The use of Fiber Bragg Grating sensors during the static load test of a composite wing structure
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F14%3A00215187" target="_blank" >RIV/68407700:21220/14:00215187 - isvavai.cz</a>
Result on the web
<a href="http://www.scopus.com/record/display.url?eid=2-s2.0-84892159902&origin=inward&txGid=B49100522A34C861A307E062E923B249.f594dyPDCy4K3aQHRor6A%3a1" target="_blank" >http://www.scopus.com/record/display.url?eid=2-s2.0-84892159902&origin=inward&txGid=B49100522A34C861A307E062E923B249.f594dyPDCy4K3aQHRor6A%3a1</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.4028/www.scientific.net/AMM.486.102" target="_blank" >10.4028/www.scientific.net/AMM.486.102</a>
Alternative languages
Result language
angličtina
Original language name
The use of Fiber Bragg Grating sensors during the static load test of a composite wing structure
Original language description
The article describes process of implementation of optical Fiber Bragg Grating (FBG) sensors into the composite wing structure and their behavior during the strength test. The wing is of all-composite construction. The upper and lower skins are made of glass/epoxy composite. The spar caps are made of carbon/epoxy unidirectional composite. Optical fibers were integrated directly into the spar caps and into the adhesive joints. They were oriented in parallel with the main spar axis. The first optical fiber with chain of multiple FBG sensors was integrated into the structure of upper spar cap. Another FBG chain of FBG sensors was located in the adhesive joint of lower spar cap and shear web. The wing was instrumented with strain gages as well. Strain gages were glued to the sides of the spar caps. Static load was produced by a hydraulic actuator. Experimental results from strain gages and FBG sensors were compared with the results of the analytical analysis of the wing.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JI - Composite materials
OECD FORD branch
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Result continuities
Project
<a href="/en/project/FR-TI1%2F290" target="_blank" >FR-TI1/290: *The model of a composite control surface for a large aeroplane in complience with the certification specification CS-25</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
51st Annual of the International Scientific Conference on Experimental Stress Analysis, EAN 2013
ISBN
978-3-03785-977-3
ISSN
1660-9336
e-ISSN
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Number of pages
4
Pages from-to
102-105
Publisher name
Trans Tech Publications Ltd
Place of publication
Kreuzstrasse 10, 8635 Durnten-Zurich
Event location
Litoměřice
Event date
Jun 11, 2013
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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