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 |
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页(从-至) | 69-74 |
页数 | 6 |
期刊 | Hangkong Cailiao Xuebao/Journal of Aeronautical Materials |
卷 | 32 |
期 | 2 |
DOI | |
出版状态 | 已出版 - 4月 2012 |