| 武装直升机抗坠毁设计研究 |
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| 引用本文： | 杨嘉陵,吴卫华.武装直升机抗坠毁设计研究[J].机械工程学报,2001,37(5). |
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| 作者姓名： | 杨嘉陵 吴卫华 |
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| 作者单位： | 北京航空航天大学固体力学研究所 |
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| 基金项目： | 航空科学基金资助! (97B5 10 42 ) |
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| 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。
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| 关 键 词： | 直升机 抗坠毁 生存力 |
STUDY ON THE ARMED HELICOPTER CRASHWORT- HINESS DESIGN |
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| Yang Jialing,Wu Weihua.STUDY ON THE ARMED HELICOPTER CRASHWORT- HINESS DESIGN[J].Chinese Journal of Mechanical Engineering,2001,37(5). |
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| Authors: | Yang Jialing Wu Weihua |
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| Affiliation: | Beijing University of Aeronautics & Astronautics |
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| 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. |
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| Keywords: | Helicopter Crashworthiness Survivability |
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