2015
DOI: 10.1016/j.compstruct.2015.02.038
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Damage identification system of CFRP using fiber Bragg grating sensors

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Cited by 39 publications
(14 citation statements)
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“…Conventional reflection spectrum demodulation, signal acquisition and characteristic central wavelength are provided by the FBG measurement systems, such as si255 (Lu et al, 2015). However, for crack detection, the FBG measurement system displays several limitations; for instance, it distinguishes a signal peak range from the multi-peak FBGs and evaluates the shape of distorted reflection spectrum.…”
Section: The Full Width At Half Maximum Extraction Algorithmmentioning
confidence: 99%
“…Conventional reflection spectrum demodulation, signal acquisition and characteristic central wavelength are provided by the FBG measurement systems, such as si255 (Lu et al, 2015). However, for crack detection, the FBG measurement system displays several limitations; for instance, it distinguishes a signal peak range from the multi-peak FBGs and evaluates the shape of distorted reflection spectrum.…”
Section: The Full Width At Half Maximum Extraction Algorithmmentioning
confidence: 99%
“…where y n is the thickness of the CFRP laminates. By substituting (12) and (14) into (13), an equation can be derived as follows:…”
Section: Of 19mentioning
confidence: 99%
“…Fiber Bragg grating (FBG) sensors, a type of optical fiber sensor, have been recognized as ideal choices for aviation structure strain measurement [11]. FBG sensors have many advantages such as their small size, high sensitivity, multiplexing capability and immunity to electromagnetic interference [12][13][14]. FBG is made by inscribing grating in an optical fiber core.…”
Section: Introductionmentioning
confidence: 99%
“…In recent years, FBG sensors have been investigated and applied for dynamic strain measurement and modal analysis [10,11,12,13]. For example, distributed FBG sensors were used for strain modal analysis and damage identification of a plate structure [14], and embedded fibre grating sensors were utilised in experimental modal analysis on an aircraft wing model [15].…”
Section: Introductionmentioning
confidence: 99%