1. High temperature abradable sealing coating for SiCf/SiC ceramic matrix composites.
- Author
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Huang, Jingqi, Liu, Ruoyu, Hu, Qing, Guo, Xiaojun, Li, Gui, Tu, Yunwei, Lu, Xiangrong, Xu, Mingyi, Deng, Longhui, Jiang, Jianing, Dong, Shujuan, Liu, Li, Chen, Meizhu, and Cao, Xueqiang
- Subjects
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HIGH temperatures , *THERMAL shock , *SLIDING wear , *SURFACE coatings , *THERMAL conductivity , *ADHESIVE wear , *THERMAL barrier coatings - Abstract
A study of porous YSZ abradable sealing coating (ASC) plasma-sprayed onto SiC f /SiC ceramic matrix composites (CMC) through the compatibility of intermediate layers is reported. The multilayer Si/Yb 2 Si 2 O 7 /LaMgAl 11 O 19 thermal-environmental barrier coating (T-EBC) is served as intermediate layers in consideration of its ability to protect the CMC from recession and ease the misfit of the thermal expansivity. Isothermal exposure and thermal shock tests were conducted at 1200°C and led to the decomposition of t'-ZrO 2 phase to t-ZrO 2 and c-ZrO 2 phases in YSZ topcoat, the formation of mud-cracks throughout the entire coating structure and thermally grown oxide (SiO 2), with following an Yb 2 Si 2 O 7 reaction layer. The measured bond strength of the coated samples was 5.47 ± 0.85 MPa, and the fracture position mainly happened inside the CMC substrate. The Superficial Rockwell Hardness (HR15Y) considered to be an important factor in abradability increased by only 1.34% after 1200°C isothermal exposure for 100 h, showing excellent high temperature hardness stability. The abradability of the ASC was investigated by a sliding wear test, the fatigue wear mainly occurred in worn scar when encountering Si 3 N 4 ceramic ball with high hardness and low thermal conductivity, while adhesive wear occurred when GCr15 steel ball with low hardness and high thermal conductivity are encountered. [ABSTRACT FROM AUTHOR]
- Published
- 2023
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