| 无人机中翼与尾撑之间易损连接结构研究 |
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| 引用本文： | 党英,马晓平.无人机中翼与尾撑之间易损连接结构研究[J].航空计算技术,2006,36(5):87-89. |
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| 作者姓名： | 党英 马晓平 |
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| 作者单位： | 1. 西北工业大学,航空学院,陕西,西安,710072;西北工业大学,无人机研究与发展中心,陕西,西安,710072
2. 西北工业大学,无人机研究与发展中心,陕西,西安,710072 |
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| 摘 要： | 针对伞降回收双尾撑后推式气动布局的中小型无人机在非正常着陆情况下中翼损伤的问题,分析了中翼损伤的原因及减少其受损的途径,论证了在尾撑上设置易损连接结构的可行性,给出了在尾撑上设置易损连接结构的原理和方法,有效地解决了此问题.
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| 关 键 词： | 无人机 中翼 尾撑 |
| 文章编号： | 1671-654X(2006)05-0087-03 |
| 修稿时间： | 2006年6月28日 |
Research of the Damageable Connection Structure between UAV's Mid-wing and Boom |
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| DANG Ying,MA Xiao-ping.Research of the Damageable Connection Structure between UAV''''s Mid-wing and Boom[J].Aeronautical Computer Technique,2006,36(5):87-89. |
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| Authors: | DANG Ying MA Xiao-ping |
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| Abstract: | This paper focuses on the problem of crucial components damage of pint and medium-sized unmanned air vehicles that adopts the general layout of double booms,and a push forward propeller engine in the case of hard landing.The reason of mid-wing damage and the method of reduce damage are analyzed.Feasibility of boom connection joint that is susceptible to damage is demonstrated,the principle is given,and the problem is resolved efficaciously. |
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| Keywords: | unmanned air vehicle mid-wing boom |
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