CVD-SiC 涂层的C/ C-SiC 复合材料的抗烧蚀性能
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西安航天复合材料研究所

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Anti鄄Ablative Preformances of CVD-SiC Coated C/ C-SiC Composites
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    摘要:

    采用CVD 法,1 050益在三维针刺C/ C-SiC 复合材料表面制备SiC 涂层,研究稀释气体与载气流
    量比分别为4 颐1 和2 颐1 制备条件下涂层的晶体结构、表面和断面的微观形貌,对比了涂层前后C/ C-SiC 复合
    材料的抗烧蚀性能。结果表明:稀释气体流量降低其制备的SiC 涂层更加平整致密,与基体结合程度更好,沉
    积产物均为单一的茁-SiC 结晶相。在600 s 的氧化烧蚀下,两种流量比条件下制备CVD-SiC 涂层的C/ C-SiC
    复合材料的线烧蚀率比未涂层的分别降低34%和50%,质量烧蚀率分别降低70%和75%,抗氧化烧蚀性能明
    显提高。

    Abstract:

    SiC coatings on the surface of the three dimensional needled carbon/ carbon and silicon carbide (C/ C
    -SiC) composites were prepared by chemical vapor deposition (CVD) at 1 050益. The coatings are prepared by two
    kinds of experimental conditions which the flow ratio of diluting gas to carrier gas are 4 颐1 and 2 颐1. The crystalline
    structure and the surface and cross section micromorphologies of the coatings are analyzed by X-ray diffraction and
    scanning electronic microscopy. The oxidation and ablation performance are compared between uncoated and coated
    C/ C-SiC composites. The results show that the deposited coatings mainly consist of 茁-SiC. The surface of coating
    prepared with reducing the flow of diluting gas is smooth and dense,and also strongly bonded with the substrate. As to
    the coated C/ C-SiC composites, the linear ablation rate is reduced by 34% and 50%, and the mass ablation rate re鄄
    duced by 70% and 75%, compared to that of the uncoated C/ C-SiC composites prepared with two kinds of flow rati鄄
    os, respectively, and the coatings show excellent antioxidation and anti鄄ablative performances.

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王玲玲. CVD-SiC 涂层的C/ C-SiC 复合材料的抗烧蚀性能[J].宇航材料工艺,2013,43(2).

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  • 在线发布日期: 2016-11-28
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