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A Study on Manufacturing Methods of Cocuring Composite Wings of Solar-Powered UAV

복합재 태양광 무인기 날개 일체성형 제작기법 연구

  • Yang, Yongman (Korea Aerospace Research Institute) ;
  • Kwon, Jeongsik (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Kim, Jinsung (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Lee, Sooyong (School of Aerospace and Mechanical Engineering, Korea Aerospace University)
  • 양용만 (한국항공우주연구원) ;
  • 권정식 (한국항공대학교 항공우주 및 기계공학부) ;
  • 김진성 (한국항공대학교 항공우주 및 기계공학부) ;
  • 이수용 (한국항공대학교 항공우주 및 기계공학부)
  • Received : 2016.01.09
  • Accepted : 2016.02.26
  • Published : 2016.03.31

Abstract

In order to suggest the optimal manufacturing technology of composite wings of solar-powered unmanned aerial vehicles, this study compared forming technologies to reduce wing weight for long-endurance flight and to improve the manufacturing process for cost-saving and mass production. It compared the manufacturing time and weight of various composite wing molding technologies, including cocuring, secondary bonding, and manufacturing by balsa. As a result, wing weight was reduced through cocuring methods such as band type composite fiber/tape lamination technology, which enabled prolonged flight duration. In addition, the reduced manufacturing time led to a lower cost, which is a good example of weight lightening for not only small solar-powered UAVs, but also composite aircraft.

Keywords

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