材料科学
微观结构
复合材料
陶瓷
涂层
增强碳-碳
烧蚀
氧化物
碳纤维
复合数
图层(电子)
冶金
工程类
航空航天工程
作者
Lin Xu,Jia Cheng,Xingchao Li,Yin Zhang,Zhen Fan,Yongzhong Song,Zhihai Feng
摘要
Abstract In order to increase the oxidation resistance of carbon/carbon (C/C) composites at long‐term high temperature, C/C‐Ultra High Temperature Ceramics composites (UHTCs) with a dual‐layer UHTCs oxidation coating was successfully designed and fabricated. The microstructure and ablation resistance were investigated and discussed. After ablation in arc‐heated wind tunnel with temperature being 2200°C for 1000s, the mass ablation rate and linear ablation rate were −1.9 × 10 −2 mg/cm 2 s and 2.9 × 10 −5 mm/s, respectively. The formation of thermodynamically compatible oxide scale including ZrO 2 skeleton and SiO 2 or Zr–Si–O glass on the surface were mainly contributed to the excellent ablation resistance of the composite.
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