材料科学
复合材料
涂层
烧蚀
纳米线
基质(化学分析)
纳米技术
工程类
航空航天工程
作者
Xinfa Tian,Li Yang,Bo Li,Hejun Li,Xiaohong Shi,Hongjiao Lin
标识
DOI:10.1016/j.jeurceramsoc.2022.07.043
摘要
A novel method to prepare a coating on the C/C composite is discussed. The precursor infiltration pyrolysis method is usually applied to prepare interior ceramic matrix, thus SiC nanowires that can absorb the surficial precursor are added to prepare surficial ceramics. The method accomplishes the integration of the coating and the matrix so that no coating peels off after ablation. Moreover, the material with a ZrC/SiC precursor ratio of 5:1 (Z5S1), whose mass and linear rates are 0.47 mg/s and 0.95μm/s, exhibits the highest overall resistance to ablation. The results demonstrate that higher ZrC content and more uniform phase distribution are beneficial to keep ZrO 2 in solid and form a denser and firmer oxide layer, which is more effective in improving the ablation resistance of the C/C composite.
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