摘要
采用CVD法,1 050℃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∶1和2∶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β-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。
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℃. The coatings are prepared by two kinds of experimental conditions which the flow ratio of diluting gas to carrier gas are 4:1 and 2:1. 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 β-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- duced by 70% and 75% , compared to that of the uncoated C/C-SiC composites prepared with two kinds of flow rati- os, respectively, and the coatings show excellent antioxidation and anti-ablative performances.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
2013年第2期78-82,共5页
Aerospace Materials & Technology
基金
国防重大基础科研项目(c0320110006)