摘要
Continuous fiber reinforced silicon carbide ceramic matrix composites were developing towards possessing self-healing properties for the need of high thrust mass ratio aerospace-engine working in thermal oxidizing environment. The microstructure and properties of a self-healing silicon carbide matrix composite were introduced. The mechanism of toughness and stiffness of the composite and the self-healing behaviors were commented. The application progress of self-healing silicon carbide component was summarized. Manufacturing method and technique feature were reviewed. Multi-component and multi-layer microstructure was the key point for this composite possessing self-healing and toughing properties, and oxidation resistant system which exhausted O2 and sealed crack in each layer. This self-healing silicon carbide matrix composite could not only meet the requirements of for aerospace-engine service but decrease weight remarkably, increased thrust-weight ratio in return.
源语言 | 英语 |
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页(从-至) | 226-232 |
页数 | 7 |
期刊 | Hangkong Cailiao Xuebao/Journal of Aeronautical Materials |
卷 | 26 |
期 | 3 |
出版状态 | 已出版 - 6月 2006 |
已对外发布 | 是 |