Advances in coating design for high-performance gas turbines

被引:359
作者
Nicholls, J
机构
[1] Cranfield University, Bldg. 61, Cranfield, Bedfordshire, MK43 0AL, United Kingdom
关键词
gas-turbine materials; jet engines; thermal-barrier coatings (TBCs); ultrahigh-temperature coatings;
D O I
10.1557/mrs2003.194
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Surface Engineering is now a key materials technology in design of future advanced gas-turbine engines. This article focuses on coating systems for hot-gas-path components, which can vary from low-cost aluminide diffusion coatings to the more exotic, and therefore expensive, thermal-barrier coatings. Available coating systems and their relative benefits are reviewed in terms of performance against manufacturing complexity and cost. Future trends in the design of environmental- and thermal- protection coatings are discussed, including the addition of multiple reactive elements modified aluminide coatings, diffusion-barrier concepts, the design of "smart" corrosion-resisitent coatings, and the development of structurally modified, low-thermal-conductivity thermal-barrier coatings.
引用
收藏
页码:659 / 670
页数:12
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