含PyC-TaC-PyC复合界面C/C材料的氧乙炔焰烧蚀行为

Ablation behaviors of C/C composites with pyrocarbon (PyC)-TaC-PyC multi-interlayers in oxyacetylene flame

  • 摘要: 用化学气相渗透方法,在准三维针刺炭毡中预沉积热解炭(PyC)和TaC涂层,再利用热解炭和树脂炭对该预制体进行后续致密化,制得含PyC-TaC-PyC复合界面的C/C复合材料(TaC-C/C),并对其进行氧乙炔焰烧蚀。与C/C相比,3 vol%TaC-C/C材料耐烧蚀性能无明显提高,且无法承受长时间的氧炔焰烧蚀;而14 vol%TaC-C/C材料表现出较好的长时间耐烧蚀性能。氧炔焰烧蚀后,复合材料表面由C、TaC、(Ta,O)及Ta2O5相组成。3 vol%TaC-C/C材料表面主要形成细小弥散的烧蚀斑点(5~20s)和烧蚀凹坑(120s);而14 vol%TaC-C/C材料表面则主要形成烧蚀斑点(5s)、较完整的氧化钽层(20s)以及烧蚀凹坑(120s)。14 vol%TaC-C/C材料在烧蚀20s后,复合材料可分为表面氧化物区、过渡区和基体区;复合材料表面完整连续的氧化钽层能有效保护复合材料。

     

    Abstract: C/C composites with PyC-TaC-PyC multi-interlayers (TaC-C/C) were prepared by the isothermal chemical vapor infiltration and impregnation and carbonization. Their ablation properties were tested with an oxyacetylene flame. Compared to the C/C composites,the ablation-resistance property of 3vol% TaC-C/C composite is not improved;14vol%TaC-C/C composite can withstand a long time in the oxyacetylene flame. After ablation for 20s in the oxyacetylene flame,the composites are mainly composed of C,TaC,(Ta,O) and Ta2O5 phases. The ablation morphologies of 3vol%TaC-C/C composite are mainly composed of the white ablation spot (5~20s) and the ablation concave (120s),while the ablation morphologies of 14vol%TaC-C/C composites are composed of the ablation spot (5s),a perfect oxide layer (20s) and the ablation concave (120s). The cross section of 14vol%TaC-C/C composites consists of a surface oxide layer,transition region and matrix region after ablation for 20s,which can protect carbon phases in composites fairly.

     

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