The technology of composite patches and their structural reliability inspection using infrared imaging

被引:45
作者
Avdelidis, NP [1 ]
Moropoulou, A
Riga, ZPM
机构
[1] Univ Bath, Mat Res Ctr, Bath BA2 7AY, Avon, England
[2] Natl Tech Univ Athens, Sch Chem Engn, Sect Mat Sci & Engn, Athens 15780, Greece
[3] Hellen Aerosp Ind, Dept Res & Dev, Composite Mat & Proc Lab, Schimatari 32009, Greece
关键词
Composite materials - Corrosion - Fatigue of materials - Stability - Thermography (imaging);
D O I
10.1016/S0376-0421(03)00002-2
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Nowadays, composite components and reinforcements are widely used in aircraft repair technology, since they present more efficient performance than conventional repairs. Composite patches (carbon or boron fibres) have been used for many years, mainly for research purposes, in aircraft maintenance. This move towards composites is mainly because of the increased mechanical performance, less corrosion and fatigue problems, allowing for longer service life of the aircraft. In this work, the technology and use of composite patching was described and reviewed. Furthermore, since the detection of structures integrity under patch, during the service life of aircraft, by non-destructive means is considered of great importance, infrared thermography was used for the detection of simulated artificially introduced damages-cracks, on the surface of Al 2024-T3 aircraft skin panels under composite patching or simulated delaminations between two plies of composite patches. Finally, real-time monitoring of damage during fatigue loading using thermography was also discussed and attempted in the laboratory on aircraft repaired panels. (C) 2003 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:317 / 328
页数:12
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