A fiber optic doppler sensor and its application in debonding detection for composite structures

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Abstract

Debonding is one of the most important damage forms in fiber-reinforced composite structures. This work was devoted to the debonding damage detection of lap splice joints in carbon fiber reinforced plastic (CFRP) structures, which is based on guided ultrasonic wave signals captured by using fiber optic Doppler (FOD) sensor with spiral shape. Interferometers based on two types of laser sources, namely the He-Ne laser and the infrared semiconductor laser, are proposed and compared in this study for the purpose of measuring Doppler frequency shift of the FOD sensor. Locations of the FOD sensors are optimized based on mechanical characteristics of lap splice joint. The FOD sensors are subsequently used to detect the guided ultrasonic waves propagating in the CFRP structures. By taking advantage of signal processing approaches, features of the guided wave signals can be revealed. The results demonstrate that debonding in the lap splice joint results in arrival time delay of the first package in the guided wave signals, which can be the characteristic for debonding damage inspection and damage extent estimation. © 2010 by the authors.

Figures

  • Figure 1. (a) The circular loop FOD sensor. (b) Sketch of the spiral FOD sensor. (c) Picture of a surface-bonded spiral FOD sensor.
  • Table 1. Properties of the optical fiber used to fabricate the FOD sensor.
  • Figure 2. Principles of interferometers using (a) the He-Ne laser and (b) infrared semiconductor laser.
  • Figure 3. Original guided ultrasonic wave signals acquired using (a) the He-Ne-laser-based interferometer and (b) the infrared-semiconductor-laser-based interferometer.
  • Figure 4. (a) SNR of guided wave signal changes with the optical fiber length of reference light of semiconductor interferometer. (b) SNR of guided wave signal changes with the absolute difference between optical fiber lengths of reference light and signal light.
  • Table 2. Properties of the CFRP laminate and epoxy.
  • Figure 5. (a) Sketch of the specimen and zoom-in view of the lap splice joint. (b) Sketch of the specimen with tablets at the two ends in the simulation. (c) Zoom-in view of the lap splice joint with debonding.
  • Figure 5. Cont.

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CITATION STYLE

APA

Li, F., Murayama, H., Kageyama, K., Meng, G., Ohsawa, I., & Shirai, T. (2010). A fiber optic doppler sensor and its application in debonding detection for composite structures. Sensors, 10(6), 5975–5993. https://doi.org/10.3390/s100605975

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