材料科学
烧蚀
复合材料
微观结构
复合数
激光烧蚀
氧化剂
陶瓷
陶瓷基复合材料
图层(电子)
激光器
光学
物理
有机化学
工程类
航空航天工程
化学
作者
Yonggang Tong,Yongle Hu,Xiubing Liang,Zhibing Zhang,Yang Li,Zhaoke Chen,Xiang Xiong,Manyu Hua
标识
DOI:10.1016/j.ceramint.2020.02.236
摘要
Abstract Ablation-resistant performance and damage mechanism of carbon fiber reinforced ZrC based ultra-high temperature ceramic matrix composite prepared via alloyed reactive melt infiltration were investigated using a laser ablation testing method under different laser power densities (LPD) and time periods. Ablation damage of the composite was obviously enhanced tested with increasing LPD and reduced with prolonging tested time. A fused ZrO2 protecting layer was in situ formed during ablation testing, significantly improving the composite's ablation-resistant performance. Ablated microstructures of the composites tested with different LPD were characterized and an ablation mechanism going through three distinct periods was proposed. In the first period, the testing temperature is low and ablation damage was thought to be mainly controlled by the oxidation of carbon, ZrC and Zr2Si phases. With the increase of testing temperatures, ablation damage became controlled by evaporating of ZrO2 and SiO2 formed in oxidizing stage. In the final period with the highest testing temperatures, ablation damage became synergistically dominated by repeatedly scouring away and new formation of the fused ZrO2 protecting layer.
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