摺翼型拍撲翼機構分析與設計

小型人造飛行器中是為了能夠在惡劣環境和危險區域從事勘查與聯繫的工作而設計的。小型飛行器以翅膀的運動模式可分類為固定翼、旋轉翼、以及拍撲翼等三大類。本研究目的僅是以鳥類或昆蟲等飛行生物之翅膀的拍打模式，設計具有翅膀且近似鳥類飛行的拍打及折翅運動的小型飛行器之摺翼型拍撲翼機構。本研究首先是收集與分析現有拍撲翼機構的相關資料，接著歸納出機構的拓撲構造特性及設計限制，以作為創思摺翼型拍撲翼機構的拓撲構造基礎，然後根據顏氏創意性機構設計方法，合成出符合限制條件的可行特殊化運動鏈，再利用向量迴路法針對所設計的機構作運動分析，最後在電腦上發展動畫以驗證本研究所提理論的可行性。本研究共得到65個新型摺翼型拍撲翼機構。

關鍵字

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並列摘要

The little air vehicles to design for adverse circumstances and investigate into danger area. The little air vehicles regard the running mode classification of the wing as the Fixed-Wing, Rotary-Wing, and Flapping-Wing etc. the three major types. According to the flight mod of the flight creature, this objective of the study is to design new folding and flapping wing mechanisms that can achieve the rotary and flapping motions. First, this work provided the requirements and constraints of folding and flapping wing mechanisms. Secondly, this work used the Yan’s creative mechanism design methodology to synthesis the feasible specialized kinematics chains and obtained satisfied morphing-wing mechanisms. Thirdly, this work designed the folding and flapping wing mechanisms dimensions by referring the flight mod of the flight creatures. Finally, we developed a computer simulation program of the designed folding and flapping wing mechanism.The results of his work are 659 new s folding and flapping wing mechanisms are designed.

並列關鍵字

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參考文獻

[4] Dial, K. P., “An Inside Look at How Birds Fly: Experimental Studies of the Internal and External Processes Controlling Flight,” Report to the Aerospace Profession, 38th Symp Proc, The Beverly Hilton, Beverly Hills, CA., 1994.

[11] Smith, M.J.C., “Simulating Moth Wing Aerodynamics: Towards the Development of Flapping-Wing Technology,” AIAA J, Vol. 34, pp. 1348-55,1996.

[21] 陳智皇，“變形翼機構之拓撲構造與運動特性之研究”，崑山大學機械工程研究所，碩士論文，2005年。

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