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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

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    JI - Composite materials

  • OECD FORD branch

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

  • 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