Strength degradation and failure mechanisms of electron-beam physical-vapor-deposited thermal barrier coatings

被引:63
作者
Ruud, JA
Bartz, A
Borom, MP
Johnson, CA
机构
[1] GE, Corp Res & Dev, Schenectady, NY 12301 USA
[2] GE, Aircraft Engines, Cincinnati, OH 45215 USA
关键词
D O I
10.1111/j.1151-2916.2001.tb00875.x
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Failure mechanisms were determined for electron-beam physical-vapor-deposited thermal barrier coating (TBC) systems from the degradation of mechanical properties and microstructural changes in a furnace cycle test. Bond strength degradation for TBCs resulted from the initiation and growth of interfacial delamination defects between the yttria-stabilized zirconia topcoat and the thermally grown alumina (TGO). It is proposed that defects started from concave depressions in the bondcoat surface created by the grit-blast-cleaning process and that defect growth was driven by the reduction in compressive strain in the TGO as the alumina deformed into and displaced the bondcoat during the cooling cycles. Inclusion of yttrium in the substrate resulted in a doubling of the furnace cycle life of the TBCs because of enhanced fracture toughness of the TGO-bondcoat interface.
引用
收藏
页码:1545 / 1552
页数:8
相关论文
共 24 条
[1]  
*AM SOC TEST MAT, C63379 ASTM
[2]   The influence of the reactive element yttrium on the stress in alumina scales formed by oxidation [J].
Christensen, RJ ;
Tolpygo, VK ;
Clarke, DR .
ACTA MATERIALIA, 1997, 45 (04) :1761-1766
[3]   MODELING OXIDE SPALLATION [J].
EVANS, HE .
MATERIALS AT HIGH TEMPERATURES, 1994, 12 (2-3) :219-227
[4]   CRACKING AND SPALLING OF PROTECTIVE OXIDE LAYERS [J].
EVANS, HE .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1989, 120 :139-146
[5]   Mechanism of spallation in platinum aluminide/electron beam physical vapor-deposited thermal barrier coatings [J].
Gell, M ;
Vaidyanathan, K ;
Barber, B ;
Cheng, J ;
Jordan, E .
METALLURGICAL AND MATERIALS TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1999, 30 (02) :427-435
[6]  
HOLMES JW, 1990, METALL TRANS A, V21, P1209
[7]   Influence of electron beam physical vapor deposited thermal barrier coating microstructure on thermal barrier coating system performance under cyclic oxidation conditions [J].
Leyens, C ;
Schulz, U ;
Pint, BA ;
Wright, IG .
SURFACE & COATINGS TECHNOLOGY, 1999, 120 :68-76
[8]   THERMODYNAMICS OF SEGREGATION IN ALLOYS [J].
LUTHRA, KL ;
BRIANT, CL .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1988, 19 (08) :2091-2098
[9]   PVD TBC experience on GE aircraft engines [J].
Maricocchi, A ;
Bartz, A ;
Wortman, D .
JOURNAL OF THERMAL SPRAY TECHNOLOGY, 1997, 6 (02) :193-198
[10]   THERMAL BARRIER COATING LIFE PREDICTION MODEL DEVELOPMENT [J].
MEIER, SM ;
NISSLEY, DM ;
SHEFFLER, KD ;
CRUSE, TA .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1992, 114 (02) :258-263