Health and usage monitoring system for the small aircraft composite structure

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F17%3A00319635" target="_blank" >RIV/68407700:21220/17:00319635 - isvavai.cz</a>
Result on the web
<a href="https://www.scopus.com/record/display.uri?eid=2-s2.0-85025817366&origin=resultslist" target="_blank" >https://www.scopus.com/record/display.uri?eid=2-s2.0-85025817366&origin=resultslist</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1063/1.4989944" target="_blank" >10.1063/1.4989944</a>

Result language
angličtina
Original language name
Health and usage monitoring system for the small aircraft composite structure
Original language description
This paper is focused on the design of the health and usage monitoring system (HUMS) of the composite ultra-light aircrafts. A multichannel measuring system was developed and installed for recording of the long-term operational measurements of the UL airplane. Many fiber Bragg grating sensors were implemented into the composite aircraft structure, mainly in the glue joints. More than ten other analog functions and signals of the aircraft is monitored and can be correlated together. Changing of the FBG sensors responses in monitored places and their correlations, comparing with the calibration and recalibration procedures during a monitored life may indicate damage (eg. in bonded joints) and complements the HUMS system.
Czech name
—
Czech description
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Project
<a href="/en/project/TA04031450" target="_blank" >TA04031450: System for monitoring of structures using fiber optic sensors</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2017
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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