Design of UGW SHM Sensor System for L-39NG Aircraft
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F27617793%3A_____%2F18%3AN0000005" target="_blank" >RIV/27617793:_____/18:N0000005 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Design of UGW SHM Sensor System for L-39NG Aircraft
Original language description
Presented paper introduces the development of SHM sensor system, based on PZT sensors. Honeywell’s SHM system intends to detect change in structural 'health' condition. Change in the structure 'health' may be caused by mechanical damage such as impact, fatigue, corrosion or any other structure damage or degradation.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
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)
Others
Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Proceedings of the Ninth European Workshop - Structural health monitoring
ISBN
9780903132699
ISSN
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e-ISSN
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Number of pages
12
Pages from-to
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Publisher name
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Place of publication
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Event location
Manchester, United Kingdom
Event date
Aug 10, 2018
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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