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...
ver más
¿Tienes un proyecto y buscas un partner? Gracias a nuestro motor inteligente podemos recomendarte los mejores socios y ponerte en contacto con ellos. Te lo explicamos en este video
Proyectos interesantes
SafePEM
Safe Fieldbus dEvelopment for Power Electronic Module
497K€
Cerrado
FLIGHT-EMA (E-RUDDER)
Advanced Flight control system Design Development and Manu...
1M€
Cerrado
AEGART
AIRCRAFT ELECTRICAL GENERATION SYSTEM WITH ACTIVE RECTIFICAT...
2M€
Cerrado
Fecha límite de participación
Sin fecha límite de participación.
Descripción del proyecto
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.