• CN:11-2187/TH
  • ISSN:0577-6686

›› 2001, Vol. 37 ›› Issue (5): 1-6.

• 论文 •    下一篇

武装直升机抗坠毁设计研究

杨嘉陵;吴卫华   

  1. 北京航空航天大学固体力学研究所
  • 发布日期:2001-05-15

STUDY ON THE ARMED HELICOPTER CRASHWORTHINESS DESIGN

Yang Jialing;Wu Weihua   

  1. Beijing University of Aeronautics & Astronautics
  • Published:2001-05-15

摘要: 介绍了武装直升机抗坠毁的概念设计原理,提出了抗坠毁设计中的一些关键问题,为武装直升机抗坠毁设计提供理论指导。

关键词: 抗坠毁, 生存力, 直升机

Abstract: After the end of the conflict in Southeast Asia of Viet Nam, the US army draws a lesson from the conventional design of armed helicopters in which the crashworthiness requirement was not considered and hence leaded to heavy casualties during the conflict. The advanced technology of the crashworthiness design was first adopted in U.S. Army UH-60 Black Hawk and AH-64 Apache Helicopters and it was demonstrated that crash survival rate is increased significantly up to 95%. This study is focused on the basic design principles of helicopter crashworthiness and the key problems in the design specification. The purpose of the paper is to provide with some theoretical instruction for new type of armed helicopter crashworthiness design in China.

Key words: Crashworthiness, Helicopter, Survivability

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