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    jsp.display-item.identifier=請使用永久網址來引用或連結此文件: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/62381

    题名: A Flapping MAV Micro Aerial Vehicle with PVDF-Parylene Composite Skin
    其它题名: 具壓電一具對二甲苯複合蒙皮之拍翼式微型飛行器
    作者: Yang, Lung-Jieh;Feng, Chao-Kang;Hsu, Cheng-Kuei;Ho, Jen-Yang;Feng, Guo-Hua;Shih, Hung-Ming;Shen, Yung-Kang
    贡献者: 淡江大學航空太空工程學系
    关键词: MAV;Flapping wing;PVDF;MEMS
    日期: 2007-01
    上传时间: 2011-10-18 20:42:11 (UTC+8)
    出版者: 中華民國航空太空學會
    摘要: he research of micro aerial vehicles (MAVs) is a new field which attracts much attention in the advanced aeronautical area. The flapping wing, proved by many natural flyers, is the most appropriate way of flying objects which sizes are less than 6 inches. However, there is still plenty of room for people to investigate the unsteady aerodynamic characteristic of flapping wings. In this paper, the flapping wing of lightweight and high strength is composed of the titanium-alloy frame and the parylene skin. Such an integration of fabrication needs the help of MEMS processing technique. In the wind-tunnel test of the flapping MAV, the signals from load cell and PVDF film are used to detect the on-site lift. Both of the lift signals from PVDF and the load-cell are accordant with the similar qualitative behavior. Finally, we integrate lithium-battery into the MAV to perform a successful free flight with a range of 10-15 meters.
    關聯: Journal of Aeronautics, Astronautics and Aviation. Series A 39(3), pp.195-201
    显示于类别:[航空太空工程學系暨研究所] 期刊論文


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