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.

引用

页数：8

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