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Composites Science and Technology
Volume 65, Issues 11-12, September 2005, Pages 1800-1807
 
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doi:10.1016/j.compscitech.2005.03.009    How to Cite or Link Using DOI (Opens New Window)
Copyright © 2005 Elsevier Ltd All rights reserved.

Damage monitoring in aluminum-foam sandwich structures based on thermoplastic fibre-metal laminates using fibre Bragg gratings

K.S.C. Kuanga, Corresponding Author Contact Information, E-mail The Corresponding Author, W.J. Cantwellb, L. Zhangc, I. Bennionc, M. Maaleja and S.T. Queka

aDepartment of Civil Engineering, National University of Singapore, 1 Engineering Drive 2, E1A 07-03, Singapore 117576, Singapore bMaterials Science and Engineering, Department of Engineering, University of Liverpool, Brownlow Hill, L69 3GH Liverpool, United Kingdom cPhotonics Research Group, Electronic Engineering, Aston University, Aston Triangle, B4 7ET Birmingham, United Kingdom

Received 8 July 2004; 
revised 2 March 2005; 
accepted 14 March 2005. 
Available online 29 April 2005.

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Abstract

This paper reports the use of fibre Bragg gratings (FBGs) as sensors for structural integrity assessment by monitoring the reduction in the flexural stiffness of a novel sandwich structure based on thermoplastic fibre-metal laminate (FML) skins and an aluminum-foam core. By monitoring the reduction in the structural flexural stiffness, the technique demonstrated its potential for detecting damage initiation in these hybrid systems. In addition, the method allows the estimation of the initial failure strain and the rate of subsequent damage development within the host material.

Cyclic three-point bend tests were conducted to characterise the degree of damage in this material in which the maximum load in each cycle was increased progressively until failure occurred. The FBG sensors, which were initially used to monitor the fabrication process, were subsequently employed as damage sensors to monitor the development of damage in the host structure. The FBG sensors were either embedded between two plies of glass fibre reinforced polypropylene within the FML or bonded to its lower surface. The shift in the Bragg wavelength was recorded during the test cycle to monitor the strain response of the sandwich beam.

Keywords: A. Layered structures; Fibre Bragg gratings

Article Outline

1. Introduction
2. Theoretical background
2.1. Fibre Bragg gratings
2.2. Elastic bending of sandwich beams
3. Experimental procedure
4. Results and discussions
5. Conclusions
Acknowledgements
References











 
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