e l de v a l u a t i o n sw e r emade f o r t h e TD N i C r and DH 242 a l l o y s .DH 242servedasreferenceo f c o m p a r i s o nf o rt h eThe r e s u l t s o b t a i n e d f o r t h eD H 242 i s t h e most commonly employed a l l o y f o r t r a n s p i r a t i o no t h e ra l l o y ss i n c e7).c o o l i n gt o d a y( r e f e r e n c e2.3PurposeThe purpose o f t h i s i n v e s t i g a t i o nwas t o e v a l u a t e t h e s e l e c t e d a l l o y s i nporousmetalformi n terms o f p o t e n t i a l a p p l i c a t i o n for t r a n s p i r a t i o nc o o l i n go f gas t u r b i n e vanes.T h i sp u r p o s e was t o beaccomplishedby(1)developingp r o c e d u r e sf o rp r o d u c i n go x i d a t i o nr e s i s t a n tp o r o u sm a t e r i a lf r o md i f f i c u l t - t o bond, o x i d a t i o nr e s i s t a n ta l l o y s ,( 2 )e v a l u a t i n ge l e c t r o nbeam w e l d j o i n t s o ft h e s em a t e r i a l st ot u r b i n eb l a d es t r u ta l l o y s ,a n d( 3 )e x p e r i m e n t a l l yd e t e r m i n i n gandmechanicalproperties.the effects of oxidationonpermeability5

3WIRE PROCUREMENT AND POROLOY PROCESS DEVELOPMENT3.1WireProcurementA l l w i r e f o r t h i s program wasmadet o a nominaldiameter o f 0.005 i n c h(0.13 mm) u n l e s so t h e r w i s en o t e d .The H 875, DH 242andDH 245 a l l o yw i r e sw e r epurchased t o c o m m e r c i a ls p e c i f i c a t i o n s from H o s k i n sM a n u f a c t u r i n g Company andD r i v e rH a r r i s Company, r e s p e c t i v e l y . A vacuum m e l t e dh e a to fGE 1541 wasp u r c h a s e df r o mt h eG e n e r a lE l e c t r i cCompany andprocessedintofinewirebyH o s k i n sM a n u f a c t u r i n g Company. The c h e m i c a la n a l y s i so fa l la l l o yw i r e sa r ep r e s e n t e di nT a b l e1 . The m e c h a n i c a lp r o p e r t i e so ft h ew i r e si nt h ea s - r e c e i v e d ,s i m u l a t e ds i n t e r e dc o n d i t i o nand a f t e r o x i d a t i o n a r e g i v e n i n T a b l e2.3.1.1A n a l y s i so fA c c e l e r a t e dO x i d a t i o n .- I t was d i s c o v e r e dd u r i n gt h edevelopment o fb o n d i n gp r o c e d u r e sf o rGE 1541 w i r e t h a t bondedsamplesunderwenta c c e l e r a t e do x i d a t i o na f t e rs h o r te x p o s u r e( 2 4h o u r s )i na i ra t1800 F (982 C).The f i r s t i m p r e s s i o n was t h a t some o ft h eb o n d i n gt e c h n i q u e sw e r ec o n t r i b u t i n gt ot h el o s so fo x i d a t i o nr e s i s t a n c ei nt h ea l l o ys i n c et h eb u l ka l l o yo x i d a t i o nr e s i s t a n c e was e x c e l l e n t .However, i t was q u i c k l yd i s c o v e r e d upon o x i d a t i o nt e s t i n go ft h eGE 1541 w i r e p r i o r t o b o n d i n gt h a tt h ep o o ro x i d a t i o nr e s i s t a n c ewas i n h e r e n ti nt h ew i r e .T h e r e f o r ean i n v e s t i g a t i o n was u n d e r t a k e nt od e t e r minethecauseo ft h ep r o b l e mand t o u s e t h i s i n f o r m a t i o n t o p r e p a r ea specific a t i o nf o rt h ew i r eand t h er o d( f r o mw h i c ht h ew i r ei s drawn)whichwouldp r e v e n td e g r a d a t i o no fo x i d a t i o nc h a r a c t e r i s t i c si nt h er e d u c t i o no ft h ea l l o yf r o mb u l kt ow i r ef o r m .The f i r s t s t e p i n t h e a n a l y s i swas m e t a l l o g r a p h i ce x a m i n a t i o n .P h o t o g r a p h so ft h ew i r es u r f a c er e v e a l e dt h ep r e s e n c eo ft r a n s v e r s ec r a c k sa l o n gt h ew i r ew h i c h had p o o r o x i d a t i o n r e s i s t a n c e w h i l e t h e w i r e w i t hgood o x i d a t i o n r e s i s t a n c e had none ( F i g u r e1 ) .E x a m i n a t i o no ft h e1/4 i n c h( 6 . 4mm) d i a m e t e r o df r o mw h i c ht h ew i r ewas drawn a l s o r e v e a l e d some s u r f a c e c r a c k s , b u t w i t hafrequency much l e s st h a no nt h ew i r e .W i r e sw i t hp o o ro x i d a t i o nr e s i s t a n c ew e r efound t o r e g a i n o x i d a t i o n r e s i s t a n c eif, priortooxidation,thewirewas e t c h e dt o remove a l lt r a c e so ft h es u r f a c ec r a c k s .T h i si n d i c a t e dt h a tt h ep o o ro x i d a t i o n r e s i s t a n c e was i n i t i a t e d by t h es u r f a c el a y e rc o n t a i n i n gt h ec r a c k s .Samples w i t h t r a n s v e r s e s u r f a c e c r a c k s w e r e f o u n d t o o x i d i z emore r a p i d l y whentheywereexposedt o h y d r o c h l o r i c a c i d and t h e n o x i d a t i o n - t e s t e d w i t h o u tc l e a n i n gt h er e s i d u e .T h e r e f o r e ,i m p r o p e rc l e a n i n gd u r i n gw i r ep r o c e s s i n gc o u l dh a v ec o n t r i b u t e dt oi t s failure.However, t h i sd i dn o te x p l a i nt h ep r e s e n c eo fI t was thoughtthatimproperdrawingprocedurescouldLea causet h ec r a c k s .( e . g . ,e x c e s s i v er e d u c t i o n s ,i m p r o p e rl u b r i c a t i o n ) .The e f f e c to fa n n e a l i n gf u r n a c ea t m o s p h e r ewas i n v e s t i g a t e d .A n n e a l i n gt h ew i r ei nh y d r o g e na t1900 F(1038 C)producedn e i t h e rc r a c k i n gn o rg r e a t l ya c c e l e r a t e do x i d a t i o n .However, t h ee f f e c to fn i t r o g e nwas pronounced. Asshown i nF i g u r e2 ,a n n e a l i n gi na n i t r o g e na t m o s p h e r ef o ro n l y1 / 2h o u ra t1900 F( 1 0 3 8 " )p r o d u c e dn i t r i d e st h r o u g h o u tt h ec r o s ss e c t i o no ft h ew i r e .Thesen i t r i d e se m b r i t t l e dt h ew i r e .C o n s e q u e n t l y ,e x p o s u r et on i t r o g e nwas mostp r o b a b l yt h ec a u s eo fs u r f a c ec r a c k i n gs i n c et h ew i r e sw e r ea n n e a l e di nc r a c k e dammonia d u r i n gp r o c e s s i n g .The e x p o s u r ed u r i n gp r o c e s s i n gwas o n l yt h e6IIllI II

e q u i v a l e n t o f a b o u to n em i n u t es t a t i ce x p o s u r eand t h e r e f o r e , n i t r i d e s w e r e n o tn o t e dt h r o u g h o u tt h ew i r e ' sc r o s ss e c t i o n .However, f o r m a t i o ni n a t h i ns u r f a c et o p r o d u c et h ec r a c k i n g .! J i r e sw h i c hw e r eh e a t e di nl a y e rw o u l db es u f f i c i e n tt h en i t r o g e na t m o s p h e r ei nt h el a b o r a t o r yw e r et h e ne x p o s e dt oa i ra t1 8 0 0 " (982 C) f o r 24 hoursandfoundt os u f f e ra c c e l e r a t e do x i d a t i o n( F i g u r e3).Therefore,exposureof thewireduringannealingtonitrogen-containingatmosp h e r e was a p p a r e n t l y t h e c a u s e o f t h e l o s s o f o x i d a t i o n r e s i s t a n c e s i n c e w i r ep r o c e s s i n gp e r f o r m e di na ni n e r t( n o n - n i t r o g e n )a t m o s p h e r ey i e l d e dgood q u a l i t yw i r e .E x a m i n a t i o no fw i r esamples d u r i n gv a r i o u ss t a g e so fw i r ed r a w i n gr e v e a l e d t h a t most o f t h e t r a n s v e r s e c r a c k s w h i c h o c c u r r e d i n p o o r q u a l i t y w i r ea p p e a r e da f t e rt h ef i n a ldraw i n d i c a t i n g t h i s t o bethemostcriticalstepintheprocess.The l o s s o f o x i d a t i o n r e s i s t a n c e a f t e r e x p o s u r et o n i t r o g e na p p e a r s t o bea r e s u l to fn i t r i d ef o r m a t i o nw i t ht h ea l l o y i n ge l e m e n t s .G e n e r a lE l e c t r i chasGE 1541 a l l o y l o s e s i t sgood o x i d a t i o nr e s i s t a n c e when t h ef o u n dt h a tt h ealuminumleveldropsbelow3.5 p e rc e n t .A p p a r e n t l yt h ef o r m a t i o no fn i t r i d e sd e p l e t e st h em a t r i xa l u m i n u mt oa c o n c e n t r a t i o nb e l o wt h i sv a l u e .3.1.2Rod and W i r eS p e c i f i c a t i o n . - Based o nt h er e s u l t so ft h i sa n a l y s i s ,s p e c i f i c a t i o n sw e r e drawnupf o r t h e GE 1541 w i r e and r o d( f r o mw h i c ht h ew i r ei s drawn) t op r e v e n tt h el o s so fo x i d a t i o nr e s i s t a n c ed u r i n gp r o c e s s i n g .Thes p e c i f i c a t i o n s were g i v e nB e n d i xR e s e a r c hL a b o r a t o r i e si d e n t i f i c a t i o nnumbersand a r ed e s i g n a t e da sPS-985 ( w i r e ) and PS-997 ( r o d ) . The essence of t h er o ds p e c i f i c a t i o ni st h a tt h ealuminumandy t t r i u mc o n t e n to ft h er o db es u f f i c i e n t l yp e rc e n t minimum y t t r i u m ) so t h a t i fh i g h ( 4 p e rc e n t minimumaluminumand0.5some d e p l e t i o no c c u r sd u r i n gw i r ed r a w i n g ,i t will n o td e g r a d et h eo x i d a t i o nc h a r a c t e r i s t i c so ft h eb u l ka l l o y .I na d d i t i o n ,t h er o dmustbethoroughlyi n s p e c t e d( v i s u a land d y ep e n e t r a n t )f o rs u r f a c ef l a w sand c r a c k s p r i o r t o w i r ed r a w i n gR. a d i o g r a p h i ce x a m i n a t i o nf o irn t e r n afll a w si sa l s or e q u i r e d .Them a j o rr e q u i r e m e n t s o f t h e w i r e s p e c i f i c a t i o n s a r e :1.no n i t r o g e n - c o n t a i n i n ga, n n e a l i n ga t m o s p h e r e sshouldbeemployedandreducingatmospheress h o u l d g e n e r a l l y beavoided;2.nophosphatew i r ed r a w i n gl u

schemes such as film and transpiration cooling will have to be utilized. Theoretically transpiration cooling is superior to film cooling as shown in reference 4, provided the oxidation problems described below can be over- come. Also good creep life can be accomplished with transpiration cooled blade

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