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系統識別號 U0002-3007201414480600
中文論文名稱 仿生微型蜂鳥機構之靜態平衡
英文論文名稱 Static Balancing of a Hummingbird-like Micro-aviation-vehicle
校院名稱 淡江大學
系所名稱(中) 機械與機電工程學系碩士班
系所名稱(英) Department of Mechanical and Electro-Mechanical Engineering
學年度 102
學期 2
出版年 103
研究生中文姓名 張育晨
研究生英文姓名 Yu-Chen Jhang
學號 601370298
學位類別 碩士
語文別 中文
口試日期 2014-07-09
論文頁數 79頁
口試委員 指導教授-劉昭華
委員-劉昭華
委員-陳正光
委員-王銀添
中文關鍵字 微型飛行器  靜態平衡  史蒂芬森三型六連桿機構 
英文關鍵字 Micro-aviation-vehicle  static balance  Stephenson III six-bar Mechanism 
學科別分類 學科別應用科學機械工程
中文摘要 本論文針對特定的微型飛行器機構做靜態平衡分析。由於此機構主要部分包含史蒂芬森三型六連桿機構,本論文首先針對此機構,利用總質心位置不變的特性,推導出此機構靜態平衡之條件,亦即機構桿長、桿件質量、及質心位置的關係式,並比較靜態平衡前後之差距。接著,根據相同原理,本文亦推導出整個微型飛行器機構所適用之靜態平衡條件,並且比較靜態平衡前後差距。另外,由於此微型飛行器可簡化為由三個滑件曲柄機構所組成之機構,本文也針對單一滑件曲柄機構做靜態平衡分析,求出滑件曲柄機構之靜態平衡條件。最後,本文針對整個微型飛行器之簡化機構做靜態平衡分析,求出其靜態平衡之條件,並分析靜態平衡後的差距。
英文摘要 Static balancing of a specific MAV is performed in this thesis. A Stephenson III six-bar mechanism is first dealt with, since it is the main part of the MAV. Conditions for static balancing of this mechanism are derived by keeping the total mass center stays at the same position. Balancing conditions for the whole MAV is derived using the same method. These conditions are checked by numerical examples. A simplified version of the MAV consists of three slider-crank mechanisms, hence static balancing of a single slider crank mechanism is also performed. Finally, conditions for static balancing of the whole simplified MAV are derived and verified numerically in an example.
論文目次 目錄

中文摘要 I
英文摘要 II
目錄 III
圖目錄 V
第1章 緒論 1
1-1 研究背景及動機 1
1-2 仿生蜂鳥微型飛行器結構 1
1-3 文獻回顧 2
第2章 史蒂芬生三型六連桿之靜態平衡 4
2-1 史蒂芬生三型六連桿之平衡條件 4
2-2 六連桿之接頭反作用力分析 8
2-3 例題 10
2-4 平衡結果 12
第3章 仿生蜂鳥機構之靜態平衡 13
3-1 仿生蜂鳥機構之靜態平衡條件 13
3-2 仿生蜂鳥機構之接頭反作用力分析 18
3-3 例題 21
3-4 平衡結果 24
第4章 滑件曲柄機構 25
4-1 滑件曲柄機構之靜態平衡條件 25
第5章 仿生蜂鳥之簡化機構 28
5-1 簡化機構之靜態平衡條件 28
5-2 仿生蜂鳥簡化機構之接頭反作用力分析 32
5-3 例題 34
5-4 平衡結果 37
第6章 結論 38
參考文獻 40
參考文獻 參考文獻
[1] Berkof, R.S., and Lowen, G.G., “a new method for completely force balancing simple linkages ”, Journal of Engineering for Industry, 1969, pp.21-26.
[2] Bagci, C., “Complete shaking force and shaking moment balancing of link mechanisms using balancing idler loops”, ASME (Paper), n80-DET-100, 1980.
[3] Walker, M.J., and Haines, R.S., “Experimental study of the effects of counterweights on a six-bar chain”, Mechanism & Machine Theory, v 17, n 6, 1982, pp.335-360.
[4] Huang, Z., and Liu, D.Y., “Shaking moment balancing of force-balanced six-bar linkages”, ASME (Paper), Design engineering Technical Conference , 1986.
[5] Bagci, C., “Complete balancing of linkages using complete dynamical equivalents of floating links. CDEL method”, American Society of Mechanical Engineers, 22nd Biennial Mechanisms Conference, September 13,1992- September 16, 1992, v 47, 1992, pp.477-488.
[6] Li, C-H., and Tso, P-L., “The study of dynamic balancing for high-speed presses”, JSME International Journal, Series C: Mechanical Systems, Machine Elements and Manufacturing, v 49, n 3, 2007, pp.657-662.
[7] Lin, P-Y., Shieh, W-B., and Chen,D-Z., “Design of perfectly statically balanced one-dof planar linkages with revolute joints only”, Journal of Mechanical Design, v 131, n 5, 2009, pp. 0510041-0510049.
[8] Zhu, X-R., Shen, H-P., Zhang, H-F., Li, J., Tao, S-B., and Yang, T-L., “Finite position method for complete balancing of shaking forces of mechanisms”, Proceeding 2009 IEEE 10th International Conference on Computer-Aided Industrial Design and Conceptual Design: E-Business, Creative Design, Manufacturing, 2009, pp 2333-2338.
[9] Sun, J-W., and Chiou, S-T., “Global optimum balancing design of Stephenson-III six-bar linkages with installing disk counterweights”, Journal of the Chinese Society of Mechanical Engineers, v 32, n 1, 2011, pp.25-34.
[10] Wilson, C.E., and Sadler, J.P., Kinematic and Dynamics of Machinery, Third Edition in SI Units, Prentice-Hall, 2006, pp.741-743
[11] Norton, R.L., Kinematics and Dynamics of Machinery, 2nd ed. in SI units, McGraw-Hill, 2013, pp. 639-640.
[12] 陳建凱,仿生蜂鳥飛行機構運動及誤差分析,淡江大學,機械與機電工程學系碩士論文,2014。
[13] 王勝弘,仿生蜂鳥微型飛行器機構運動分析,淡江大學,機械與機電工程學系碩士論文,2013。
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