A global assessment of barely visible impact damage for CFRP sub-components with FBG-based sensors

被引:23
|
作者
Goossens, Sidney [1 ]
Berghmans, Francis [1 ]
Munoz, Kirsa [2 ]
Jimenez, Miguel [2 ]
Karachalios, Evangelos [3 ]
Saenz-Castillo, Diego [4 ]
Geernaert, Thomas [1 ]
机构
[1] Vrije Univ Brussel & Flanders Make, Dept Appl Phys & Photon, Brussels Photon B PHOT, Pl Laan 2, B-1050 Brussels, Belgium
[2] Wilbur & Orville Wright, Element Mat Technol Seville SL, 1 Aeropolis Seville, San Jose De La Rinconada 41300, Spain
[3] Hellenic Aerosp Ind, Engn Res Design & Dev Directorate, Schimatari 32009, Greece
[4] FIDAMC, Fdn Res Dev & Applicat Composite Mat, Avda Rita Levi Montalcini 29, Madrid 28906, Spain
基金
欧盟地平线“2020”;
关键词
Barely visible impact damage; BVID; CFRP; Fibre Bragg gratings; FBG; Aerospace-grade; Sub-components; Stiffened panels; BRAGG GRATING SENSORS; LOW-VELOCITY IMPACT; LOCALIZATION; COMPOSITES;
D O I
10.1016/j.compstruct.2021.114025
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Barely visible impact damage (BVID) on carbon fibre reinforced polymer (CFRP) aerospace components can create interlaminar defects that may deteriorate during operation with potential failure as a result. Especially damage-prone regions such as the feet of a stiffener must therefore be inspected for BVIDs frequently, which is an effort that increases downtimes and operational costs. The potential of optical fibre sensors as part of a permanently installed structural health monitoring network is well-known. Individual FBG-based strain sensors have shown their capability to detect BVIDs. In this work we introduce a global damage index (GDI) as a figure of merit for the combined response of 60 FBG sensors mounted on several aerospace-grade CFRP flat stiffened panels. We first obtain a detection threshold for the GDI and then demonstrate its use for BVID detection. The proposed methodology is the first of its kind for the representation of the health of a component in a single parameter.
引用
收藏
页数:12
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