Ablation properties of 2D C/SiC-ZrB 2 composite

科研成果: 期刊稿件文章同行评审

7 引用 (Scopus)

摘要

2D C/SiC-ZrB 2 composite was fabricated by combining chemical vapor infiltration, ZrB 2 slurry infiltration and polymer infiltration and pyrolysis method. The ablation properties of the composite under oxyacetylene flame and 1800°C methane combustion wind tunnel were studied. The results show that under the oxyacetylene flame environment, the linear ablation rate and the mass ablation rate of the 2D C/SiC-ZrB 2 are 6.1×10 -2mm/s and 1.0×10 -2g/s respectively. The anti-ablation performance is improved by infiltrated ZrB 2 particles into C/SiC matrix. Under the 1800°Cmethane combustion wind tunnel, the coating density plays a major role on the ablation behavior. At the same coating density, the mass ablation rate increases with the open porosity of the composites. The addition of ZrB 2 to C/SiC has little effect on the anti-ablation performance.

源语言英语
页(从-至)69-74
页数6
期刊Hangkong Cailiao Xuebao/Journal of Aeronautical Materials
32
2
DOI
出版状态已出版 - 4月 2012

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