| 研究生: |
江柏逸 Chiang, Po-Yi |
|---|---|
| 論文名稱: |
飛天車飛行性能的初步設計 Aero Runner Preliminary Design on Aero Performance |
| 指導教授: |
林清一
Lin, C. E. |
| 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: | 2012 |
| 畢業學年度: | 100 |
| 語文別: | 英文 |
| 論文頁數: | 81 |
| 中文關鍵詞: | 旋翼飛機 、主旋翼回收 、升力分析 、應力分析 |
| 外文關鍵詞: | Gyroplane, Folder system of main rotor, Lift & Stress analysis |
| 相關次數: | 點閱:112 下載:2 |
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本篇論文主要目的為設計以gyroplane為主體的飛天車,同時擁有汽車般的陸地行走能力,重要概念為主旋翼回收應力分析,因此選用結構簡單的gyroplane為出發點,並使用能得到較好氣動特性的外形為飛天車的主要結構,同時執行旋翼升力的Fluent模擬,其最終目的希望能在短距離、不需要特定跑道的情況下直接穩定起飛,並能在空中以gyroplane的普通操作,達到短程或特殊用途的短程飛行,此飛天車應較傳統直升機及飛機更為安全,也是在設計過程中不可或缺的一環,最終則是對車輛的法規及輕航機的法規的探討,增加飛天車在特定用途的應用能力。
The thesis is about how to redesign a gyroplane into a car obtaining car’s maneuverability and fly ability. The main concept includes the stress analysis for folder system of main rotor. For the structure simplicity, gyroplane is our target obtaining a better Aero Runner shape for aerodynamics. The lift simulations are also accomplished in Fluent environment. In the results, the Aero Runner is redesigned from a gyroplane which can take off within a short distance. This will greatly helpful for some particular purposes under regulations. The Aero Runner will accomplish its application capability in special demands.
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校內:2022-12-31公開