小型長滯空連翼型無人飛行載具研製

Developments of Long-Endurance Small Joined-Wing UAV

賈澤民(Jir-Min Char) ； 江志煌(Chih-Hunag Chiang) ； 陳唐徵(Tang-Cheng Chen) ； 徐子圭(Zue-Kue Hsu) ； 黃俊榮(Chun-Jung Huang) ； 林啟裕(Chi-Yu Lin)

《航空太空及民航學刊.系列B》 42卷1期 (2010/04) Pp. 11-17

https://doi.org/10.6124/JAAA.201004_42(1).02

摘要

無人飛行載具之應用已是廣?認知之事實，其應用範疇當然受限於載具航行能力，本研究重點在於自行研製連翼構型且可長滯空（8小時）之無人飛行載具。已開發完成之縮小比例原型機，可攜帶酬載30Kg，最大航速約130Km/hr，巡航速度約?50 Km/hr，研製過程包括初步設計、細部設計、風洞實驗、CFD氣動力模擬及結構應力分析，最後製造完成原型機，並已執行各項試飛驗測工作。預期未來將開發應用在各項酬載匹配任務，以落實連翼型UAV多功能特色。

關鍵字

連翼型 ； 無人飛行載具 ； 飛機設計

並列摘要

This study was devoted to investigating the flight characteristics of joined-wing aircrafts by means of design, manufacture, and flight test of actual vehicles, in order to evaluate the feasibility for application to unmanned aerial vehicles. There were two developing stages. The design of joined-wing UAV of the first stage was based on the results and suggestions of literatures. Manual and automatic flight tests of this UAV were both successful. The stability and controllability were suitable except when the Reynolds number was less than 1.8×105. The design of the second stage was improved according to the test results of stage one. The stability and control quality were proved to be better. The joined-wing configuration is adequate for autonomous unmanned aerial vehicles.

並列關鍵字

Joined wing ； Unmanned aerial vehicle ； Aircraft design