放电等离子烧结
材料科学
热解炭
图层(电子)
陶瓷
烧结
烧蚀
复合材料
碳纤维
化学工程
热解
复合数
工程类
航空航天工程
作者
Chuangfang Tao,Huanyi Liao,Bin Chen,Weiguo Mao,Jie Wang,Cuiying Dai,Zheqiong Fan,Zhe Zhou,Jinglv Zuo
标识
DOI:10.1016/j.corsci.2024.111873
摘要
The (PyC-Csf)/ZrB2-SiC-ZrC ceramics are fabricated by reactive spark plasma sintering (RSPS) at 1200 °C. The sample has a low density and intact pyrolytic carbon modified carbon fiber (PyC-Csf). After three cycles of ablation (heat flux = 2.38 MW/m2, t = 120 s), samples demonstrate excellent resistance to oxidative ablation. The mass recession rate and linear recession rate for the sample are 3.41 g/m2∙s and 0.68 µm/s, respectively. Excessive content of carbon destroys the oxide layer by forming large amounts of CO2 during the ablation process. The inner layer of intact PyC-Csf aggregates around the borosilicate which are denser in the oxide layer. Finally, a porous ZrO2-SiO2 layer and a dense ZrO2-SiO2-Csf layer are formed on the surface of the sample which resists ablation.
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