Debonding monitoring of a composite repair patch using small-diameter FBG sensors

被引:1
作者
Takeda, SI [1 ]
Yamamoto, T [1 ]
Okabe, Y [1 ]
Takeda, N [1 ]
机构
[1] Univ Tokyo, Takeda Lab, Komaba Open Labs, Grad Sch Frontier Sci,Meguro Ku, Tokyo 1538904, Japan
来源
SMART STRUCTURES AND MATERIALS 2004: SMART STRUCTURES AND INTEGRATED SYSTEMS | 2004年 / 5390卷
关键词
FBG sensor; composite patch; fatigue; debonding; health monitoring;
D O I
10.1117/12.539722
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
This paper presents the health monitoring technique of composite repair patches using small-diameter fiber Bragg grating (FBG) sensors. The composite patch structures consist of carbon fiber reinforced plastic (CFRP) patches, aluminum substrates and adhesive layers. The debonding progressed between aluminum substrate and the adhesive layers under cyclic loading. In this research, two types of the specimen were prepared for evaluation of the debonding size. One is specimen with the patches glued on the both side of the aluminum plate. The other is pre-notched specimen for investigation of the influence of the crack propagation in the substrate. The FBG sensors were embedded into the adhesive layers easily, because the diameter of the sensor was only 52 mum. Reflection spectra from the sensor were measured at various lengths of the debonding. The form of the spectrum changed sensitively with an increase in the debonding size. For confirmation of the measured results, the spectra were simulated theoretically. As a result, the change in the calculated spectrum was consistent with that in the measured spectrum, and the relation between the spectrum and the debonding was clarified. Moreover, the debonding length was evaluated quantitatively by the monitoring of the form of the reflection spectrum.
引用
收藏
页码:495 / 504
页数:10
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