IMPNLFFD

"Design, Manufacturing, Qualification and Assembly of an Improved NLF Wing Leading Edge and Upper Cover Flight Test Article"

 Coordinatore GKN Aerospace Services Limited 

 Organization address address: Ferry Road
city: East Cowes
postcode: PO32 6RA

contact info
Titolo: Mr.
Nome: Will
Cognome: Broom
Email: send email
Telefono: +44 117317547

 Nazionalità Coordinatore United Kingdom [UK]
 Totale costo 2˙150˙000 €
 EC contributo 1˙075˙000 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2013-03
 Funding Scheme JTI-CS
 Anno di inizio 2014
 Periodo (anno-mese-giorno) 2014-07-01   -   2016-01-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    GKN Aerospace Services Limited

 Organization address address: Ferry Road
city: East Cowes
postcode: PO32 6RA

contact info
Titolo: Mr.
Nome: Will
Cognome: Broom
Email: send email
Telefono: +44 117317547

UK (East Cowes) coordinator 1˙075˙000.00

Mappa


 Word cloud

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

laminar    metallic    flight    edge    starboard    manufacture    cover    aircraft    wing    flow    upper    impnlffd    engineering    natural   

 Obiettivo del progetto (Objective)

'A Natural Laminar Flow (NLF) aerofoil is considered to be one of the key technologies to reduce drag and improve the performance of an aircraft; it is also identified as a potential key technology for the next generation of aircraft. The ImpNLFFD project is a critical enabler that will, through mature design concept and stress justification, facilitate the manufacture of the starboard Upper Cover and Metallic Leading Edge of an A340-300 test aircraft and validate that the required level of aerodynamic surface quality can achieve Natural Laminar Flow.

The ImpNLFFD project objectives surround the finalisation and maturity of engineering data to enable subsequent manufacture of an advanced composite starboard Upper Cover and Metallic Leading Edge for installation on the flight test aircraft wing. To support this objective a number of work packages are identified that progress the current status of engineering through to delivery of hardware, concession support, permit to fly, and support operations during the final wing assembly and flight test campaign.'

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CORA (2010)

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