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A study on the direct effect of lightning on structures and systems of aircraft

항공기의 구조물과 시스템에 대한 낙뢰직접영향에 관한 연구

  • Jeong, Duckyoung (Aerospace Product Assurance Center, Korea Aerospace Research Institute) ;
  • Yang, Hyundeok (Aerospace Product Assurance Center, Korea Aerospace Research Institute)
  • 정덕영 (한국항공우주연구원 항공우주제품보증센터) ;
  • 양현덕 (한국항공우주연구원 항공우주제품보증센터)
  • Received : 2016.04.12
  • Accepted : 2016.06.21
  • Published : 2016.06.30

Abstract

Statistical data show that a large aircraft(transport category) is struck by lightning once a year or once per 1,000 ~ 20,000 flight time. The protection design for lightning must be applied to the aircraft because an aircraft is developed on condition that it is absolutely struck by lightning. For the proper protection design, we need to understand direct effect and indirect effect of lightning. This paper described the direct effect of lightning on aircraft's structures and systems.

Keywords

References

  1. National Aeronautics and Space Administration, "Lightning Protection of Aircraft" pp. 75-76, 1977.
  2. Society of Automotive Engineers, "ARP5412A, Aircraft Lightning Environment and Related Test Waveforms", pp. 20, 2005.
  3. 정덕영, 양현덕, "낙뢰간접영향에 대한 항공전자장비의 환경시험", 항공우주시스템공학회지, 제7권 제2호, pp. 55-59, 2013.
  4. Federal Aviation Administration, "DOT/FAA/CT-89/22, Aircraft Lightning Protection Handbook", pp. 73-192, 1989.
  5. Franklin A. Fisher, J. Anderson Plumer, and Rodney A. Perala, "Lightning Protection of Aircraft", 2nd Ed., Lightning Technology Inc., USA, 2004. pp. 87-101.
  6. B. J. Lim, "Certification Report for KC-100 Lightning Direct Effect Protection", KAI, Sacheon, 2012, pp. 58.
  7. Society of Automotive Engineers, "ARP5414A, Aircraft Lightning Zoning", pp. 27, 2005.
  8. Federal Aviation Administration, "AC 20-37E, Aircraft Propeller Maintenance", pp. 4-5, 2005.
  9. 이해선, "항공기 직접낙뢰에 대한 동체 구조손상 인증", 항공우주시스템공학회지, 제6권 제3호, pp. 13-18, 2012.