GdYbZrO thermal barrier coatings by EB-PVD: Phase, microstructure, thermal properties and failure

被引:25
作者
Shen, Zaoyu [1 ]
Liu, Zheng [1 ,2 ]
Liu, Guanxi [1 ]
Mu, Rende [1 ]
He, Limin [1 ]
Dai, Jianwei [1 ]
机构
[1] Aero Engine Corp China, Beijing Inst Aeronaut Mat, Key Lab Adv Corros & Protect Aviat Mat, Beijing 100095, Peoples R China
[2] Univ Sci & Technol Beijing, Sch Mat Sci & Engn, Beijing 100083, Peoples R China
关键词
Thermal barrier coatings; Electron beam physical vapor deposition; Thermal shock lifetime; Cracks; Failure; DOPED GD2ZR2O7; EVOLUTION; DURABILITY; SCIENCE; YB2O3; TBCS;
D O I
10.1016/j.surfin.2021.101123
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
Advanced thermal barrier coatings (TBCs) have attracted particular attention due to their low thermal conductivities and high phase stabilities. The thermal properties and failure behaviors of advanced TBCs still remain a challenge in the thermal shock test. This work focuses on thermal expansion coefficient, thermal conductivity, microstructure evolution and failure behaviors of the GdYbZrO/ Y2O3-stabilized ZrO2 (GYZ/YSZ) double ceramic layers (DCL) TBCs. Microstructure characterizations mainly include X-ray diffraction (XRD), scanning electron microscope (SEM) and transmission electron microscopy (TEM). The GYZ/YSZ DCL TBCs exhibit good thermal shock lifetime at 1100 degrees C due to the feathery nanostructure with columnar gaps leading to the improvement of strain tolerance. After thermal shock test, the failure regions occur on the cracks area and the interface instability within GYZ, YSZ and TGO. The interface instability has an effect on the failure behaviors of GYZ/YSZ DCL TBCs.
引用
收藏
页数:6
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