宇航学报

宇航学报 ›› 2021, Vol. 42 ›› Issue (4): 409-424.doi: 10.3873/j.issn.1000-1328.2021.04.002

• 综述 • 上一篇    下一篇

高超声速飞行器新型热防护机制研究进展

梁伟，金华，孟松鹤，杨强，曾庆轩，许承海   

  1. 哈尔滨工业大学特种环境复合材料技术重点实验室，哈尔滨 150080
  • 收稿日期:2020-05-12 修回日期:2020-07-03 出版日期:2021-04-15 发布日期:2021-04-15
  • 基金资助:
    国家自然科学基金(11972136)

Research Progress on New Thermal Protection Mechanism of  Hypersonic Vehicles

LIANG Wei, JIN Hua, MENG Song he, YANG Qiang, ZENG Qing xuan, XU Cheng hai   

  1. National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China
  • Received:2020-05-12 Revised:2020-07-03 Online:2021-04-15 Published:2021-04-15

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摘要： 从气动热载荷的来源出发，介绍了基于流动控制、光辐射操控、原子重组、电子耗散等物理机制的新型热防护机制的原理和进展。分别从环境和材料两方面实现对流热、化学热和辐射热的主动调控，进一步分析了高超声速飞行器新型热防护机制发展的特点和不足，对该领域未来研究的重点方向提出了建议。

关键词: 高超声速飞行器, 热防护机制, 对流热, 化学热, 辐射热

Abstract: Starting from the source of aerodynamic thermal load, the principles and progress of a new thermal protection mechanism based on the physical mechanism of flow control, optical radiation control, atomic reorganization, and electron dissipation are introduced. The active control of convection heat, chemical heat and radiant heat is realized from the aspects of regulating environment and materials, the characteristics and shortcomings of the development of a new thermal protection mechanism for hypersonic vehicles are further analyzed, and the suggestions on the key directions of future research in this field are put forward.

Key words: Hypersonic vehicle, Thermal protection mechanism; Convective heat, Chemical heat, Radiant heat

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