| 研究生: |
蘇威仲 Su, Wei-Zhong |
|---|---|
| 論文名稱: |
以仿生拍撲機構探討雀類前飛運動中肩-腕關節距離之氣動力效應 Aerodynamic effects of distance change between shoulder and wrist joints of passerines in forward flight using flapping wing robot |
| 指導教授: |
葉思沂
Yeh, Szu-I |
| 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: | 2020 |
| 畢業學年度: | 109 |
| 語文別: | 中文 |
| 論文頁數: | 71 |
| 中文關鍵詞: | 拍撲翼 、內翼收縮 、等速前飛 、垂直力表現 、翼面積變化 |
| 外文關鍵詞: | flapping wing, forward flight, wing area variation in inner wing, force measurement |
| 相關次數: | 點閱:89 下載:2 |
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本研究以綠繡眼為研究對象,參考其等速前飛之動作,並製作四自由度仿生拍撲機構,於風洞及真空艙中模擬其飛行動作,並量測垂直力變化,探討內翼的動作變化對於垂直力的影響,期望可做為微型拍撲飛行器的翼型設計參考。本實驗參考前人生物觀察之結果,以具有四個自由度的仿生拍撲機構模擬綠繡眼等速前飛運動過程中的動作變化,以拍撲動作所產生的垂直力變化來探討肩-腕關節距離在不同風速下之氣動力效應。實驗分為兩組,分別為動作模式一為具有肩-腕關節距離變化的綠繡眼前飛運動,以及模式二的固定內翼且其他拍撲角度仍模擬綠繡眼之動作。實驗結果在來流速度較低時,動作模式二有較佳的垂直力表現,但動作模式一卻有較好的飛行穩定性;而在較高的來流速度時,動作模式一則為最佳的選擇,因此,在微型拍撲飛行器的設計上,可根據飛行條件以及策略作翼型設計;在較低的飛行速度且需要較佳的垂直力表現,則可以選擇動作模式二,不需設計可調式內翼,但如果需要較佳的飛行穩定性,則可以將內翼變化納入考量;在較高的飛行速度下,動作模式一為最佳的拍撲動作,可提供較好的垂直力表現,同時有不錯的飛行穩定性。在未來拍撲微飛行器的設計上,可參考本論文可調節式內翼的兩段式飛翼設計,並針對不同飛行任務之飛行條件選擇飛行模式,增進拍撲微飛行器之飛行表現。
The aim of this study is to design and fabricate a multiarticulate flapping-wing robot with four degrees of freedom in order to imitate forward flying motion of passerines for force measurement in low-speed wind tunnel. To investigate the aerodynamic effects of inner wing change of passerines in forward flight, the previous work which observed the wing kinematics of passerines was utilized to obtain wing trajectories. Tow modified motion cases were experimented in this study, one with the cyclic change in inner wing area, resemble the real passerines, and one with the fixed inner wing area. Two cameras were utilized to completely record kinematic of robot and verify the wing trajectories by direct linear transformation (DLT), which is sure that the motion of the robot has high correlation with the desired trajectories. The experiments were executed not only in wind tunnel with wind velocity at 3 m/s and 5 m/s but also in vacuum chamber to subtract inertial part from wind tunnel results so as to observe the aerodynamic difference between two cases. The force measurement results can be split into three phases in a wingbeat cycle and show that changing the inner wing area truly has certain degree of impact on three-dimension flow field structure especially in upstroke period. In phase two, lateral motion to decrease the wing area do inhibit the negative perpendicular force. However, this lateral motion has an impact on leading edge vortex (LEV) and some complicate wing-wake interaction. With the wind speed increase, aerodynamic effect of lateral motion has less impact on phase tow so that decreasing the wing area can better reduce the negative perpendicular force. On this basis, we can provide a wing design and fly motion idea to MAV design and PIV experiment should be done in the future to get thoroughly understand on aerodynamic mechanism during forward flight of passerines.
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