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Proceedings Paper

Application issues of fiber-optic sensors in aircraft structures
Author(s): Zhuo Jun Lu; Franz A. Blaha
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Paper Abstract

This paper considers two important application issues of fiber optic sensors in aircraft structures. The first concerns the interfacing of optical fibers with composite material structures: concepts have been developed for realizing a reliable exit point for the embedded fiber from a composite aircraft component, by means of single-mode connector assemblies embedded in composite material structures. The second issue relates to the temperature stability of the sensors: temperature characteristics of two-mode fiber optic strain sensors were investigated, sensors made of elliptical core and bow-tie fibers are compared, and the trade-offs among strain sensor range, sensitivity and temperature stability are discussed.

Paper Details

Date Published: 1 December 1991
PDF: 6 pages
Proc. SPIE 1588, Fiber Optic Smart Structures and Skins IV, (1 December 1991); doi: 10.1117/12.50186
Show Author Affiliations
Zhuo Jun Lu, Canadian Marconi Co. (Canada)
Franz A. Blaha, Canadian Marconi Co. (Canada)

Published in SPIE Proceedings Vol. 1588:
Fiber Optic Smart Structures and Skins IV
Richard O. Claus; Eric Udd, Editor(s)

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