材料科学
涂层
复合材料
微观结构
扫描电子显微镜
陶瓷
化学气相沉积
热重分析
热稳定性
碳化硅
纳米技术
化学工程
工程类
作者
J. P. Zhang,Qiangang Fu,Lei Zhuang,X. Chen,H. J. Li,Xiao-Ying Nan,Changchun Sun,Jian Xie
标识
DOI:10.1179/1743294414y.0000000401
摘要
SiC coating was prepared on the surface of C/C–ZrC–ZrB 2 –SiC composites by chemical vapour deposition (CVD). The microstructures and phase compositions were characterised by scanning electron microscopy and X-ray diffraction respectively. The CVD SiC coating exhibited a dense structure with a thickness of 30–40 μm. Oxidation behaviour of the coated sample was studied in a wind tunnel at 1600°C. Thermogravimetric analysis of C/C–ZrC–ZrB 2 –SiC was measured. The results show that the coated sample fractured after being exposed in the wind tunnel for 21 h. The failure of the SiC coating is attributed to excessive local stress caused by the change of thermal expansion coefficient, resulting in the generation of cracks and holes. Once the failure of SiC coating appears, the fracture would not happen quickly due to the addition of ceramics (ZrC, ZrB 2 , SiC), which could promote the oxidation resistance performance and increase the stability of C/C composites in complicated service condition.
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