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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/96506

    Title: 可撓機翼架構誘導之仿生八字形拍翼
    Other Titles: A Biomimic Figure-Eight Flapping Induced by Flexible Wing Frames
    Authors: 徐振貴;施宏明;楊龍杰
    Contributors: 淡江大學機械與機電工程學系
    Keywords: 拍翼;微飛行器;八字形;Flapping;Micro aerial vehicle (MAV);Figure-eight
    Date: 2007-11
    Issue Date: 2014-03-07 11:53:50 (UTC+8)
    Abstract: 有別於傳統的拍翼機構為剛性的認定,本研究提議使用可撓式的碳纖維棒與聚對二甲苯薄膜,分別作為掌狀大小微飛行器之機翼骨架與機翼蒙皮。即便拍翼(齒輪連桿)傳動機構只是單自由度的四連桿(機構)設計,但上下拍翼的連動經由可撓性機翼的材質與外型設計,成功耦合到流向的前後振動,故使翼尖組合出三維的八字形拍翼軌跡。該八字形軌跡以高速攝影機成功拍攝驗證,且發生於接近或甚至超過18Hz 的拍翼頻率,本仿生機翼應用於全機重10gw 以下,翼展20cm 以下的拍翼微飛行器,已可持續飛行32 秒以上。飛行測試結果顯示,本仿生八字形拍翼軌跡可經由空氣彈性力學之本質而自動產生,無需藉助複雜精巧的三維機構設計。
    Relaxing from the conventional regarding of the "rigid" flapping mechanism, in this work the authors proposed to use the "flexible" carbon-fibers and parylene films as the wing frames for palm-size micro aerial vehicles (MAVs). By combining the coupling streamwise vibration of the wing frame and the driving flapping motion with one degree of freedom only, a figure-eight stroke of wing tips trajectory is verified via a high speed camera with the flapping frequency beyond 18 Hz. The experiment results conclude that this biomimic figure-eight flapping is done by the very nature of the aero-elastic interaction rather than the delicate 3D motion formulated purposely from the mechanism design.
    Relation: 2007中華民國航空太空學會第四十九屆航太學術研討會論文集,6頁
    Appears in Collections:[機械與機電工程學系暨研究所] 會議論文

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    可撓機翼架構誘導之仿生八字形拍翼 _中文摘要.docx摘要14KbMicrosoft Word153View/Open
    可撓機翼架構誘導之仿生八字形拍翼 _英文摘要.docx摘要14KbMicrosoft Word122View/Open

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