材料科学
残余应力
烧蚀
复合材料
涂层
图层(电子)
压力(语言学)
偏转(物理)
光学
语言学
物理
工程类
哲学
航空航天工程
作者
Dou Hu,Qiangang Fu,Xiaoxuan Li,Lei Zhou,Jiaping Zhang
标识
DOI:10.1016/j.surfcoat.2022.128243
摘要
The multilayer ZrC/TaC ablation resistant coatings with different layers were designed and fabricated on the SiC coated carbon/carbon composites by plasma spraying. Based on stress distribution and ablation performance under heat flux of 2.4 MW/m2, structural parameters of the multilayer ZrC/TaC coatings (total thickness d, number of layers n and thickness ratio R) were discussed and optimized. When R was equal to 1 and d was ~300 μm, the multilayer ZrC/TaC coating with three layers (n = 3) exhibited moderate stress distribution and the best ablation resistance, induced by the ZrC anti-scouring layer with sufficient thickness and effective crack deflection at the interface. The optimized structural parameters for multilayer ZrC/TaC system are considered as follows: (i) the larger d value was beneficial to reducing the residual thermal stress during ablation process; (ii) d/n for the ZrC layer was between 100–150 μm, while d/n for the TaC layer was between 40–100 μm.
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