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Influence of infiltration temperature on the microstructure and oxidation behavior of SiC-ZrC ceramic coating on C/C composites prepared by reactive melt infiltration

机译:渗透温度对反应熔渗C / C复合材料SiC-ZrC陶瓷涂层组织和氧化行为的影响

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SiC-ZrC ceramic coating on C/C composites was prepared by reactive melt infiltration (RMI) using a powder mixture composed of Zr, Si and C as the infiltrator. The phase composition and microstructure of the ceramic coating were characterized by X-ray diffraction (XRD), scanning electron microscopy (SEM) and energy dispersive X-ray spectroscopy (EDS). The oxidation resistance of the as-prepared composites was tested at 1550 degrees C in static air. The results indicate that the infiltration temperature has remarkable effects on the phase composition and microstructure of the ceramic coating, as well as on the oxidation resistance of the composites. The SiC-ZrC coated C/C composites prepared at 2000 degrees C exhibit an excellent oxidation resistance. They gain weight about 5.9 wt% after oxidation at 1550 degrees C in static air for 5 h, whereas the SiC-ZrC coated C/C composites prepared at 1800 degrees C lose weight about 3.2 wt%. As a comparison, SiC coated C/C composites prepared at 2000 degrees C by RMI show an inferior oxidation resistance. After 5 h oxidation, SiC coated C/C composites are severely damaged and their weight loss reaches up to 44.3 wt%. The outstanding oxidation resistance of the SiC-ZrC coated C/C composites prepared at 2000 degrees C can be attributed to the rapid formation of a continuous glass-like layer composed of ZrO2, ZrSiO4 and SiO2, which covers the surface of the composites and retards the oxygen diffusion and the attack on the underlying C/C substrate. For SiC coated C/C composites, the large SiC particles formed on the surface of the composites are difficult to oxidize rapidly and so a continuous and dense SiO2 layer cannot be formed in time to significantly hinder fast oxygen diffusion leading to the consequent severe oxidation of the C/C substrate. (C) 2014 Elsevier Ltd and Techna Group S.r.l. All rights reserved.
机译:C / C复合材料上的SiC-ZrC陶瓷涂层是通过使用Zr,Si和C组成的粉末混合物作为渗透剂,通过反应熔体渗透(RMI)制备的。通过X射线衍射(XRD),扫描电子显微镜(SEM)和能量色散X射线光谱(EDS)表征了陶瓷涂层的相组成和微观结构。在静态空气中于1550摄氏度下测试所制备复合材料的抗氧化性。结果表明,渗透温度对陶瓷涂层的相组成和微观结构以及复合材料的抗氧化性具有显着影响。在2000摄氏度下制备的SiC-ZrC涂层C / C复合材料表现出优异的抗氧化性。在1550摄氏度的静态空气中氧化5小时后,它们的重量增加了约5.9 wt%,而在1800摄氏度下制备的SiC-ZrC涂层的C / C复合材料的重量减少了约3.2 wt%。作为比较,通过RMI在2000℃下制备的SiC涂覆的C / C复合材料显示出较差的抗氧化性。氧化5小时后,SiC涂层的C / C复合材料受到严重破坏,其重量损失高达44.3 wt%。在2000摄氏度下制备的SiC-ZrC涂层C / C复合材料具有出色的抗氧化性,这归因于快速形成由ZrO2,ZrSiO4和SiO2组成的连续玻璃状层,该层覆盖了复合材料的表面并阻滞了复合材料。氧扩散和对下面的C / C基材的侵蚀。对于SiC涂层的C / C复合材料,在复合材料表面形成的大SiC颗粒难以快速氧化,因此无法及时形成连续而致密的SiO2层,从而严重阻碍了氧气的快速扩散,从而导致氧化严重。 C / C基板。 (C)2014 Elsevier Ltd和Techna Group S.r.l.版权所有。

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