Evolution of Ni-based superalloys for single crystal gas turbine blade applications

被引:527
作者
Caron, P
Khan, T
机构
[1] Off Natl Etud & Rech Aerosp, Met Mat & Proc Dept, F-92322 Chatillon, France
[2] Off Natl Etud & Rech Aerosp, Gen Sci Directorate, F-92322 Chatillon, France
来源
AEROSPACE SCIENCE AND TECHNOLOGY | 1999年 / 3卷 / 08期
关键词
superalloy; single crystal; rhenium;
D O I
10.1016/S1270-9638(99)00108-X
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The chemistry of the Ni-based superalloys designed for single crystal gas turbine blades has significantly evolved since the development of the first generation of alloys derived from columnar grained materials. Thr overall performance of the second and third generations has, been significantly improved by the addition of increasing amounts of rhenium. However, the problems of increased density, grain defects and microstructural stability have also become more and more acute and render necessary to carefully control the level of the various alloying elements in order to effectively benefit from the: high potential of the most recently developed third generation alloys. (C) 1999 Editions scientifiques ct medicales Elsevier SAS.
引用
收藏
页码:513 / 523
页数:11
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