To develop nanostructured thermal barrier coatings

被引:2
|
作者
Wang, Ning
Zhao, Weixun
Wang, Ping
Wei, Zheng
机构
[1] Inst Aeronaut Mat, AVICI, Beijing 100095, Peoples R China
[2] Shengyang Liming Engine Maker Co Ltd, AVICI, Shenyang, Peoples R China
[3] Hubei Dida Nanoceram Manufacture Co Ltd, Wuhan, Peoples R China
来源
INTERNATIONAL JOURNAL OF MODERN PHYSICS B | 2006年 / 20卷 / 25-27期
关键词
TBCs; nanopowder; nanostructure; PARTIALLY-STABILIZED ZIRCONIA;
D O I
10.1142/S0217979206041045
中图分类号
O59 [应用物理学];
学科分类号
摘要
Advanced turbine engines require the application of thermal barrier coatings (TBCs) to provide still higher reliability, thermal insulation effect and longer lifetime under harsh operating conditions. TBCs with nanostructure proved to be promising to deliver the desired property and performance. To exploit full potentials of the current widely used yttria-partially-stabilized zirconia (YSZ), nano-sized YSZ powders were developed and used as the ceramic source material. By controlling the deposition processes, novel TBCs with outstanding nanostructure such as nano-sized grains and pores were produced by atmospheric plasma spray (APS) and electron beam physical vapor deposition (EB-PVD), respectively. The incorporated nanostructure in TBCs resulted in substantial increase in thermal barrier effect and their lifetime. The long-term microstructure stability of the nanocoating was also investigated.
引用
收藏
页码:4171 / 4176
页数:6
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