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研究生:呂崇境
研究生(外文):Lu, Chung-ching
論文名稱:旋翼/固定翼兩用型飛行器之概念設計與製作
論文名稱(外文):Conceptual Design and Manufacture of Hybrid Fixed / Rotary Wing Flight Vehicle
指導教授:楊憲東楊憲東引用關係
指導教授(外文):C.D.Yang
學位類別:碩士
校院名稱:國立成功大學
系所名稱:航空太空工程學系
學門:工程學門
學類:機械工程學類
論文種類:學術論文
論文出版年:1998
畢業學年度:86
語文別:中文
論文頁數:116
中文關鍵詞:兩用型飛行器同軸雙層圓盤加旋翼概念性設計可行性評估飛行性能分析遙控模型機
外文關鍵詞:hybrid aircraftcoaxial double-layer counter-rotating disk wingconceptual designfeasibility studyanalysis of flight performanceremote-control model
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在本論文中,吾人針對台灣多離島、多山岳的特有飛航環境與運輸需
求,提出一套新概念飛行器的設計構想與研發計劃,此一新概念飛行器的
最大特色,是其兼具有旋翼機垂直起降與固定翼飛機高速巡航的能力,利
用旋翼機模式,不需跑道,既可在一般空地垂直起降,免除台灣地狹人稠
,機場數量有限的限制,當達到巡航高度與速度後,轉換成固定翼的模式
飛行,即與一般的民航機一樣,具有速度快、運量高的優越性,可說是集
旋翼機與固定翼機的優點於一身, 完全符合台灣民航市場未來發展的需求
。此兩用型飛行器之所以能具備旋翼∕固定翼兩種飛行模式,關鍵在於其
「同軸雙層圓盤加旋翼」的機構設計。本論文分兩部份,第一部分,首先
對兩用型飛行器進行概念性設計(Conceptual Design),包括(1)外型尺
寸之估算與設計(2)飛行功能配置(3)可行性評估(4)飛行性能分析(5)控制
機構設計以及(6)「同軸雙層圓盤加旋翼」創意設計說明。 在第二部
份中,吾人根據第一部分的設計理念,實際製作一架兩用型飛行器的實體
遙控模型機並進行試飛,以驗證此設計構想的可行性。 最後,根據分
析的結果,提出兩用型飛行器研發過程中需要克服的關鍵技術以及預期的
貢獻。

To accommodate air traffic to Taiwan's special geographic
environment with numerous islands and mountains, in this thesis
we propose the design concept and development plan for a novel
flight vehicle. The main characteristic of the proposed flight
vehicle is to combine the advantages of rotary wing and fixed
wing. A flight vehicle with rotary wing is able to take off
vertically, while a flight vehicle with fixed wing has high
cruising speed. The vehicle designed in this thesis can take off
vertically as a helicopter and can cruise with a high speed as a
civil aircraft. Because of its vertical take-off and landing
ability,airport's runway becomes unnecessary, and because of its
high cruising speed, traveling time can be greatly reduced. This
kind of hybrid aircraft is undoubtedly the most suitable flight
vehicle for future air traffic in Taiwan. The key technique of
this hybrid aircraft is the mechanic design of the coaxial
double-layer disk wing with extending blades. This thesis
comprises two parts. Part I considers the conceptual design of
the hybrid aircraft, including (a) estimate of external sizing
(b) hybrid flight function design (c) feasibility study (d)
analysis of flight performance (e) design of control mechanism
(f) creative design of coaxial double-layer counter-rotating
disk wing with extending blades . According to the conceptual
design in Part I, we actually manufacture a remote-control model
in Part II, and a series of flight testing is conducted to
verify the feasibility of the proposed hybrid aircraft.
Finally, based on the experience from the manufacturing process
of remote-control model,we propose the possible difficulties to
be conquered in the manufacture of full-scale vehicle. The
prospective advantages of this new design are stressed in the
end.

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