复合材料科学与工程 ›› 2022, Vol. 0 ›› Issue (10): 107-118.DOI: 10.19936/j.cnki.2096-8000.20221028.016

• 综述 • 上一篇    下一篇

高超声速飞行器热防护用超高温复合材料的研究进展

刘永胜, 曹立阳, 张运海, 曹晔洁, 王晶, 董宁   

  1. 西北工业大学 材料学院,西安710072
  • 收稿日期:2022-06-27 出版日期:2022-10-28 发布日期:2022-11-01
  • 作者简介:刘永胜(1975-),男,博士,教授,主要从事陶瓷基复合材料的高导热耐烧蚀、抗水氧腐蚀以及3D打印等方面的研究,yongshengliu@nwpu.edu.cn。
  • 基金资助:
    国家自然科学基金(92060202)

Research progress on ultra-high temperature composites for thermal protection of hypersonic vehicles

LIU Yong-sheng, CAO Li-yang, ZHANG Yun-hai, CAO Ye-jie, WANG Jing, DONG Ning   

  1. School of Material Science and Engineering, Northwestern Polytechnical University, Xi'an 710072, China
  • Received:2022-06-27 Online:2022-10-28 Published:2022-11-01

摘要: 热防护系统是高超声速飞行器的关键技术之一,决定了飞行器研制的成败,而高温热防护材料则直接决定了热防护系统的性能。本文综述了以C/C复合材料、C/SiC复合材料、C/UHTC复合材料等为代表的热防护用超高温复合材料的研究进展,并重点分析了近年来超高温复合材料导热和烧蚀性能相关的研究进展,进而提出了未来发展方向,为热防护用超高温复合材料的发展提供参考。

关键词: 高超声速飞行器, 热防护材料, C/C, C/SiC, C/UHTC, 超高温复合材料

Abstract: Thermal protection system (TPS) is one of the key technologies of hypersonic vehicles, determining the success of its development. And the high-temperature thermal protection materials directly determine the performance of the TPS. In this paper, the research status of ultra-high temperature composites for thermal protection application such as C/C, C/SiC and C/UHTC composites was introduced. Then, the research progress on thermal conduction and ablation performances of the C/C, C/SiC and C/UHTC composites were mainly discussed, and the future directions were proposed. This paper is expected to provide a reference for the development of ultra-high temperature composites for thermal protection.

Key words: hypersonic vehicles, thermal protection materials, C/C, C/SiC, C/UHTC, ultra-high temperature
composites

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