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Structural Development for Human Powered Aircraft

인간동력항공기 구조 개발

  • 신정우 (한국항공우주연구원 항공혁신기술연구소) ;
  • 우대현 (한국항공우주연구원 항공혁신기술연구소) ;
  • 박일경 (한국항공우주연구원 항공혁신기술연구소) ;
  • 이무형 (한국항공우주연구원 항공혁신기술연구소) ;
  • 임주섭 (한국항공우주연구원 항공혁신기술연구소) ;
  • 박상욱 (한국항공우주연구원 항공혁신기술연구소) ;
  • 김성준 (한국항공우주연구원 항공혁신기술연구소) ;
  • 안석민 (한국항공우주연구원 항공혁신기술연구소)
  • Received : 2012.12.21
  • Accepted : 2013.03.15
  • Published : 2013.03.31

Abstract

Human Powered Aircraft (HPA) should be light in weight and have high efficiency because power source of propulsion is human muscles. Airframe structure takes up most of empty weight of aircraft, so weight reduction of structure is very important issue for HPA. In this paper, design/analysis/test procedures for ultra light weight structure of the HPA developed by Korea Aerospace Research Institute (KARI) are explained briefly. Structural design is conducted through case studies on HPA in the USA and Japan. Loads analysis is performed to calculate design loads which is needed for structural design and analysis. Structural analysis is conducted for structure sizing. Static strength test of main wing spar which is primary structure of wing is performed to verify structural integrity.

Keywords

References

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