JIF2LAND

Jigs and Fixtures for Assembly of the Laminar Wing at the BLADE flight test demonstrator Final Assembly Line

 Coordinatore "ARITEX CADING,S.A." 

 Organization address address: C/ Progres 319
city: Badalona
postcode: 8918

contact info
Titolo: Mr.
Nome: Carlos
Cognome: Mendez
Email: send email
Telefono: 34933984111

 Nazionalità Coordinatore Spain [ES]
 Totale costo 899˙988 €
 EC contributo 516˙737 €
 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) 2014-09-01   -   2016-12-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    "ARITEX CADING,S.A."

 Organization address address: C/ Progres 319
city: Badalona
postcode: 8918

contact info
Titolo: Mr.
Nome: Carlos
Cognome: Mendez
Email: send email
Telefono: 34933984111

ES (Badalona) coordinator 316˙504.80
2    FUNDACIO PRIVADA ASCAMM

 Organization address address: "AVENIDA UNIVERSITAT AUTONOMA , PARC TECNOLOGIC DEL VALLES 23"
city: CERDANYOLA DEL VALLES
postcode: 8290

contact info
Titolo: Mr.
Nome: ángel
Cognome: Lagraña
Email: send email
Telefono: 34648725077

ES (CERDANYOLA DEL VALLES) participant 200˙233.00

Mappa


 Word cloud

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

wing    original    wings    tooling    flight    laminar    flow    compensation   

 Obiettivo del progetto (Objective)

'The objective of JIF2LAND proposal it to conduct the evelopment, design, manufacture and installation of jig platforms, staging and operational tooling for removing the BLADE wing (Natural Laminar Flow) sections of an A340-300, after the flight test and to assembly the original wings tips of the aircraft. The SFWA flight test demonstrator aims to validate that a specific wing profile can sustain laminar flow with an acceptable stability versus in flight deformation and contamination. After the flight test the original wings will need to be restored and challenging tooling design and manufacturing are expected, beside the challenges an added one will be to be very cost-effective for a tooling to be one time used. Temperature compensation, twist compensation, tolerance achievements are some of the key points to be addressed on this development.'

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