| 小型太阳能无人机超大展弦比轻质主梁设计 |
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| 引用本文： | 李冰,高永,郭卫刚,康小伟,孟浩.小型太阳能无人机超大展弦比轻质主梁设计[J].海军航空工程学院学报,2017,32(5):483-486. |
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| 作者姓名： | 李冰 高永 郭卫刚 康小伟 孟浩 |
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| 作者单位： | 海军航空大学,山东烟台 264001,海军航空大学,山东烟台 264001,海军航空大学,山东烟台 264001,海军航空大学,山东烟台 264001,海军航空大学,山东烟台 264001 |
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| 摘 要： | 太阳能无人机表面需要铺设太阳能电池,这就要求太阳能无人机的结构要同时满足不影响太阳能电池效率的光学特性和要达到足够强度、刚度的力学特性。文章针对小型太阳能飞机超大展弦比机翼进行轻质化结构设计,过程中充分考虑超大展弦比机翼的柔性变形,对比不同的设计方案并提出合理设计方案。
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| 关 键 词： | 太阳能 超大展弦比 轻质结构 |
Design of Large Aspect Ratio Light Beam for Small Solar UAV |
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| LI Bing,GAO Yong,GUO Weigang,KANG Xiaowei and MENG Hao.Design of Large Aspect Ratio Light Beam for Small Solar UAV[J].Journal of Naval Aeronautical Engineering Institute,2017,32(5):483-486. |
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| Authors: | LI Bing GAO Yong GUO Weigang KANG Xiaowei and MENG Hao |
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| Affiliation: | Naval Aviation University, Yantai Shandong 264001, China,Naval Aviation University, Yantai Shandong 264001, China,Naval Aviation University, Yantai Shandong 264001, China,Naval Aviation University, Yantai Shandong 264001, China and Naval Aviation University, Yantai Shandong 264001, China |
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| Abstract: | Solar UAV surface lays solar cell, which requires the structure of solar UAV to satisfy the optical properties doesnot affect the efficiency of solar cell and achieving sufficient strength, stiffness and mechanical properties. The small solarpowered aircraft large aspect ratio wing of lightweight was structural designed, the large aspect ratio wing flexible deforma.tion process was fully consided, different design schemes were comparal and the reasonable design scheme was put for.ward. |
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| Keywords: | solar UAV large aspect ratio lightweight structure |
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