[1]崔红,闫联生,刘勇琼,等.掺杂改性C/C复合材料研究进展[J].中国材料进展,2011,(11):013-17.
CUI Hong,YAN Liansheng,LIU Yongqiong,et al. Advances on Ceramic Hybird Modified Carbon/Carbon Composites[J].MATERIALS CHINA,2011,(11):013-17.
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掺杂改性C/C复合材料研究进展(
)
中国材料进展[ISSN:1674-3962/CN:61-1473/TG]
- 卷:
-
- 期数:
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2011年第11期
- 页码:
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013-17
- 栏目:
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特约研究论文
- 出版日期:
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2011-11-25
文章信息/Info
- Title:
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Advances on Ceramic Hybird Modified Carbon/Carbon Composites
- 作者:
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崔红; 闫联生; 刘勇琼; 张强; 孟祥利
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(西安航天复合材料研究所，陕西 西安 710025)
- Author(s):
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CUI Hong; YAN Liansheng; LIU Yongqiong; ZHANG Qiang; MENG Xiangli
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(Xi an Aerospace Composite Material Institute, Xian 710025，China)
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- 关键词:
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; 高温材料; C/C复合材料; 掺杂改性; 抗氧化
- 文献标志码:
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A
- 摘要:
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陶瓷掺杂改性碳/碳（C/C）复合材料在保持C/C复合材料原有优异高温力学性能及尺寸稳定性等特性的前提下，显著提高了C/C复合材料的高温抗氧化、抗烧蚀性能，且其具有可设计性和良好的抗热震性能等优势，是新型高超声速飞行器和新一代高性能发动机热防护部件的理想候选材料。综述了国内外在SiC陶瓷掺杂改性C/C复合材料，ZrC，ZrB2超高温陶瓷掺杂改性C/C复合材料以及TaC，HfC超高温陶瓷掺杂改性C/C复合材料等方面的最新研究进展和应用情况，并分析了陶瓷掺杂改性C/C复合材料目前研究及应用中存在的主要问题和今后潜在的研究发展方向。
- Abstract:
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Being the ideal candidate material for thermal protection parts in supersonic flight and the high performance rocket engine, carbon/carbon composites modified by ceramic hybrid have good oxidation and ablation resistance, designability, good thermal shock resistance as well as the inherent unique comprehensive properties, such as excellent mechanical properties and dimensional stability at high temperature. The present status of research and application of carbon/carbon composites modified by the SiC ceramics and ZrC, ZrB2, TaC, HfC ultrahigh temperature ceramics were summarized. The existing problems and the potential development direction on the investigation of the ceramic hybrid modification C/C composites were also proposed.
更新日期/Last Update:
2011-12-06