Problems of Aircraft Engine Thermal Barrier Coating and Its Developing Direction

ZHU Chen, YU Jian-hai, DING Kun-ying

Surface Technology ›› 2016, Vol. 45 ›› Issue (1) : 13-19.

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Surface Technology ›› 2016, Vol. 45 ›› Issue (1) : 13-19. DOI: 10.16490/j.cnki.issn.1001-3660.2016.01.003
Special Topic—Progress of Projects of the National Natural Science Foundation of China 2025

Problems of Aircraft Engine Thermal Barrier Coating and Its Developing Direction

  • ZHU Chen, YU Jian-hai, DING Kun-ying
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Abstract

Thermal barrier coating is mainly applied on the hot components of engine, which can reduce fuel consumption, increase 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 article 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. Finally, this paper also reviewed and prospected the novel low-conductive TBC and the TBC which is currently applied on CMC matrix.

Key words

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

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ZHU Chen, YU Jian-hai, DING Kun-ying. Problems of Aircraft Engine Thermal Barrier Coating and Its Developing Direction[J]. Surface Technology. 2016, 45(1): 13-19

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Supported by the National Natural Science Foundation of China(51501222)
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