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Thermal shock resistance of continuous carbon fiber reinforced ZrC based ultra-high temperature ceramic composites prepared via Zr-Si alloyed melt infiltration

机译:Zr-Si合金熔体渗透制备连续碳纤维增强ZrC基超高温陶瓷复合材料的抗热震性

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摘要

Thermal shock resistance of continuous carbon fiber reinforced ZrC based ultra-high temperature ceramic matrix composite (C/C-ZrC) from ultra high temperatures (particularly 1500 degrees C) to the room temperature was evaluated using a novel self-developed equipment with high heating-cooling rates in controllable atmosphere. Residual strength and mass variation of the as-prepared composite under different thermal shock cycles and temperatures were tested to characterize the thermal shock resistance. Flexural strength of the composite slightly decreases initially without obvious weight loss below 1300 degrees C, while it decreases by relatively high values at 1300-1900 degrees C and then sharply decreases over 1900 degrees C with obvious increase of weight loss. Microstructure of the thermally shocked specimens was examined to reveal the thermal shock damage. Matrix cracking, interfacial debonding and matrix pores were clearly observed, which were the main reasons for the strength degradation of the composite thermally shocked for different cycles and temperatures.
机译:使用新型的自行研发的高温度设备,评估了连续碳纤维增强的ZrC基超高温陶瓷基复合材料(C / C-ZrC)从超高温(尤其是> 1500摄氏度)到室温的耐热冲击性。可控气氛中的加热-冷却速率。测试了所制备复合材料在不同热冲击周期和温度下的残余强度和质量变化,以表征其抗热冲击性能。复合材料的挠曲强度最初在1300℃以下略有下降,而没有明显的失重,而在1300-1900℃时则下降相对较高的值,然后在1900℃时急剧下降,且失重明显增加。检查了热冲击试样的微观结构,以揭示热冲击损伤。清楚地观察到基体开裂,界面剥离和基体孔,这是在不同的循环和温度下热冲击复合材料强度下降的主要原因。

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