Proceedings of the Korean Society For Composite Materials Conference (한국복합재료학회:학술대회논문집)

The Korean Society for Composite Materials (한국복합재료학회)
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Design Scheme of FBG Sensor System for Aircraft Application

항공기 탑재를 위한 FBG 센서 장비의 설계조건 도출

  • 박상욱 (한국과학기술원 기계공학과 항공우주공학) ;
  • 윤혁진 (한국과학기술원 기계공학과 항공우주공학) ;
  • 박상오 (한국과학기술원 기계공학과 항공우주공학) ;
  • 송지용 (한국과학기술원 기계공학과 항공우주공학) ;
  • 김천곤 (한국과학기술원 기계공학과 항공우주공학)
  • Published : 2005.11.18
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Abstract

In this research, design scheme of fiber Bragg grating(FBG) sensor system for aircraft application is suggested from the results and the know-how from the fon11er researches on structural health monitoring techniques using fiber optic sensors. Design factors to be taken into consideration were derived for both sensor parts including connection and system parts. For the stability of FBG sensor system, design requirements of temperature, vibration, humidity, electromagnetic interference were presented from U. S. military standards. The direction of software programming which increases stability and perfon11ance of the aircraft with the FBG sensor system was also examined.

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