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Content archived on 2024-06-18

RELIABILITY AND SAFETY ENHANCED ELECTRICAL ACTUATION SYSTEM ARCHITECTURES

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.

Call for proposal

FP7-AAT-2013-RTD-Russia
See other projects for this call

Coordinator

COMPANIA ESPANOLA DE SISTEMAS AERONAUTICOS SA
EU contribution
€ 372 336,00
Address
PASEO JOHN LENNON 4 GETAFE
28906 Madrid
Spain

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Region
Comunidad de Madrid Comunidad de Madrid Madrid
Activity type
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Administrative Contact
Santiago Abelaira Taberna (Mr.)
Links
Total cost
No data

Participants (6)