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Use of FBG Sensors for SHM in Aerospace Structures

Use of FBG Sensors for SHM in Aerospace Structures

作     者:Gayan C. KAHANDAWA Jayantha EPAARACHCHI Hao WANG K. T. LAU 

作者机构:Centre of Excellence in Engineered Fibre Composites University of Southern Queensland Toowoomba 4350Queensland Australia 

出 版 物:《Photonic Sensors》 (光子传感器(英文版))

年 卷 期:2012年第2卷第3期

页      面:203-214页

核心收录:

学科分类:070207[理学-光学] 07[理学] 08[工学] 0803[工学-光学工程] 0702[理学-物理学] 

基  金:Interdisciplinary Photonics Laboratory (iPL) University of Sydney 

主  题:Structural health monitoring aerospace structures fiber Bragg grating sensors 

摘      要:This paper details some significant findings on the use of the fiber Bragg grating (FBG) sensors for structural health monitoring (SHM) in aerospace fiber reinforced polymer (FRP) structures. A diminutive sensor provides a capability of imbedding inside FRP structures to monitor vital locations of damage. Some practical problems associated with the implementation of FBG based SHM systems in the aerospace FRP structures such as the difficulty of embedding FBG sensors during the manufacturing process and interrelation of distortion to FBG spectra due to internal damage, and other independent effects will be thoroughly studied. An innovative method to interpret FBG signals for identifying damage inside the structures will also be discussed.

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