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Proceedings Paper

Smart aircraft composite structures with embedded small-diameter optical fiber sensors
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Paper Abstract

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.

Paper Details

Date Published: 31 January 2012
PDF: 8 pages
Proc. SPIE 8351, Third Asia Pacific Optical Sensors Conference, 83510I (31 January 2012); doi: 10.1117/12.915129
Show Author Affiliations
Nobuo Takeda, The Univ. of Tokyo (Japan)
Shu Minakuchi, The Univ. of Tokyo (Japan)


Published in SPIE Proceedings Vol. 8351:
Third Asia Pacific Optical Sensors Conference

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