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Ablation resistance of carbides-coated C/C composites

机译:碳化物涂覆的C / C复合材料的消融抗性

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摘要

To improve the ablation resistance of C/C composites under oxyacetylene flame, SiC, TaC and HfC coatings were fabricated on composites surface. Ablation properties of coatings were detected and the ablation mechanism was discussed in the paper as well. The centre region of SiC and TaC coatings has failed during ablation and exhibited high ablative rates; it attributed to so high ablation temperature, which was much higher melting point of their oxides (Ta2O5 and SiO2). HfC coating exhibited lowest ablative rates. The reason is that the ablation temperature was just between sinter point and melting temperature of HfO2, the oxides could behave as the thermal barrier coating during ablation and provide efficient protection for C/C composites. It can be indicated that the carbide coating provides best ablation protection between the Tammann temperature and melting point of their oxides.
机译:为了改善氧乙炔火焰下C / C复合材料的消融抗性,在复合材料表面上制造SiC,TAC和HFC涂层。 检测到涂层的消融性质,并在论文中讨论了烧蚀机理。 SiC和TAC涂层的中心区域在消融期间失败并表现出高烧蚀率; 它归因于如此高的消融温度,其氧化物的熔点(Ta2O5和SiO 2)是更高的熔点。 HFC涂层表现出最低的消融率。 原因是消融温度恰好在HFO2的烧结点和熔化温度之间,氧化物可以在消融期间表现为热阻挡涂层,并为C / C复合材料提供有效的保护。 可以表明碳化物涂层在其氧化物的茶金温度和熔点之间提供最佳消融保护。

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