PERFORMANCE OF THERMAL BARRIER COATINGS IN HIGH HEAT-FLUX ENVIRONMENTS

被引:82
作者
MILLER, RA
BERNDT, CC
机构
[1] NASA, Lewis Research Cent,, Cleveland, OH, USA, NASA, Lewis Research Cent, Cleveland, OH, USA
关键词
REFRACTORY MATERIALS - Zirconia - THERMAL INSULATION;
D O I
10.1016/0040-6090(84)90534-0
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Thermal barrier coatings were exposed to the high temperature and high heat flux produced by a 30 kw plasma torch. Analysis of the specimen heating rates indicates that the temperature drop across the thickness of the 0. 038 cm ceramic layer was about 1100 degree C after 0. 5 s in the flame. An as-sprayed ZrO//2-8wt%Y//2O//3 specimen survived 3000 of the 0. 5 s cycles without failing. A coated specimen with no surface modification but which was heat treated in argon also did not surface spall. Heat treatment in air led to spalling in as early as one cycle from heating stresses. Failures at edges were investigated and shown to be a minor source of concern.
引用
收藏
页码:195 / 202
页数:8
相关论文
共 18 条
[1]  
BERNDT CC, 1982, CERAM ENG SCI P, V3, P792
[2]   PLASMA APPLICATIONS IN METALS PROCESSING [J].
CHANG, CW ;
SZEKELY, J .
JOURNAL OF METALS, 1982, 34 (02) :57-64
[3]  
CURREN AN, 1972, NASA TM X2461 TECH M
[4]  
HUMMIK J, 1963, HIGH TEMPERATURE INO, P197
[5]  
LIEBERT CH, 1976, NASA TM X3410 TECH M
[6]  
MANSON SS, 1966, THERMAL STRESS LOW C, P277
[7]   EFFECT OF THERMAL CYCLING ON ZRO2-Y2O3 THERMAL BARRIER COATINGS [J].
MCDONALD, G ;
HENDRICKS, RC .
THIN SOLID FILMS, 1980, 73 (02) :491-496
[8]  
MILLER RA, 1983, AM CERAM SOC BULL, V62, P1355
[9]   FAILURE MECHANISMS OF THERMAL BARRIER COATINGS EXPOSED TO ELEVATED-TEMPERATURES [J].
MILLER, RA ;
LOWELL, CE .
THIN SOLID FILMS, 1982, 95 (03) :265-273
[10]  
SCHENK H, 1959, FORTRAN METHODS HEAT, P93