BULCANATU

"Developement of CNT doped reinforced aircraft composite parts and a ssociated tooling, using the Liquid Resin Infusion method."

 Coordinatore TECHNICAL & RACING COMPOSITES SL 

 Organization address address: CARRER LLEVANT POLIGONO INDUSTRIAL PLA DE FOGARS 10
city: FOGARS DE LA SELVA
postcode: 8495

contact info
Titolo: Ms.
Nome: Ester
Cognome: Peralta
Email: send email
Telefono: 34972874800

 Nazionalità Coordinatore Spain [ES]
 Totale costo 238˙671 €
 EC contributo 134˙690 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2012-02
 Funding Scheme JTI-CS
 Anno di inizio 2013
 Periodo (anno-mese-giorno) 2013-08-01   -   2015-09-30

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    TECHNICAL & RACING COMPOSITES SL

 Organization address address: CARRER LLEVANT POLIGONO INDUSTRIAL PLA DE FOGARS 10
city: FOGARS DE LA SELVA
postcode: 8495

contact info
Titolo: Ms.
Nome: Ester
Cognome: Peralta
Email: send email
Telefono: 34972874800

ES (FOGARS DE LA SELVA) coordinator 86˙285.80
2    UNIVERSIDAD REY JUAN CARLOS

 Organization address address: CALLE TULIPAN S/N
city: MOSTOLES (MADRID)
postcode: 28933

contact info
Titolo: Dr.
Nome: Susana
Cognome: De Dios Sinovas
Email: send email
Telefono: 34914888156

ES (MOSTOLES (MADRID)) participant 48˙405.00

Mappa


 Word cloud

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

thanks    techniques    epoxy    of    parts    composite    cnt    infusion    resin   

 Obiettivo del progetto (Objective)

'BULCANATU project wants to develop feasible techniques for advanced and cost effective composite manufacturing of aviation parts. The development of new epoxy resin Carbon Nanotube doping techniques compatible with Liquid Resin Infusion will open a new era on fabrication of aerospace parts with improved mechanical properties, thanks to nanoparticles. Future aircraft manufactured with doped CNT epoxy resins, would be the increase on electrical conductivity that could lead to the removal of cooper lightning protection mesh of advanced composite fuselage. The main issues to overcome are the dispersion and stability of the CNT over the epoxy resin, filtration phenomena within the infusion process, and the manufacture of high performance composite parts under “out of autoclave” conditions at greater viscosities than expected. Thanks to the joint venture between TR Composites and the Universidad Rey Juan Carlos, all aspects of the call are covered with wide experience to achieve good results.'

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