Fiber optic strain sensor system for structural analysis of jet engine air intake

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F19%3A00338734" target="_blank" >RIV/68407700:21220/19:00338734 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Fiber optic strain sensor system for structural analysis of jet engine air intake
Original language description
This paper describes experimental verification of a fiber optic strain sensor system for a composite air intake. The new L-39NG jet trainer aircraft from Aero Vodochody is equipped with all-composite air intake. Because there is a need of its acoustic load analysis, both optical and electric strain sensors were installed to its surface. Engine ground test was performed to test fiber optic sensor system at first. It was found that the system is fully functional with capability to provide the required performance. Acquired data were used for further air intake design improvement.
Czech name
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Czech description
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Project
<a href="/en/project/TE02000032" target="_blank" >TE02000032: Advanced Aerostructures Research Centre</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
EAN 2019 57th conference on experimental stress analysis CONFERENCE PROCEEDINGS
ISBN
9788021457669
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
77-80
Publisher name
Česká společnost pro mechaniku
Place of publication
Praha
Event location
Luhačovice
Event date
Jun 3, 2019
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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