Towards damage and structural health monitoring of aerospace composite structures using optical fiber sensors

被引:0
|
作者
Takeda, N. [1 ]
机构
[1] Univ Tokyo, Grad Sch Frontier Sci, Kashiwa, Chiba 2778561, Japan
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Optical fiber sensors are promising as tools for damage and structural health monitoring (SHM) of aerospace composite structures. The authors and Hitachi Cable, Ltd. have recently developed small-diameter optical fiber and its fiber Bragg grating (FBG) sensor for embedment inside a lamina of composite laminates without strength reduction. First, a brief summary is presented for some previous studies on the small-diameter FBG sensors for damage monitoring and SHM of composite structures. Then, some recent results in the current ACS-SIDE project are presented on optical fiber based SHM for some feasible applications in aerospace composite structures, which include (1) PZT/FBG hybrid sensing system for bond-line monitoring in CFRP box structures, (2) Highly reliable advanced grid structures (HRAGS), and (3) Distributed strain sensing using Brillouin optical correlation domain analysis.
引用
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页码:34 / 45
页数:12
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