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航空发动机热障涂层存在的问题及其发展方向

朱晨 于建海 郭亚飞 丁坤英

表面技术2016,Vol.45Issue(1):13-19,7.
表面技术2016,Vol.45Issue(1):13-19,7.DOI:10.16490/j.cnki.issn.1001-3660.2016.01.003

航空发动机热障涂层存在的问题及其发展方向

Problems of Aircraft Engine Thermal Barrier Coating and Its Developing Direction

朱晨 1于建海 1郭亚飞 1丁坤英1

作者信息

  • 1. 中国民航大学 天津市民用航空器适航与维修重点实验室,天津300300
  • 折叠

摘要

Abstract

Thermal barrier coating is mainly applied on the hot components of engine, which can reduce fuel consumption, in-crease efficiency and prolong the service life of hot components. The rapid development of thermal barrier coating technology has greatly promoted the improvement of aviation engine performance,but there exist some failure problems in using process. This arti-cle mainly discussed four problems of the YSZ thermal barrier coating, including high temperature sintering,TGO growth stress,hot corrosion in high temperature and mismatch of interfacial stress. In addition, it also introduced the solution of these problems. Fi-nally, this paper also reviewed and prospected the novel low-conductive TBC and the TBC which is currently applied on CMC matrix.

关键词

热障涂层/陶瓷层/失效/低热导率/EBC-CMC

Key words

thermal barrier coatings/ceramic layer/failure/low thermal conductivity/EBC-CMC

分类

矿业与冶金

引用本文复制引用

朱晨,于建海,郭亚飞,丁坤英..航空发动机热障涂层存在的问题及其发展方向[J].表面技术,2016,45(1):13-19,7.

基金项目

国家自然科学基金(51501222) Fund: Supported by the National Natural Science Foundation of China(51501222) (51501222)

表面技术

OA北大核心CSCDCSTPCD

1001-3660

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