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CYCLIC OXIDATION BEHAVIOR OF THERMAL BARRIERCOATINGS ON SINGLE CRYSTAL SUPERALLOYS |
Zhongyuan Zhang;Meiheng Li;Xiaofeng Sun |
中科院金属所 |
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Abstract The thermal barrier coatings (TBC),which Ni30C r12Al0.3Y bond coating was deposited by magnetron sputtering and ZrO2 ceramic top coating was deposited by electron beam-physical vapor deposition (EB-PVD),wa s produced on Ni-base superalloy.The bond coatings,which the mean grain size was less than 100 nm,were nanostructured coatings,and had good oxidation-resist ance.The ceramic topcoats,which were columnar structure,permitted larger strain in the coatings.The as-deposited ceramic coatings consisted of large quantity no nequilibrium tetragonal (t′),a small amount cubic (c) and monoclinic ( m) phases.The t′ phases,which had important role to the stabilization o f zirconia at high temperature,can not directly transform into m phase during co oli ng.During cyclic oxidation at 1050℃,the scale of the cast alloy had spalled aft er two cycles.After 100 cycles,the surface scale of single-crystal superalloy wa s mainly composed of NiO、Cr2O3,a little Al2O3 and pores by the Kirkenda ll effect.However,the ceramic coatings,which had microcrack,have not spalled and the thermally grown oxide (TGO) was Al2O3.There were some microcrack betwee n TGO and bond coating after 300 cycles.
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Received: 03 December 2001
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Corresponding Authors:
Zhongyuan Zhang
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[1]MillerRA .Thermalbarriercoatingsforaircraftengineshistoryanddirections[J].J .ThermalSpayTech.,1997,6(1):35 [2]LouHY ,WangFH ,etal.High-temperatureoxidationresistanceofsputteredmicro-grainsuperalloy[J].Oxid.Met.,1992,38:299-308 [3]Schmitt-ThomaKHG ,DierlU .Thermalbarriercoatingwithim provedoxidationresistance[J].Sur.Coat.Technol.,1994,68/69:113 [4]LeeEY ,BiedrmanRR ,SissonRD .Diffusionalinteractionsandre actionsbetweenapartiallystabilizedzirconiathermalbarriercoatingandtheNiCrAlYbondcoat[J].Mater.Sci.Engi.,1989,A121:467 |
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