材料科学
复合材料
四方晶系
烧结
烧蚀
相(物质)
化学
有机化学
航空航天工程
工程类
作者
Yi Zhang,Dou Hu,Lingxiang Guo,Bing Liu,Xiaoshuang Wang,Qiangang Fu
摘要
Abstract The compactness of in situ protective film for carbon‐based composites during ablation is particularly important for improving their service life. Herein, La 2 O 3 ‐modified C/C‐ZrC composites were designed by vacuum filtration combined with reactive melt infiltration to construct an in situ dense protective structure. Experimental results show that adding La element could improve the cyclic ablation performance of C/C‐ZrC composites significantly. As the La 2 O 3 addition amount is 5.6 wt.%, the linear ablation rate of La 2 O 3 ‐modified C/C‐ZrC composites is –2.62 µm/s and 0.18 µm/s after exposure to an oxyacetylene flame (4.2 MW/m 2 ) for 40 s and 240 s, far superior to that of C/C‐ZrC composites (40 s, –6.2 µm/s). The excellent ablation resistance was attributed to the introduction of La element partially weakened Zr‐O bonds to induce more oxygen vacancies, which facilitated the sintering of ZrO 2 and eventually promoted the compactness and tetragonal phase stability of the Zr‐La‐O layer.
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