항공우주시스템공학회지 (Journal of Aerospace System Engineering)
- 제6권3호
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- Pages.13-18
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- 2012
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- 1976-6300(pISSN)
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- 2508-7150(eISSN)
DOI QR Code
항공기 집접낙뢰에 대한 동체 구조손상 인증
Certification of Structure Damage from Direct Lightning
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이해선
(한국항공우주연구원)
- 투고 : 2012.07.11
- 심사 : 2012.08.31
- 발행 : 2012.09.30
초록
Every 3000 hour an aircraft is stricken by a lightning. Also the lightning damage to the aircraft during flight are continually occurred due to extreme weather phenomena such as global warming. Under the airworthiness standards, the aircraft must be designed to protect lightning. To show compliance for lightning, the test should be conducted by the actual lightning current and voltage waveform for the actual aircraft or parts. After test, structure damage is detected via visual inspection or NDI. Structure substantiation for damage is to show retaining limit or near limit load capability. This is conducted by test or analysis based on test. Thus, the aircraft should retain structural strength to land safely, even though the damage of aircraft fuselage from Lightning strike are occurred.