RANKING PROTECTIVE COATINGS - LABORATORY VS FIELD EXPERIENCE

被引:4
作者
CONNER, JA [1 ]
CONNER, WB [1 ]
机构
[1] GE CO,POWER GENERAT,HIGH TEMP MAT ENGN TEAM,SCHENECTADY,NY 12301
来源
JOM-JOURNAL OF THE MINERALS METALS & MATERIALS SOCIETY | 1994年 / 46卷 / 12期
关键词
D O I
10.1007/BF03222662
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Environmentally protective coatings are used on a wide range of gas turbine components for survival in the harsh operating conditions of engines. A host of coatings are commercially available to protect hot-section components, ranging from simple aluminides to designer metallic overlays and ceramic thermal barrier coatings. A variety of coating-application processes are available, and they range from simple pack cementation processing to complex physical vapor deposition, which requires multimillion dollar facilities. Detailed databases are available for most coatings and coating/process combinations for a range of laboratory tests. Still, the analysis of components actually used in engines often yields surprises when compared against predicted coating behavior from laboratory testing. This paper high-lights recent work to develop new laboratory tests that better simulate engine environments. Comparison of in-flight coating performance as well as industrial and factory engine testing on a range of hardware is presented along with laboratory predictions from standard testing and from recently developed cyclic burner-rig testing.
引用
收藏
页码:35 / 38
页数:4
相关论文
共 7 条
[1]  
BUNGARDT K, 1972, Patent No. 3677789
[2]  
CONNER JA, 1991, INT GAS TURB AEROENG
[3]  
CONNER JA, 1992, INT GAS TRUBINE AERO
[4]  
FONTANA MG, 1978, CORROSION ENG, P347
[5]  
FOSTER AD, 1993, GER3632B GE POW GEN
[6]  
Pettit F.S., 1987, SUPERALLOYS, P327
[7]  
Schaeffer J., 1989, ROLE ACTIVE ELEMENTS, P231