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Monitoring of a CFRP-Stiffened Panel Manufactured by VaRTM Using Fiber-Optic Sensors

  • Takeda, Shin-Ichi (Institute of Aerospace Technology, Japan Aerospace Exploration Agency) ;
  • Mizutani, Tadahito (Graduate School of Frontier Sciences, The University of Tokyo) ;
  • Nishi, Takafumi (Graduate School of Frontier Sciences, The University of Tokyo) ;
  • Uota, Naoki (KADO Corporation) ;
  • Hirano, Yoshiyasu (Institute of Aerospace Technology, Japan Aerospace Exploration Agency) ;
  • Iwahori, Yutaka (Institute of Aerospace Technology, Japan Aerospace Exploration Agency) ;
  • Nagao, Yosuke (Institute of Aerospace Technology, Japan Aerospace Exploration Agency) ;
  • Takeda, Nobuo (Graduate School of Frontier Sciences, The University of Tokyo)
  • Published : 2008.06.01

Abstract

FBG (Fiber Bragg Grating) sensors and optical fibers were embedded into CFRP dry preforms before resin impregnation in VaRTM (Vacuum-assisted Resin Transfer Molding). The embedding location was the interface between the skin and the stringer in a CFRP-stiffened panel. The reflection spectra of the FBG sensors monitored the strain and temperature changes during all the molding processes. The internal residual strains of the CFRP panel could be evaluated during both the curing time and the post-curing time. The temperature changes indicated the differences between the dry preform and the outside of the vacuum bagging. After the molding, four-point bending was applied to the panel for the verification of its structural integrity and the sensor capabilities. The optical fibers were then used for the newly-developed PPP-BOTDA (Pulse-PrePump Brillouin Optical Time Domain Analysis) system. The long-range distributed strain and temperature can be measured by this system, whose spatial resolution is 100 mm. The strain changes from the FBGs and the PPP-BOTDA agreed well with those from the conventional strain gages and FE analysis in the CFRP panel. Therefore, the fiber-optic sensors and its system were very effective for the evaluation of the VaRTM composite structures.

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References

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