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Reaction kinetics and ablation properties of C/C-ZrC composites fabricated by reactive melt infiltration

机译:反应性熔体渗透制备C / C-ZrC复合材料的反应动力学和烧蚀性能

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摘要

Carbon/carbon-zirconium carbide (C/C-ZrC) composites were prepared by reactive melt infiltration. Carbon fiber felt was firstly densified by carbon using chemical vapor infiltration to obtain a porous carbon/carbon (C/C) skeleton. The zirconium melt was then infiltrated into the porous C/C at temperatures higher than the melting point of zirconium to obtain C/C-ZrC composites. The infiltration depth as a function of annealing temperature and dwelling time was studied. A model based on these results was built up to describe the kinetic process. The ablation properties of the C/C-ZrC were tested under an oxyacetylene torch and a laser beam. The results indicate that the linear and mass ablation rates of the C/C-ZrC composites are greatly reduced compared with C/SiC-ZrB_2, C/SiC, and C/C composites. The formation of a dense layer of ZrC and Zr02 mixture at high temperatures is the reason for high ablation resistance.
机译:碳/碳锆碳化物(C / C-ZrC)复合材料是通过反应性熔渗法制备的。碳纤维毡首先通过使用化学气相渗透的碳致密化,以获得多孔碳/碳(C / C)骨架。然后在高于锆熔点的温度下将锆熔体渗透到多孔C / C中以获得C / C-ZrC复合材料。研究了渗透深度与退火温度和停留时间的关系。建立了基于这些结果的模型来描述动力学过程。在氧乙炔炬和激光束下测试了C / C-ZrC的烧蚀性能。结果表明,与C / SiC-ZrB_2,C / SiC和C / C复合材料相比,C / C-ZrC复合材料的线性和质量烧蚀速率大大降低。高温下形成致密的ZrC和ZrO2混合物层是抗烧蚀性高的原因。

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