항공기의 구조물과 시스템에 대한 낙뢰직접영향에 관한 연구 = A study on the direct effect of lightning on structures and systems of aircraft

다국어 초록 (Multilingual 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.

참고문헌 (Reference)

1 이해선, "항공기 집접낙뢰에 대한 동체 구조손상 인증" 항공우주시스템공학회 6 (6): 13-18, 2012

2 정덕영, "낙뢰 간접영향에 대한 항공전자장비의 환경시험" 항공우주시스템공학회 7 (7): 55-59, 2013

3 National Aeronautics and Space Administration, "Lightning Protection of Aircraft"

4 Franklin A. Fisher, "Lightning Protection of Aircraft" Lightning Technology Inc 87-101, 2004

5 Federal Aviation Administration, "DOT/FAA/CT-89/22, Aircraft Lightning Protection Handbook"

6 B. J. Lim, "Certification Report for KC-100 Lightning Direct Effect Protection" KAI 58-, 2012

7 Society of Automotive Engineers, "ARP5414A, Aircraft Lightning Zoning"

8 Society of Automotive Engineers, "ARP5412A, Aircraft Lightning Environment and Related Test Waveforms"

9 Federal Aviation Administration, "AC 20-37E, Aircraft Propeller Maintenance"