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Carbon fiber reinforced ZrC based ultra-high temperature ceramic matrix composite subjected to laser ablation: Ablation resistance, microstructure and damage mechanism

机译:基于碳纤维增强ZRC的超高温陶瓷基质复合材料进行激光烧蚀:消融电阻,微观结构和损伤机制

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摘要

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.
机译:在不同激光功率密度(LPD)和时间段下,使用激光烧蚀试验方法研究了通过合金反应熔体渗透制备的碳纤维增强ZRC基于超高温陶瓷基质复合物的抗热性能和损伤机理。复合材料的烧蚀损伤明显增强,随着LPD的增加,随着延长的测试时间而减少。在消融测试期间,熔融ZrO2保护层原位形成,显着提高了复合材料的消融性能。提出了用不同LPD测试的复合材料的烧蚀微观结构,并提出了通过三个不同时段的消融机制。在第一时期,测试温度低,敏感损伤被认为主要由碳,Zrc和Zr2Si阶段的氧化控制。随着测试温度的增加,通过在氧化阶段形成的ZrO2和SiO 2蒸发来控制消融损伤。在最高测试温度的最后一段时间内,通过反复擦除和新的熔融ZrO2保护层的新形成,消融损坏变得协同主导。

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