운항 중 실구조물(항공기 축소모델)에서의 탄소섬유강화플라스틱(CFRP)의 음향방출신호 특성에 관한 연구

A Study on Acoustic Emission Characteristics of CFRP in aircraft operations

  • 이경원 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 안주선 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 황웅기 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 이종오 (한국기계연구원 부설 재료연구소) ;
  • 이상율 (한국항공대학교 항공재료공학과) ;
  • 이보영 (한국항공대학교 항공우주 및 기계공학부)
  • 투고 : 2010.11.20
  • 심사 : 2010.12.26
  • 발행 : 2010.12.31

초록

Aerospace structures need high stability and long life because many personal injuries can result from an accident and securing structural integrity for various external environments is more important than any other thing. So first of all we must prove the destruction properties for operating environment, have prediction technology about damage evolution and life, and develop an economical non-destructive technology capable of detecting structure damage. Acoustic emission (AE) have no need of artificial environment like ultrasonic inspection or radio fluoroscopy to emit a certain energy, is a testing technique using seismic signal resulting from interior changes of solids, and enables to observe if any fault is appeared and it grows seriously or not while running. In this study we suggest the method of structural integrity evaluation for aerospace structures through the acoustic emission technique, for which a model plane was manufactured and an actual operation test was conducted.

키워드

참고문헌

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