Smart Aircraft Composite Structures with Embedded Small-Diameter Optical Fiber Sensors

被引:2
|
作者
Takeda, Nobuo [1 ]
Minakuchi, Shu [1 ]
机构
[1] Univ Tokyo, Grad Sch Frontier Sci, Dept Adv Energy, Kashiwa, Chiba 2778561, Japan
关键词
Fiber optic sensor; structural health monitoring; composite structures; aerospace structures; DAMAGE DETECTION; SPATIAL-RESOLUTION;
D O I
10.1117/12.915129
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 talk describes the embedded optical fiber sensor systems for smart aircraft composite structures. First, a summary of the current Japanese national project on structural integrity diagnosis of aircraft composite structures is described with special emphasis on the use of embedded small-diameter optical fiber sensors including FBG sensors. Then, some examples of life-cycle monitoring of aircraft composite structures are presented using embedded small-diameter optical fiber sensors for low-cost and reliable manufacturing merits.
引用
收藏
页数:8
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