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SiC whisker-toughened SiC oxidation protective coating for carbon/carbon composites

机译:碳/碳复合材料用SiC晶须增韧SiC氧化保护涂层

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摘要

Carbon/carbon (C/C) composites are one of the most promising high temperature structural materials for engine, aircraft and aerospace applications, in which C/C composites are required to operate in an oxidizing environment. However, the oxidation of C/C composites at temperatures above 723 K limits their use to inert atmosphere 1,2. Oxidation protective coatings are the logical choice for preventing C/C from oxidation at high temperatures. SiC ceramics are considered as the most suitable coating materials for C/C composites due to their excellent oxidation resistance and good compatibility with C/C substrates 3-6. However, thermal expansion mismatch between SiC and C/C composites will result in the crazing and debonding of SiC coating, and induce the failure of the coatings. According to the toughening mechanism including crack bridging due to whisker pull-out and crack deflection around whiskers 7,8, the toughness of SiC ceramic coatings could be increased by adding SiC whisker (SiCw) in them 9, which will improve the oxidation and thermal stress resistance of SiC ceramic coating.
机译:碳/碳(C/C)复合材料是发动机、飞机和航空航天应用中最有前途的高温结构材料之一,其中C/C复合材料需要在氧化环境中运行。然而,C/C复合材料在高于723 K的温度下氧化,限制了它们在惰性气氛中的使用[1,2]。氧化保护涂层是防止 C/C 在高温下氧化的合理选择。碳化硅陶瓷具有优异的抗氧化性和与C/C基材的良好相容性,被认为是最适合C/C复合材料的涂层材料[3-6]。然而,SiC和C/C复合材料之间的热膨胀不匹配会导致SiC涂层的裂纹和脱粘,并导致涂层的破坏。根据晶须拔出引起的裂纹桥接和晶须周围的裂纹偏转等增韧机理[7,8],通过添加SiC晶须(SiCw)可以提高SiC陶瓷涂层的韧性[9],从而提高SiC陶瓷涂层的抗氧化性和抗热应力性。

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