Simultaneous Measurement of Strain and Temperature During and After Cure of Unsymmetric Composite Laminate Using Fiber Optic Sensors

비대칭 복합적층판의 성형시 및 성형후 광섬유 센서를 이용한 변형률 및 온도의 동시 측정

  • 강동훈 (한국과학기술원 항공우주공학과) ;
  • 강현규 (한국과학기술원 항공우주공학) ;
  • 김대현 (한국과학기술원 항공우주공학) ;
  • 방형준 (한국과학기술원 항공우주공학) ;
  • 홍창선 (한국과학기술원 항공우주공학) ;
  • 김천곤 (한국과학기술원 항공우주공학과)
  • Published : 2001.05.01

Abstract

In this paper, we present the simultaneous measurement of the fabricaition strain and temperature during and after cure of unsymmetric composite laminate uising fiber optic sensors. Fiber Bragg grating/extrinsic Fabry-Perot interferometric (FBG/EFPl) hybrid sensors are used to measure those measurands. The characteristic matrix of sensor is analytically derived and measurements can be done without sensor calibration. A wavelength-swept fiber laser is utilized as a light source. FBG/EFPI sensors are embedded in a graphite/epoxy unsymmetric cross-ply composite laminate at different direction and different location. We perform the real time measurement of fabrication strains and temperatures at two points of the composite laminate during cure process in an autoclave. Also, the thermal strains and temperatures of the fabricated laminate are measured in thermal chamber. Through these experiments, we can provide a basis for the efficient smart processing of composite and know the thermal behavior of unsymmetric cross-ply composite laminate.

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