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武装直升机抗坠毁设计研究

STUDY ON THE ARMED HELICOPTER CRASHWORT- HINESS DESIGN

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【作者】 杨嘉陵; 吴卫华;

【Author】 Yang Jialing Wu Weihua (Beijing University of Aeronautics & Astronautics)

【机构】 北京航空航天大学固体力学研究所!北京100083;

【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。

【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.

【关键词】 直升机; 抗坠毁; 生存力;
【Key words】 Helicopter Crashworthiness Survivability;
【基金】 航空科学基金资助! (97B5 10 42 )
  • 【文献出处】 机械工程学报 ,Chinese Journal of Mechanical Engineering , 编辑部邮箱 ,2001年05期
  • 【分类号】V275.1
  • 【被引频次】34
  • 【下载频次】561
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