自愈合碳化硅陶瓷基复合材料研究及应用进展

张立同 成来飞 徐永东 刘永胜 曾庆丰 董宁 栾新刚

张立同, 成来飞, 徐永东, 刘永胜, 曾庆丰, 董宁, 栾新刚. 自愈合碳化硅陶瓷基复合材料研究及应用进展[J]. 航空材料学报, 2006, 26(3): 226-232.
引用本文: 张立同, 成来飞, 徐永东, 刘永胜, 曾庆丰, 董宁, 栾新刚. 自愈合碳化硅陶瓷基复合材料研究及应用进展[J]. 航空材料学报, 2006, 26(3): 226-232.
ZHANG Li-tong, CHENG Lai-fei, XU Yong-dong, LIU Yong-sheng, ZENG Qing-feng, DONG Ning, LUAN Xin-gang. Progress on Self-Healing Silicon Carbide Ceramic Matrix Composites and Its Applications[J]. Journal of Aeronautical Materials, 2006, 26(3): 226-232.
Citation: ZHANG Li-tong, CHENG Lai-fei, XU Yong-dong, LIU Yong-sheng, ZENG Qing-feng, DONG Ning, LUAN Xin-gang. Progress on Self-Healing Silicon Carbide Ceramic Matrix Composites and Its Applications[J]. Journal of Aeronautical Materials, 2006, 26(3): 226-232.

自愈合碳化硅陶瓷基复合材料研究及应用进展

详细信息
    作者简介:

    张立同(1938- ),女,中国工程院院士,主要从事陶瓷基复合材料研究.

  • 中图分类号: TB332;TQ174

Progress on Self-Healing Silicon Carbide Ceramic Matrix Composites and Its Applications

  • 摘要: 为了满足高推重比航空发动机长时热力氧化环境的使用需求,连续纤维增韧碳化硅陶瓷基复合材料正朝自愈合方向发展。本文介绍自愈合碳化硅陶瓷基复合材料的微结构与性能,自愈合与强韧化机理,制造方法和工艺特点及其在航空发动机热端部件的应用情况,表明多元多层微结构形成了“层层设防,就地消灭”的氧化防御体系,是复合材料实现自愈合与强韧化的关键。自愈合碳化硅陶瓷基复合材料能够满足发动机高温服役环境要求,显著降低发动机的结构重量,从而有效提高发动机的推重比。

     

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出版历程
  • 收稿日期:  2006-02-20
  • 修回日期:  2006-03-20
  • 刊出日期:  2006-06-01

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