返回届次CSCP-ICC-2024-496

Rare earth modified lanthanum zirconate thermal barrier coatings by EB-PVD: thermal performance, morphology and degradation behavior

作者

Guanxi LiuZaoyu ShenLimin HeRende Mu

单位

1Key Laboratory of Advanced Corrosion and Protection for Aviation Materials、Beijing Institute of Aeronautical Materials、Aero Engine Corporation of China、Beijing 100095 (PR China)

关键词

TBCslanthanum zirconatethermal conductivityfailure behaviorTGO

收录来源

International Corrosion Congress · 第22届国际腐蚀大会

摘要

Thermal barrier coatings have been widely investigated over the last decade. Lanthanum zirconate is known for its high melting point and good thermal stability in aircraft engine environment. Owing to the distinctive thermophysical properties, Y, Pr or Eu doping in pyrochlore La 2Zr2O7 might be a promising TBCs material as the top ceramic layer. It remains a challenge to completely understand the rare earth doped La2Zr2O7/YSZ double ceramic layer TBCs properties and microstructure evolution during thermal cyclic. In our present work, rare earth doped La2Zr2O7/YSZ double ceramic layer TBCs have been prepared by EB -PVD. The phase structure, thermal performance, microstructur e and thermal cyclic lifetime have been researched. Thermal conductivity has been decreased compared with YSZ and pure La2Zr2O7, simultaneously, coefficient of thermal expansion has been increased compared with pure La2Zr2O7. The failure behavior of rare earth doped La2Zr2O7/YSZ double ceramic layer TBCs have been elucidated as typical TGO growth mode and specific sintering crack evolution mode. This study of properties and failure behaviors might provide the valuable investigation and thought for other advanced TBCs.

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