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RELIABILITY AND SAFETY ENHANCED ELECTRICAL ACTUATION SYSTEM ARCHITECTURES

Objetivo

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.

Convocatoria de propuestas

FP7-AAT-2013-RTD-Russia
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Coordinador

COMPANIA ESPANOLA DE SISTEMAS AERONAUTICOS SA
Aportación de la UE
€ 372 336,00
Dirección
PASEO JOHN LENNON 4 GETAFE
28906 Madrid
España

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Región
Comunidad de Madrid Comunidad de Madrid Madrid
Tipo de actividad
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Contacto administrativo
Santiago Abelaira Taberna (Mr.)
Enlaces
Coste total
Sin datos

Participantes (6)