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直升机尾传动轴抗弹击损伤研究综述
作者:
作者单位:

1.南京航空航天大学直升机传动技术国家级重点实验室，南京 210016;2.中国人民解放军陆航研究所，北京 101121;3.中国航发湖南动力机械研究所直升机传动技术国家级重点实验室，株洲 412002

通讯作者:

王旦，男，副教授，E-mail： wangdan_053@nuaa.edu.cn。

基金项目:

国家自然科学基金（52005253）；直升机传动技术国家级重点实验室开放基金（HTL-A-21G07，HTL-A-22K01）。


Research on Ballistic Damage and Anti-ballistic Design of Helicopter Tail Drive Shaft: An Overview
Author:
Affiliation:

1.National Key Laboratory of Science and Technology on Helicopter Transmission， Nanjing University of Aeronautics & Astronautics， Nanjing 210016， China;2.Army Aviation Research Institute， PLA， Beijing 101121， China;3.National Key Laboratory of Science and Technology on Helicopter Transmission， Hunan Aviation Powerplant Research Institute， AECC， Zhuzhou 412002， China

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    摘要:

    直升机尾传动轴在军事应用中容易遭受弹击损伤，严重影响直升机飞行安全。为此，国内外开展了大量直升机尾传动轴抗弹击损伤研究工作。本文首先从军事需求角度阐述尾传动轴抗弹击损伤研究的重要意义。然后从尾传动轴弹击损伤评定指标、研究方法、影响因素以及尾传动轴抗弹击性能提升方法4方面介绍了国内外直升机尾传动轴抗弹击损伤研究现状及其发展趋势。最后论述了国内在尾传动轴抗弹击损伤研究方面的不足之处，并从材料性能参数测试、新型数值仿真模拟方法、尾传动轴抗破片冲击研究和弹击复合材料尾传动轴数值模拟4方面展望了我国在尾传动轴抗弹击损伤方面亟需开展的研究。

    Abstract:

    Helicopter tail drive shaft is susceptible to ballistic damage in military applications， significantly compromising the safety of helicopter flight. Consequently， extensive research on ballistic damage and anti-ballistic design of helicopter tail drive shaft has been conducted both domestically and internationally. Firstly， the military significance of researching the ballistic damage and anti-ballistic design of helicopter tail drive shaft is elaborated. Secondly， the current research status and development trends of ballistic damage and anti-ballistic design of helicopter tail drive shaft at home and abroad are detailed from four aspects： evaluation criteria， research methods， influencing factors， and methods for improving anti-ballistic performance of the tail drive shaft. Finally，the shortcomings of domestic research in this area are discussed， and the research directions that urgently need to be carried out in the future are prospected from the views of material property testing， new numerical simulation methods， research on damage by fragment penetration and numerical simulation of ballistic damage of composite tail drive shaft.

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王旦,未雷,李鹏,徐鹏行,王希,李坚,朱如鹏.直升机尾传动轴抗弹击损伤研究综述[J].南京航空航天大学学报,2024,56(2):197-207

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  • 收稿日期:2023-08-02
  • 最后修改日期:2024-01-16
  • 在线发布日期: 2024-04-05
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