Application of piezoelectric sensors for structural health monitoring in aerospace

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F18%3APU130042" target="_blank" >RIV/00216305:26210/18:PU130042 - isvavai.cz</a>

Výsledek na webu

<a href="https://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=8443161" target="_blank" >https://ieeexplore.ieee.org/xpl/mostRecentIssue.jsp?punumber=8443161</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/MetroAeroSpace.2018.8453610" target="_blank" >10.1109/MetroAeroSpace.2018.8453610</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Application of piezoelectric sensors for structural health monitoring in aerospace

Popis výsledku v původním jazyce

This paper deals with an innovative approach for SHM with piezoelectric elements utilized as active sensors. The increasing interest in reduction of maintenance costs of aircrafts can be solved by embedding permanent and self-sufficient monitoring networks into the structure of the aircraft in order to prevent structural failures. Piezoelectric elements are currently undergoing a rapid development and due to their inexpensive and non-intrusive nature, they can be used to assemble such monitoring networks. The proposed method utilizes a virtual model of the structure to pinpoint suitable locations for the sensors with respect to the requirement of local and global SHM, serving as an initial point for further research to describe behaviour of the structure during operation and predict any inadmissible state.

Název v anglickém jazyce

Application of piezoelectric sensors for structural health monitoring in aerospace

Popis výsledku anglicky

This paper deals with an innovative approach for SHM with piezoelectric elements utilized as active sensors. The increasing interest in reduction of maintenance costs of aircrafts can be solved by embedding permanent and self-sufficient monitoring networks into the structure of the aircraft in order to prevent structural failures. Piezoelectric elements are currently undergoing a rapid development and due to their inexpensive and non-intrusive nature, they can be used to assemble such monitoring networks. The proposed method utilizes a virtual model of the structure to pinpoint suitable locations for the sensors with respect to the requirement of local and global SHM, serving as an initial point for further research to describe behaviour of the structure during operation and predict any inadmissible state.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20304 - Aerospace engineering

Projekt

<a href="/cs/project/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Centrum pokročilých leteckých technologií</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>O - Projekt operacniho programu

Rok uplatnění

2018

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Proceedings

ISBN

978-1-5386-2473-9

ISSN

—

e-ISSN

—

Počet stran výsledku

6

Strana od-do

596-601

Název nakladatele

Institute of Electrical and Electronics Engineers Inc.

Místo vydání

Rome, Italy

Místo konání akce

Rome

Datum konání akce

20. 6. 2018

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

000454855500111