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http://dx.doi.org/10.12985/ksaa.2017.25.4.044

Design Modification of Airframe Shape for Ultra Light Quad-Rotor Development  

Park, Dae-Jin (한국항공대학교 대학원 항공우주 및 기계공학과)
Lee, Sangchul (한국항공대학교 항공우주 및 기계공학부)
Park, Saeng-Jin (인터켐)
Song, Tae-Hun ((주) 휴인스)
Publication Information
Journal of the Korean Society for Aviation and Aeronautics / v.25, no.4, 2017 , pp. 44-51 More about this Journal
Abstract
An ultra light quad-rotor is utilized in various areas for military and commercial purpose. Especially, the airframe shape is designed with various airframe size, weight and purpose. In this paper, the initial airframe shape of the quad-rotor was designed and manufactured. Flight test was conducted for the quad-rotor. The design modification of airframe shape was conducted to meet design requirement. By changing design, weight of airframe structure was reduced and payloads were placed to the best position. By reinforcing ribs and reducing vehicle's legs, the durability of airframe structure was enhanced.
Keywords
Ultra Light Quad-Rotor; Airframe Structure; Design Modification; Weight Reduction;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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