Study of Electrical Properties of TBC Coated on Aero-Engine Turbine Blade
DUAN Li1, JI Zhonglin1, WENG Haotian1, CHEN Xi1, YANG Zhi1, ZOU Binglin2,WANG Ying2, LI Jie3, WANG Qiang3
1. Institute of Micro/Nano Engineering, Shanghai Jiao Tong University, Shanghai 200240, China;
2. Changchun Institute of Applied Chemistry (CIAC), Chinese Academy of Sciences, Changchun 130022, China;
3. AECC Commercial Aircraft Engine Co., Ltd., Shanghai 200240, China
Traditional aero-engine thermal barrier coatings (TBC) mainly focus on thermal insulation properties and reliability, and YSZ-based TBC is already well-developed technology. Yet its electrical properties under elevated temperatures is missing. On the other hand, due to the need to build sensors on turbine blade, study on electrical insulation of TBC is necessity. In this paper, the electrical properties of YSZ thermal barrier coatings at high temperature were studied, and a new YSZ spraying formula is proposed that its high temperature electrical insulation performance. Experiments show that adding a certain amount of alumina into the coating can improve the electrical insulation performance at high temperature by four orders of magnitude, and can meet the practical needs to embed MEMS sensors on the surface of turbine blades. In addition, the electrical properties of the metal/TBC/metal sandwich structure at high temperature have been analyzed by computer simulation. Sensor performance is a composite function of the electric conduction properties under high temperatures as well as size and dimensions of each layer.
引用本文:
段力,姬中林,翁昊天,陈熙,杨志,邹兵林,王盈,李杰,王强. 航空发动机热障涂层导电性能研究[J]. 航空制造技术, 2019, 62(17): 81-87.
DUAN Li, JI Zhonglin, WENG Haotian, CHEN Xi, YANG Zhi, ZOU Binglin,WANG Ying, LI Jie, WANG Qiang. Study of Electrical Properties of TBC Coated on Aero-Engine Turbine Blade. Aeronautical Manufacturing Technology, 2019, 62(17): 81-87.