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Remote Sensing of Lamb Waves Using Optical Fibres—An Investigation of Modal Composition

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TLDR
In this paper, the differences between directly and remotely-bonded optical fiber Bragg grating (FBG) sensors when measuring Lamb waves in an aluminum plate were investigated.
Abstract
This paper reports on an experimental investigation into the differences between directly and remotely bonded optical fiber Bragg grating (FBG) sensors when measuring Lamb waves in an aluminum plate. A sensor array, comprising 16 individual short gauge-length FBG sensing elements, is used to decompose the wave into its constituent modes for the directly bonded case, where the array is attached directly to the plate and for the remotely bonded case where the same array is located in a suspended fiber 250 mm downstream from the fiber/plate contact region. The experimental results were consistent with model predictions and show that while the directly bonded fiber array can resolve the full multimodal Lamb wave spectrum in the plate, the remotely bonded sensor measures only a single nondispersive longitudinal acoustic mode predicted by the analytical solution for a cylindrical waveguide. The inability of remote sensing to distinguish between different modes of Lamb wave propagation represents a significant limitation with respect to the diagnostic utility of this sensing approach.

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Citations
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High-Strain Fiber Bragg Gratings for Structural Fatigue Testing of Military Aircraft

TL;DR: In this paper, the authors discuss FBG and FBG's role in the development of FBG, and propose FBG as a FBG-based FBG platform, which is used to train FBG workers.
Journal ArticleDOI

An ultrasonic visualization system using a fiber-optic Bragg grating sensor and its application to damage detection at a temperature of 1000 °C

TL;DR: In this article, the authors developed a laser ultrasonic visualization system with a heat-resistant fiber-optic Bragg grating (FBG) sensing configuration, which enabled clear damage identification at temperatures as high as 1000°C.
Journal ArticleDOI

A Theoretical/Numerical Study on Ultrasound Wave Coupling From Structure to Remotely Bonded Fiber Bragg Grating Ultrasound Sensor

TL;DR: In this paper, the analytical model of the structure-adhesive-optical fiber section, treated as an ultrasound coupler, is derived and analyzed to explain the observed experimental phenomena.
Journal ArticleDOI

Laser Doppler Vibrometry Measurements of Conversion of Surface Guided Waves to Optical Fiber Modes

TL;DR: In this article, a 3D laser Doppler vibrometer was used to measure the mode conversion of ultrasonic waves through an adhesive bond, implementing a high-resolution 3-dimensional laser doppler simulator.
Journal ArticleDOI

Guided waves based damage localization using acoustically coupled optical fibers and a single fiber Bragg grating sensor

TL;DR: In this article , the authors presented a proof-of-concept of the use of the acoustically coupled optical fibers and single fiber bragg grating (FBG) sensors for damage localization.
References
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Journal ArticleDOI

The interaction of Lamb waves with defects

TL;DR: The results indicate that Lamb waves may be used to find notches when the wavelength to notch depth ratio is on the order of 40, and the 2-D Fourier transform method is used to quantify Lamb wave interactions with defects.
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A two-dimensional Fourier transform method for the measurement of propagating multimode signals

TL;DR: In this article, a two-dimensional Fourier transform (2D FFT) was used to measure the amplitudes and velocities of the Lamb waves propagating in a plate, the output of the transform being presented using an isometric projection which gives a three-dimensional view of the wave-number dispersion curves.
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Active health monitoring of an aircraft wing with embedded piezoelectric sensor/actuator network: I. Defect detection, localization and growth monitoring

TL;DR: In this article, an ultrasonic guided wave structural health monitoring (SHM) system was developed for aircraft wing inspection, where small, low-cost and light-weight piezoelectric (PZT) discs were bonded to various parts of the aircraft wing, in a form of relatively sparse arrays, for simulated cracks and corrosion monitoring.
Journal ArticleDOI

Piezoelectric Wafer Embedded Active Sensors for Aging Aircraft Structural Health Monitoring

TL;DR: In this paper, the state-of-the-art in piezoelectric-wafer active sensors structural health monitoring and damage detection is reviewed, and two main detection strategies are considered: the E/M impedance method for near field damage detection, and wave propagation methods for far-field damage detection.
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Acousto-ultrasonic sensing using fiber Bragg gratings

TL;DR: In this paper, a fiber-optic system based on fiber Bragg grating sensors is proposed to detect ultrasonic Lamb waves in aircraft structures, in particular aircraft structural structures.
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