RESEARCH
Financiado
RELIABILITY AND SAFETY ENHANCED ELECTRICAL ACTUATION SYSTEM ARCHITECTURES
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...
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.
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Duración del proyecto: 34 meses
Fecha Inicio: 2013-10-01
Fecha Fin: 2016-08-31
Fecha Fin: 2016-08-31
Línea de financiación: concedida
El organismo FP7 notifico la concesión del proyecto el día 2016-08-31
FP7
No se conoce la línea exacta de financiación, pero conocemos el organismo encargado de la revisión del proyecto.
Presupuesto
El presupuesto total del proyecto asciende a
3M€
Líder del proyecto
COMPANIA ESPANOLA DE SISTEMAS AERONAUTICOS
No se ha especificado una descripción o un objeto social para esta compañía.
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