Advances in modifications and high-temperature applications of silicon carbide ceramic matrix composites in aerospace: A focused review

被引:180
|
作者
Wang, Xiulei [1 ]
Gao, Xiaodong [1 ]
Zhang, Zhenghe [1 ]
Cheng, Lisheng [1 ,2 ]
Ma, Haopeng [1 ]
Yang, Weimin [1 ,2 ]
机构
[1] Beijing Univ Chem Technol, Coll Mech & Elect Engn, Beijing 100029, Peoples R China
[2] Beijing Univ Chem Technol, State Key Lab Organ Inorgan Composites, Beijing 100029, Peoples R China
关键词
Aerospace materials; Ceramic matrix composites (CMCs); High-temperature mechanical properties; Modification measures; Silicon carbide (SiC); THERMAL-SHOCK RESISTANCE; SIC-BASED CERAMICS; SINGLE-SOURCE PRECURSOR; IN-SITU SYNTHESIS; MECHANICAL-PROPERTIES; CARBON-FIBER; OXIDATION BEHAVIOR; ABLATION BEHAVIOR; C/SIC COMPOSITES; TRIBOLOGICAL PROPERTIES;
D O I
10.1016/j.jeurceramsoc.2021.03.051
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
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 hightemperature applications.
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页码:4671 / 4688
页数:18
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