ELWIPS

Electro-thermal Laminar Wing Ice Protection System Demonstrator

 Coordinatore ARTUS SAS 

 Organization address address: CHEMIN DU CHAMP DES MARTYRS
city: AVRILLE
postcode: 49241

contact info
Titolo: Mr.
Nome: Marcello
Cognome: Biondi
Email: send email
Telefono: +33 2 41 33 63 42

 Nazionalità Coordinatore France [FR]
 Totale costo 1˙498˙445 €
 EC contributo 888˙216 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2011-03
 Funding Scheme JTI-CS
 Anno di inizio 2012
 Periodo (anno-mese-giorno) 2012-10-01   -   2016-12-31

 Partecipanti

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

 Organization address address: CHEMIN DU CHAMP DES MARTYRS
city: AVRILLE
postcode: 49241

contact info
Titolo: Mr.
Nome: Marcello
Cognome: Biondi
Email: send email
Telefono: +33 2 41 33 63 42

FR (AVRILLE) coordinator 153˙440.96
2    MEGGITT AEROSPACE LIMITED

 Organization address address: ATLANTIC HOUSE AVIATION PARK WEST
city: CHRISTCHURCH
postcode: BH23 6EW

contact info
Titolo: Mr.
Nome: Ian
Cognome: Cowley
Email: send email
Telefono: +44 0 1509 500008

UK (CHRISTCHURCH) participant 317˙794.21
3    THE UNIVERSITY OF SHEFFIELD

 Organization address address: FIRTH COURT WESTERN BANK
city: SHEFFIELD
postcode: S10 2TN

contact info
Titolo: Ms.
Nome: Joanne
Cognome: Watson
Email: send email
Telefono: 441142000000

UK (SHEFFIELD) participant 294˙828.90
4    AEROTEX UK LLP

 Organization address address: "SENTINEL HOUSE HARVEST CRESCENT, ANCELLS BUSINESS PARK"
city: FLEET
postcode: GU51 2UZ

contact info
Titolo: Mr.
Nome: Richard
Cognome: Moser
Email: send email
Telefono: +44 1252 540693

UK (FLEET) participant 122˙152.53

Mappa


 Word cloud

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

protection    etips    ice    wing    heater    consumption    laminar    weight    tested    power   

 Obiettivo del progetto (Objective)

'This proposal regards designing, building and testing a functional prototype of part of a laminar wing fitted with electro-thermal ice protection (ETIPS) for a business jet. The aim is to show innovation in the use of composite materials for the fixed leading edge, (e.g. Fibre/Metal Laminates), which are thermally efficient, can be manufactured to tight laminar wing tolerances and comparable to aluminium for weight & cost. Furthermore, the structure will be evaluated for its basic damage resistance properties and ease of repair. The ETIPS aspects will be innovative through a focus on minimising power consumption, using sensors to allow power demand management and thereby achieve a Smart ETIPS. Different types of heater elements will be tested in a range of configurations to optimise ice protection coverage and power consumption. Trials will also be conducted to minimise the weight of the ETIPS heater elements, controllers and wiring. Several structural and layout trade-off studies will be conducted and the final solution tested in an icing wind tunnel.'

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