FOS3D

Fiber Optic System for Deflection and Damage Detection

 Coordinatore Aerospace & Advanced Composites GmbH 

 Organization address address: Viktor-Kaplan-Strasse 2
city: Wiener Neustadt
postcode: 2700

contact info
Titolo: Ms.
Nome: Margit
Cognome: Kovacic
Email: send email
Telefono: 4326230000000
Fax: 4326230000000

 Nazionalità Coordinatore Austria [AT]
 Totale costo 598˙226 €
 EC contributo 448˙669 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2010-03
 Funding Scheme JTI-CS
 Anno di inizio 2011
 Periodo (anno-mese-giorno) 2011-12-01   -   2014-02-28

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    Aerospace & Advanced Composites GmbH

 Organization address address: Viktor-Kaplan-Strasse 2
city: Wiener Neustadt
postcode: 2700

contact info
Titolo: Ms.
Nome: Margit
Cognome: Kovacic
Email: send email
Telefono: 4326230000000
Fax: 4326230000000

AT (Wiener Neustadt) coordinator 222˙511.50
2    INTEGRATED MICROSYSTEMS AUSTRIA GMBH

 Organization address address: VIKTOR KAPLAN STRASSE 2
city: WIENER NEUSTADT
postcode: 2700

contact info
Titolo: Ms.
Nome: Jischa
Cognome: Alexandra
Email: send email
Telefono: +43 2622 22859 15

AT (WIENER NEUSTADT) participant 226˙158.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

optic    actuated    damage    deflection    wing    monitoring    fiber   

 Obiettivo del progetto (Objective)

'Within the EC Clean Sky - Smart Fixed Wing Aircraft initiative concepts for actuating morphing wing structures are under development. In order for developing a complete integrated system including the actuation, the structure to be actuated and the closed loop control unit a hybrid deflection and damage monitoring system is required. The aim of the proposed project 'FOS3D' is to develop and validate a fiber optic sensing system based on low-coherence interferometry for simultaneous deflection and damage monitoring. The proposed system uses several distributed and multiplexed fiber optic Michelson interferometers to monitor the strain distribution over the actuated part. In addition the same sensor principle will be used to acquire and locate the acoustic emission signals originated from the onset and growth of defects like impact damages, cracks and delaminations.'

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