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研究生: 林哲旭
Lin, Che-Shu
論文名稱: 振翅翼飛行載具之探討
Study on Ornithopter
指導教授: 楊文彬
Young, Wen-Bin
學位類別: 碩士
Master
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2005
畢業學年度: 93
語文別: 中文
論文頁數: 81
中文關鍵詞: 拍翅翼振翅翼
外文關鍵詞: flapping-wing, ornithopter
相關次數: 點閱:126下載:12
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  •   人類已藉由各式各樣的飛行載具來飛行約一世紀,雖然人類的飛行靈感取源於鳥類的飛行,但我們卻不是非常明瞭其飛行原理。 本文藉由對四連桿機構的概念,設計完整的拍翅機構來模擬小鳥的動作,並可以控制向上及向下拍動的角度。在實驗當中主要是進行空氣動力特性的探討(升力、推力等),瞭解其與風速、頻率以及攻角之間的關連,並藉此探討與一般固定翼飛機有何不同之處。如此一來,將有利後續研究者對這方面的研究有初步的認知並加以改進,日後將拍翅翼廣泛運用於生活的各方面上。

      Human beings flying with the help of aircraft of various kinds have been able to fly for about one century. Although the flapping wings of animals served as an inspiration to pioneers of human flight, we don’t really understand how they work. In this thesis, we employ the concept of four- bar linkage to design a flapping mechanism which simulates the flapping motion of a bird. The upstroke angle and downward angle can be varied in the design. This experiment focuses on aerodynamic characters including the lift and thrust. The effects of frequency, wind velocity and angle of attack on the left and thrust were investigated. This research provides some preliminary understanding to the flapping wing, which could give some information for the following research.

    授權書 論文摘要 英文摘要 誌謝 目錄……………………………………………………………………………I 表目錄…………………………………………………………………….…IV 圖目錄………………………………………………………………………. V 符號說明…………………………………………………………………..VIII 第一章緒論……………………………………………………………….. 1 1.1 前言…………………………………………………………………... 1 1.2 文獻回顧……………………………………………………………... 2 1.3 研究目的……………………………………………………………... 7 第二章研究方法………………………………………………………….. 8 2.1 四連桿機構…………………………………………………………... 8 2.1.1 雙平行曲柄四連桿機構……………….……………………….9 2.1.2 非平行等長曲柄連桿機構…………………..…………………9 2.1.3 曲柄搖桿機構………………..………………………………..10 2.1.4直拉桿機構………..…………………………………………...10 2.2 角度問題……………………………………………………………..11 2.3 實驗設計……………………………………………………………. 15 第三章實驗方法………………………………………………………… 18 3.1 複材翅膀之設計過程………………………………………………. 18 3.1.1 材料與尺寸…………………………..……………………… 18 3.1.2 製作設備……………………………………………..……… 19 3.1.3 製作流程……………………………..……………………… 20 3.2 拍翅翼機構之製作…………………………………………………. 21 3.2.1 材料與設計…………………..……………………………… 21 3.2.2 製作設備………………………..…………………………… 22 3.2.3 製作過程………………………..…………………………… 22 3.3 升力量測……………………………………………………………. 23 3.3.1 實驗設備………………………..…………………………… 23 3.3.2 升力量測之流程…………..………………………………… 24 3.4 推力量測……………………………………………………………. 25 3.4.1 實驗設備…………………..………………………………… 25 3.4.2 推力量測之流程…………………………………..………… 25 第四章實驗結果與討論………………………………………………… 26 4.1 升力…………………………………………………………………. 26 4.2 推力…………………………………………………………………. 29 4.3 空氣動力特性………………………………………………………..30 第五章結論與建議……………………………………………………… 33 5.1 結論…………………………………………………………………. 33 5.2 未來工作與建議……………………………………………………. 34 參考文獻…………………………………………………………………….36 附表………………………………………………………………………….39 附圖………………………………………………………………………….46 自述 著作權聲明

    [1] Y.C. Tai, C.M. Ho, S.W. Lee, “MEMS wing technology for a battery-powered ornithopter”, Micro Electro Mechanical System, 799-804, 2000.

    [2] F.E. Mehler, “The Structure testing and Modification of a Full-Scale Ornithopter’s Wing Spars,” M.A.Sc. Thesis, University of Toronto Institute for Aerospace Studies, 1997.

    [3] P.S. Sanjay, “The aerodynamics of insect flight”, The Fournal of Experimental Biology, Vol. 206, 4191-4208, 2003.

    [4] W. Shyy, M. Berg, D Ljungqvist, “Flapping and flexible wings for biological and micro air vehicles” Aerospace Sciences, Vol. 35, 455-505, 1999 .

    [5] J.D. DeLaurier, “An aerodynamic model for flapping-wing flight”, Aeronautical Journal, 125-130, April 1993.

    [6] J.D. DeLaurier, J.M. Harris, “A study of mechanical flapping-wing flight”, Aeronautical Journal, 277-286, Oct. 1993.

    [7] J.D. DeLaurier, “An Ornithopter wing design”, Canadian Aeronautics and Space Journal, Vol. 40, No. 1, 10-18, March 1994.

    [8] P.G. Ifju, D.A. Jenkins, W. Shyy, “Flexible-Wing-Based Micro Air Vehicles”, American Institute of Aeronautics and Astronautics, 1-13, 2002.

    [9] C.H. Greenewalt, “Dimensional relationships for flying animals”, Smithson Misc Collect, Vol. 144, 1-46, 1962.

    [10] C.J. Pennycuick, “Wingbeart frequency of birds in steady cruising flight: new data and improved oredictions”, Journal of Experimental Biology, Vol. 199, 1613-1618, 1996.

    [11] S.J. Kirkpatrick , “Scale effects on the stresses and safety factors in the wing bones of birds and bats”, Journal of Experimental Biology, Vol. 190, 195-215, 1994.

    [12] A.M. Lippisch, “Man Powered Flight in 1929,” Journal of the Royal Aeronautical Society, Vol. 64, 395-398, July 1960.

    [13] T.N. Pornsin-Sirirak, Y.C. Tai, H. Nassef, C.M. Ho, “Flexible parylene actuator for micro adaptive flow control.” Micro Electro Mechanical System, 2001. MEMS 2001. The 14th IEEE Internation Conference , 511-514, Jan. 2001.

    [14] T.N. Pornsin-sirirak, Y.C. Tai, H. Nassef, C.M. Ho, “Titanium-alloy MEMS wing technology for a micro aerial vehicle application,” Sensors and Actuators, A 89, 95-103, 2001.

    [15] N. Pornsin-Sirirak, M. Liger, Y.C. Tai, S. Ho, C.M. Ho, “Flexible parylene-valved skin for adaptive flow control”, Micro Electro Mechanical System, 2002. The Fifteenth IEEE International Conference, 101-104, Jan. 2002.

    [16] R. Madangopal, Z.A. Khan, S.K. Agrawal, “Engergetics Based Design of Small Flapping Wing Air Vehicles”, Robotics and Automation, Vol. 3, 2367-2372, 2004.

    [17] N. Miki, I. Shimoyama, “Analysis of the performance of small magnetic rotating wings for use in microrobots”, Robotics and Automation, 1998. Vol. 4, 3065-3070, May 1998.

    [18] F.O. Lehmann, “Aerial locomotion in flies and robots: kinematic control and aerodynamics of oscillating wings”, Arthropod Structure and Development, Vol. 33, issue 3, 331-345, 2004.

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