STRESS-RELAXATION OF LOW-PRESSURE PLASMA-SPRAYED NICRALY ALLOYS

被引:53
作者
BRINDLEY, WJ
WHITTENBERGER, JD
机构
[1] National Aeronautics and Space Administration, Lewis Research Center, Cleveland
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 1993年 / 163卷 / 01期
关键词
D O I
10.1016/0921-5093(93)90575-Y
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The stress relaxation behavior of three NiCrAlY alloys that are commonly used as bond coats for thermal barrier coatings (TBCs) has been directly measured. The relaxation study was conducted at temperatures of 800-1000-degrees-C and over a wide range of stresses. It was established that all three bond coat alloys relaxed quite rapidly at temperatures of 900-degrees-C and above. Since the upper use temperatures for bond coats in gas turbine engines are between 900 and 1000-degrees-C, bond coat relaxation is expected to occur in service. Therefore, relaxation of the bond coat has the potential to affect TBC life. Furthermore, the relaxation differences observed between the three alloys offers a possible explanation for the differences in TBC life observed for these bond coats. While bond coat relaxation is expected to occur for a TBC in service, the mechanism for a relaxation effect on TBC life, if it exists, is yet to be determined.
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页码:33 / 41
页数:9
相关论文
共 13 条
[1]  
BRINDLEY WJ, 1989, ADV MATER PROCESS, V136, P29
[2]   THERMAL BARRIER COATING LIFE AND ISOTHERMAL OXIDATION OF LOW-PRESSURE PLASMA-SPRAYED BOND COAT ALLOYS [J].
BRINDLEY, WJ ;
MILLER, RA .
SURFACE & COATINGS TECHNOLOGY, 1990, 43-4 (1-3) :446-457
[3]  
COOK LS, UNPUB J MATER SCI
[4]  
GEDWILL MA, 1980, NASA TM81567 TECH ME
[5]   STRESS RELAXATION, INTERNAL STRESS, AND WORK HARDENING IN SOME BCC METALS AND ALLOYS [J].
GUPTA, I ;
LI, JCM .
METALLURGICAL TRANSACTIONS, 1970, 1 (08) :2323-&
[6]   STRESS RUPTURE AND CREEP-BEHAVIOR OF A LOW-PRESSURE PLASMA-SPRAYED NICOCRALY COATING ALLOY IN AIR AND VACUUM [J].
HEBSUR, MG ;
MINER, RV .
THIN SOLID FILMS, 1987, 147 (02) :143-152
[7]  
HILLERY RV, 1988, NASA180807 CONTR REP
[8]   STRESS RELAXATION AND MECHANICAL BEHAVIOR OF METALS [J].
LEE, D ;
HART, EW .
METALLURGICAL TRANSACTIONS, 1971, 2 (04) :1245-&
[9]   CURRENT STATUS OF THERMAL BARRIER COATINGS - AN OVERVIEW [J].
MILLER, RA .
SURFACE & COATINGS TECHNOLOGY, 1987, 30 (01) :1-11
[10]   FAILURE MECHANISMS OF THERMAL BARRIER COATINGS EXPOSED TO ELEVATED-TEMPERATURES [J].
MILLER, RA ;
LOWELL, CE .
THIN SOLID FILMS, 1982, 95 (03) :265-273