101. Plasma-sprayed Yb3Al5O12 as a novel thermal barrier coating for gas turbine applications.
- Author
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Lu, Xiangrong, Yuan, Jieyan, Li, Gui, Xu, Mingyi, Lu, Guoqiang, Zhang, Yixing, Yuan, Fuhe, Huang, Jingqi, Deng, Longhui, Jiang, Jianing, Dong, Shujuan, Chen, Wenbo, and Cao, Xueqiang
- Subjects
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THERMAL barrier coatings , *GAS turbines , *PLASMA spraying , *THERMOCYCLING , *STRUCTURAL stability - Abstract
In this study, the garnet-type Yb 3 Al 5 O 12 coating was fabricated by atmospheric plasma spraying and its properties were systematically investigated. Results show the as-sprayed coating consists of crystalline Yb 3 Al 5 O 12 with amorphous phase, recrystallization occurs at 918.5 °C accompanied by a 0.32% volume shrinkage. Yb 3 Al 5 O 12 coating demonstrates low thermal conductivity (2.1 W/(m∙K) at 1000 °C) coupled with a moderate thermal expansion coefficient (8.87 × 10−6 K−1 from 200 °C to 1400 °C). Additionally, Yb 3 Al 5 O 12 coating displays remarkable structure stability and sintering resistance at elevated temperatures. Its robust corrosion resistance can be demonstrated by rapidly generating dense anorthite layers during CMAS corrosion and the lack of a discernible corrosion layer in water vapor corrosion. Yb 3 Al 5 O 12 /YSZ TBC undertakes a thermal cycling lifetime of 970 cycles, superior to YSZ of 764 cycles. This improvement is primarily ascribed to lower oxygen permeability of garnet layer. These preliminary results indicate that Yb 3 Al 5 O 12 coating might be suitable for advanced TBC applications. [ABSTRACT FROM AUTHOR]
- Published
- 2024
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