Effect of Heat-treatment Temperature on Thermal and Mechanical Properties of LaMgAl11O19 Coating

被引:1
|
作者
An Wenran [1 ]
Huang Jingqi [1 ]
Lu Xiangrong [1 ]
Jiang Jianing [1 ]
Deng Longhui [1 ]
Cao Xueqiang [1 ]
机构
[1] Wuhan Univ Technol, State Key Lab Silicate Mat Architectures, Wuhan 430070, Peoples R China
基金
中国国家自然科学基金;
关键词
LaMgAl11O19; thermal barrier coating; heat-treatment; thermal and mechanical property; BARRIER COATINGS; CYCLING BEHAVIOR; MICROSTRUCTURE; MAGNETOPLUMBITE; PERFORMANCE;
D O I
10.15541/jim20210720
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
LaMgAl11O19 (LMA) coating prepared by atmospheric plasma spraying has large amounts of amorphous phase, which seriously affects the service life of coating. Effects of microstructure, such as grain size, porosity and amorphous phase content, on mechanical, thermophysical and thermal shock resistance properties of LMA coatings after heat-treatement at 900-1600. for 12 h were investigated. The results show that the as-sprayed LMA coating possesses two crystallization temperature points, 900 and 1163 degrees C. After heat-treatement at 900 degrees C, the lowest thermal diffusivity of 0.53 mm(2)/s was obtained for LMA coating at 1000 degrees C due to the large amount of amorphous phase and the highest porosity of (18.88 +/- 2.15)%. LMA coatings, heat-treated at 1100-1400 degrees C, exhibited higher hardness owing to reduced amorphous content and porosity through recrystallization and sintering with the maximum hardness of (12.08 +/- 0.58) GPa at 1100 degrees C. After heat-treatement at 1300 degrees C, the coating displayed the highest average thermal cycling life (588 times), which attributed to abundant micron flake crystals with high strain tolerance. When the heat-treatment temperature reached 1500 degrees C, the grain thickness increased rapidly due to parallel stacking of lamellar crystals, porosity increased and mechanical properties significantly decreased. During the thermal shock, grain breaking and crack propagation occurred in the coating due to the repeated thermal stress, resulting in final failure of the coating.
引用
收藏
页码:925 / 932
页数:8
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