材料科学
碳化硅
航空航天
复合材料
陶瓷
陶瓷基复合材料
韧性
造型(装饰)
相(物质)
碳化物
基质(化学分析)
政治学
有机化学
化学
法学
作者
Xiulei Wang,Xiaodong Gao,Zhenghe Zhang,Lisheng Cheng,Haopeng Ma,Weimin Yang
标识
DOI:10.1016/j.jeurceramsoc.2021.03.051
摘要
This article is a detailed review of the measures to modify the high-temperature mechanical properties of silicon carbide ceramic matrix composites (SiC CMCs), namely toughness, high-temperature stability and wear resistance. Additionally, it briefly describes the common processing methods of the SiC CMCs and their application in the high-temperature field of aerospace. The advantages and disadvantages of various existing processing and molding methods for the SiC CMCs are also discussed. The high-temperature mechanical properties of the SiC CMCs are mainly affected by the properties of the matrix, added phase and interface. It is crucial to reduce the crystal defects of the matrix and select a suitable enhancement phase for an elevated performance. Moreover, it is important to improve the bonding at the interface between the enhancement phase and the matrix. This review is expected to provide useful information for the subsequent development of complex SiC CMCs for high-temperature applications.
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