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Durable anti-oxidation mechanism and failure analysis of the ZrSiO4 compound glass coating for carbon/carbon composites

机译:碳/碳复合材料ZRSIO4复合玻璃涂层的耐用抗氧化机理及失效分析

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摘要

In order to improve the anti-oxidation property of glass coating for aviation thermal structural components such as C/C airplane brake disc under extreme conditions up to 1473 K, ZrSiO4 is doped to improve the stability of the glass coating and to prolong its service life. The microstructures of the ZrSiO4 compound glass (ZSO-glass) coating after different oxidation time at 1473 K were studied. The anti-oxidation mechanism and failure of the coating was comprehensively analyzed. The results show that the novel ZSO-glass coating prepared by slurry method displayed excellent oxidation resistance and protected the carbon/carbon matrix at 1473 K for 573 h with only 0.33 wt% weight-loss, and it also displayed good thermal shock resistance. The excellent oxidation resistance of the coating system is attributed to self-healing effect of glass phase and toughening effect of ZrSiO4 in the coating. The fine ZrSiO4 particles can inhibit crystallization of glass coating while the agglomerated ZrSiO4 particles with a little larger size can pin microcracks in the glass phase during oxidation. The reason for the failure of ZSO-glass coating is that bubbles gradually grow up during oxidation and finally break through the ZSO-glass coating forming main oxygen diffusion channels. The service life of the ZSO-glass/SiC coating can be predicted by the bubble growth model.
机译:为了改善诸如C / C飞机制动盘的玻璃涂层的玻璃涂层的抗氧化性能,例如C / C飞机制动盘在最高的条件下,ZRSIO4被掺杂以改善玻璃涂层的稳定性并延长其使用寿命。研究了在1473 k下不同氧化时间后ZrSiO4化合物玻璃(ZSO-玻璃)涂层的微观结构。综合分析涂层的抗氧化机理和损失。结果表明,浆料法制备的新型ZSO-玻璃涂层显示出优异的抗氧化性,并在1473K下保护碳/碳基质573小时,仅为0.33重量%的重量损失,也显示出良好的抗热冲击性。涂层系统的优异抗氧化性归因于玻璃相的自愈合和锌涂层中ZrsiO4的增韧效果。细ZrSiO 4颗粒可以抑制玻璃涂层的结晶,同时聚集的ZrSiO4颗粒具有较大尺寸的较大尺寸的颗粒可以在氧化过程中销在玻璃相中的微裂纹。 ZSO-玻璃涂层失效的原因是气泡在氧化过程中逐渐升高,最后突破形成主要氧扩散通道的ZSO-玻璃涂层。可以通过气泡生长模型预测ZSO-玻璃/ SiC涂层的使用寿命。

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