材料科学
热解炭
复合数
微观结构
碳化锆
复合材料
烧蚀
碳纤维
单斜晶系
碳化物
化学工程
热解
晶体结构
结晶学
化学
工程类
航空航天工程
作者
Wen Zhou,Li Ping Ran,Ke Peng,Yi Cheng Ge,Haijun Wu,Mao Zhong Yi
标识
DOI:10.1002/adem.201500206
摘要
A carbon/carbon–ZrC(C/C–ZrC) composite was fabricated by reactive infiltration of a Zr–40 wt% Cu powder mixture. The C/C–ZrC composite was composed of C, ZrC, and residual Cu. Continuous ZrC layers around the pyrolytic carbon and isolated ZrC particles dispersed in Cu were detected. Linear ablation rate of the composite increased with the increase of ablation time. Ablation surface of the composite was mainly composed of monoclinic ZrO 2 , while the quantity of Cu and Cu 2 O decreased with the increase of ablation time. The better ablation resistance of the C/C–ZrC composite was mainly attributed to the protective ZrO 2 layer and the cooling effect of Cu.
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