RESEARCH
RELIABILITY AND SAFETY ENHANCED ELECTRICAL ACTUATION SYSTEM ARCHITECTURES
| Coordinatore | COMPANIA ESPANOLA DE SISTEMAS AERONAUTICOS
Organization address
address: AVENIDA JOHN LENNON 4 contact info |
| Nazionalità Coordinatore | Spain [ES] |
| Totale costo | 3˙404˙582 € |
| EC contributo | 1˙177˙472 € |
| Programma | FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics) |
| Code Call | FP7-AAT-2013-RTD-Russia |
| Funding Scheme | CP-FP |
| Anno di inizio | 2013 |
| Periodo (anno-mese-giorno) | 2013-10-01 - 2016-03-31 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
COMPANIA ESPANOLA DE SISTEMAS AERONAUTICOS
Organization address
address: AVENIDA JOHN LENNON 4 contact info |
ES (MADRID (GETAFE)) | coordinator | 372˙336.00 |
| 2 |
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
Organization address
address: Avenue de la Division Leclerc 29 contact info |
FR (CHATILLON) | participant | 299˙127.00 |
| 3 |
UMBRA CUSCINETTI SPA
Organization address
address: LOCALITA PACIANA ZONA INDUSTRIALE contact info |
IT (FOLIGNO PERUGIA) | participant | 270˙000.00 |
| 4 |
FUNDACION TECNALIA RESEARCH & INNOVATION
Organization address
address: PARQUE TECNOLOGICO DE MIRAMON PASEO MIKELETEGI 2 contact info |
ES (DONOSTIA-SAN SEBASTIAN) | participant | 236˙009.00 |
| 5 |
FEDERAL STATE UNITARY ENTERPRISE THE CENTRAL AEROHYDRODYNAMIC INSTITUTE NAMED AFTER PROF. N.E. ZHUKOVSKY
Organization address
address: Zhukovsky str 1 contact info |
RU (ZHUKOVSKY) | participant | 0.00 |
| 6 |
JOINT STOCK COMPANY UNITED AIRCRAFT CORPORATION
Organization address
address: "ULANSKY PEREULOK 22, BLDG. 1" contact info |
RU (MOSKVA) | participant | 0.00 |
| 7 |
STATE EDUCATIONAL INSTITUTION OF HIGHER PROFESSIONAL EDUCATION MOSCOW AVIATION INSTITUTE STATE TECHNICAL UNIVERSITY
Organization address
address: Volokolamskoe Shosse 4 contact info |
RU (MOSKVA) | participant | 0.00 |
Mappa
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Obiettivo del progetto (Objective)
'The main objective of RESEARCH project is the definition of an electrical architecture for Flight Control System capable of controlling a flight control surface on an Aircraft with the help of electrically operated actuators, thus replacing the hydraulic actuators commonly used in current Aircraft designs. This architecture will be designed with the main objective of being electrical, as this is the main purpose of this call, and certifiable, since the intention is to be able to use it in a possible future Aircraft. The objective of the RESEARCH project is to find a robust architecture to meet the constraints imposed by safety regulations while keeping other system performances (as weight, Reliability) as optimal as possible.'