材料科学
航空航天
陶瓷
复合材料
结构材料
烧蚀
政治学
工程类
航空航天工程
法学
作者
Ruize Gao,Shuibin Wang,Tianci Zhou,Tianxing Jiang,Lu Li,Qingbo Wen,Shasha Tao,Xiang Xiong
出处
期刊:Materials
[Multidisciplinary Digital Publishing Institute]
日期:2025-08-20
卷期号:18 (16): 3891-3891
被引量:1
摘要
C/C composites have excellent high-temperature mechanical properties and are one of the most promising high-temperature structural materials. However, poor oxidation and ablation resistance of the C/C composites in high-temperature oxygen-containing environments seriously hinder their practical applications. Ultrahigh-temperature ceramics (UHTCs)-modified C/C composites (C/C-UHTCs) are considered to be the most effective way to improve the oxidation and ablation resistance of C/C composites, demonstrating significant application prospects in aerospace and related fields. This article reviews recent research progress on C/C-UHTCs composites, including application prospects, performance testing methods, preparation techniques, phase composition, structural design principles, microstructural characteristics, as well as oxidation/ablation mechanisms. Addressing current challenges in C/C-UHTCs composites and future research directions are also proposed.
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