A SURVEY ON APPLICATION OF TBC FOR AEROENGINE HOT SECTIONS

Yang Xiaoguang; Gen Rui; Xiong Changbin

Volume 12 Issue 2

Apr. 1997

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Article Navigation > Journal of Aerospace Power > 1997 > 12(2): 183-188,221

Yang Xiaoguang, Gen Rui, Xiong Changbin. A SURVEY ON APPLICATION OF TBC FOR AEROENGINE HOT SECTIONS[J]. Journal of Aerospace Power, 1997, 12(2): 183-188,221.

Citation:

Yang Xiaoguang, Gen Rui, Xiong Changbin. A SURVEY ON APPLICATION OF TBC FOR AEROENGINE HOT SECTIONS[J]. Journal of Aerospace Power, 1997, 12(2): 183-188,221.

Yang Xiaoguang, Gen Rui, Xiong Changbin. A SURVEY ON APPLICATION OF TBC FOR AEROENGINE HOT SECTIONS[J]. Journal of Aerospace Power, 1997, 12(2): 183-188,221.

Citation:

Yang Xiaoguang, Gen Rui, Xiong Changbin. A SURVEY ON APPLICATION OF TBC FOR AEROENGINE HOT SECTIONS[J]. Journal of Aerospace Power, 1997, 12(2): 183-188,221.

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A SURVEY ON APPLICATION OF TBC FOR AEROENGINE HOT SECTIONS

4th Dept.Beijing University of Aeronautics and Astronautics, Beijing 100083

Received Date: 1996-03-01
Rev Recd Date: 1996-09-01
Publish Date: 1997-04-28

Abstract

Abstract

This paper gives a detailed survey about application of Thermal Barrier Coating(TBC)technology to aeroengines.First of all,thermal barrier coating system and coating technology are examined to identify the state of art of the coating technique,then characteristics of Plasma Spray Coating are compared with those of Electric Beam-Physic Vapor Deposition Coating.Meanwhile,the coating failure mechanism,coating interface strength and life prediction method are also surveyed.According to the thermal barrier coating researches at home and abroad,the authors offer some suggestions to promote the Chinese thermal barrier coating research and application.
- Aircraft engines,
- Heat insulation layer,
- Ceramics