INDUCTOR

Induction based Curing Tool for Optimized heating of composite Repairs

 Coordinatore GMI AERO SAS 

 Organization address address: Rue Buffault 9
city: PARIS
postcode: 75009

contact info
Titolo: Mr.
Nome: Roland
Cognome: Chemama
Email: send email
Telefono: +33 6 77771473

 Nazionalità Coordinatore France [FR]
 Totale costo 150˙000 €
 EC contributo 112˙500 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2010-01
 Funding Scheme JTI-CS
 Anno di inizio 2010
 Periodo (anno-mese-giorno) 2010-11-01   -   2012-04-30

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    GMI AERO SAS

 Organization address address: Rue Buffault 9
city: PARIS
postcode: 75009

contact info
Titolo: Mr.
Nome: Roland
Cognome: Chemama
Email: send email
Telefono: +33 6 77771473

FR (PARIS) coordinator 90˙000.00
2    NATIONAL TECHNICAL UNIVERSITY OF ATHENS - NTUA

 Organization address address: HEROON POLYTECHNIOU 9 ZOGRAPHOU CAMPUS
city: ATHINA
postcode: 15780

contact info
Titolo: Ms.
Nome: Georgia
Cognome: Mertzelou
Email: send email
Telefono: +30 210 7722033
Fax: +30 210 7724181

EL (ATHINA) participant 22˙500.00

Mappa


 Word cloud

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

repair    metallic    heat    temperature    differences    mesh    repairs    generation    larger    conduction    induction    currents    heating    placed    special    patch    structure    composite   

 Obiettivo del progetto (Objective)

'Appropriate curing of the patch resin and the adhesive layer is an essential step to secure the integrity and the sound mechanical performance of bonded composite repairs. Today, the required temperature elevation is achieved by means of resistance heating blankets, conducting heat to the repair area. This method is simple and works adequately for small repairs, but when larger areas need to be heated, discrepancies, like cold or hot spots, occur, due to variable heat losses, caused by “heat sinks”. The scope of this proposal is to change the currently used heat generation principle, from conduction to induction heating for large repair cases (i.e. 65x65cm or larger). Heat will be generated within the repair by induced electrical currents (eddy currents) through a coil placed on top of the patch, creating an alternating electromagnetic field to the conductive elements of the repair (susceptors). The system is made of several flexible coils, driven by induction equipment employing multi-channel temperature control, to compensate for differences in temperature development across the structure. The process will be monitored by special software, capable of compensating temperature differences by variable heat generation algorithm. The susceptor will be one or a combination of the following elements: a) the lightning protection metallic mesh placed on top of composite repairs, b) the carbon fibers of the patch and surrounding structure, c) a special metallic mesh embedded into a silicon mat, placed directly on top of the patch. The induction heating method will achieve better temperature homogeneity and process efficiency compared to conventional conduction heating equipment and methods, resulting in direct improvement of the repair quality. As induction heating is a non-contact method, equipment and consumables requirements will be minimized, making induction heating more robust, reliable, faster, cheaper and easier to apply, compared to conduction heating techniques.'

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