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
来源：
THIRD ASIA PACIFIC OPTICAL SENSORS CONFERENCE | 2012年 / 8351卷
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.
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页数：8
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