DocumentCode :
3094459
Title :
Optical fiber sensors for structural health monitoring in airplanes
Author :
Zubia, Joseba ; Mateo, Javier ; Losada, M.A. ; Durana, Gaizka ; Aldabaldetreku, Gotzon ; Illarramendi, M. Asuncion
Author_Institution :
Univ. of the Basque Country (UPV/EHU), Bilbao, Spain
fYear :
2013
fDate :
23-27 June 2013
Firstpage :
1
Lastpage :
4
Abstract :
Structural health monitoring (SHM) is a cost-effective approach to meet operational requirements, and to reduce maintenance costs in aircrafts. Besides, fiber optic sensor technology is a mature technology which can be used to monitor physical parameters of wing leading-edge surfaces and fuselage sections made of composites carbon fiber-reinforced plastic (CFRP) materials. This paper deals with some applications of plastic and glass optical fiber based sensors for SHM. Among other, we will describe the results we have obtained for damage detection, impact location, strain and deformation measurements. We will also show some results of the blade tip timing and tip clearance in aircraft turbines. These are two of the main parameters governing the efficiency of turbine engine.
Keywords :
aircraft; carbon fibre reinforced plastics; condition monitoring; deformation; fibre optic sensors; turbines; CFRP materials; SHM; aircraft turbines; airplanes; composites carbon fiber-reinforced plastic materials; damage detection; deformation measurements; fuselage sections; glass optical fiber; impact location; optical fiber sensors; physical parameter monitoring; plastic optical fiber; strain measurements; structural health monitoring; turbine engine; wing leading-edge surfaces; Blades; Fiber gratings; Optical fiber sensors; Optical fibers; Strain; Optical fiber sensors; structural health monitoring; tip clearance; tip timing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Transparent Optical Networks (ICTON), 2013 15th International Conference on
Conference_Location :
Cartagena
ISSN :
2161-2056
Type :
conf
DOI :
10.1109/ICTON.2013.6602712
Filename :
6602712
Link To Document :
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