航空学报 > 2022, Vol. 43 Issue (6): 527590-527590   doi: 10.7527/S1000-6893.2022.27590

高超声速飞行器强度技术的现状、挑战与发展趋势

孙聪   

  1. 中国航空研究院, 北京 100029
  • 收稿日期:2022-06-07 修回日期:2022-06-20 出版日期:2022-06-15 发布日期:2022-06-17
  • 通讯作者: 孙聪

Development status, challenges and trends of strength technology for hypersonic vehicles

SUN Cong   

  1. Chinese Aeronautical Establishment, Beijing 100029, China
  • Received:2022-06-07 Revised:2022-06-20 Online:2022-06-15 Published:2022-06-17

摘要: 高超声速飞行器作为一种前沿科技武器装备,对国家安全和利益具有重要战略作用,目前已成为航空航天领域的研究热点,在世界范围内的竞争态势日趋激烈。先进材料与结构设计是支撑高超声速飞行器研制的基础关键技术,极端严酷服役环境下材料与结构的强度问题依然是制约该类飞行器研制的瓶颈。本文回顾了过去几十年来高超声速飞行器领域的结构强度问题和演化特点,结合当前型号发展需求与技术发展趋势,剖析了当前结构强度技术在支撑高超声速飞行器研制方面的现状与短板,探讨了未来该领域内强度问题将呈现出的新需求、新特点及新方法。总结提出了未来高超声速飞行器结构强度领域的前沿发展方向。

关键词: 高超声速飞行器, 材料与结构, 结构强度, 地面试验, 多场耦合

Abstract: As a type of hi-tech weapon, hypersonic vehicle plays an important strategic role in national security and benefits. It has now become a research hotspot in the field of aerospace, and the competition is becoming increasingly fierce all over the world. Advanced material and structure design is a basic key technology to support the development of hypersonic vehicle. The strength of materials and structures in extremely severe service environments is still a key issue restricting the development of this type of aircraft. This paper reviews the structure strength problems and evolution characteristics in the field of hypersonic vehicles in the past few decades. Combined with the current vehicle model development demand and technology development trend, this paper analyzes the current situation and shortcomings of structure strength technology in supporting the development of hypersonic vehicles and discusses the new requirements, new characteristics and new methods of strength problems in this field in the future. Finally, the future development direction in the field of hypersonic vehicle structure strength is proposed after summarization.

Key words: hypersonic vehicle, material and structure, structure strength, ground test, multi-field coupling

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