北京航空航天大学
纸质出版:1997
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杨晓光, 耿瑞, 熊昌炳. 航空发动机热端部件隔热陶瓷涂层应用研究[J]. 航空动力学报, 1997,12(2).
Yang Xiaoguang, Gen Rui, Xiong Changbin. A SURVEY ON APPLICATION OF TBC FOR AEROENGINE HOT SECTIONS[J]. 1997, 12(2).
杨晓光, 耿瑞, 熊昌炳. 航空发动机热端部件隔热陶瓷涂层应用研究[J]. 航空动力学报, 1997,12(2). DOI:
Yang Xiaoguang, Gen Rui, Xiong Changbin. A SURVEY ON APPLICATION OF TBC FOR AEROENGINE HOT SECTIONS[J]. 1997, 12(2). DOI:
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.
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