7 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Reliable Electromechanical actuator for PRImary SurfacE with health monitoring (REPRISE)
Date du début: 1 juil. 2016, Date de fin: 31 déc. 2018,
The REPRISE project responds to the call JTI-CS2-2015-CFP02-SYS-03-01. The objective of the project is the design and development of an innovative electromechanical actuation system with health monitoring for primary-control-surface of a small aircraft. It is well-known that the electromechanical actuation will lead to weight saving and life-cycle cost reduction but some critical issues of this te ...
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3
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TERMINÉ
RELIABILITY AND SAFETY ENHANCED ELECTRICAL ACTUATION SYSTEM ARCHITECTURES (RESEARCH)
Date du début: 1 oct. 2013, Date de fin: 31 août 2016,
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 th ...
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7
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TERMINÉ
Hyper Performance Motor, Air-Cooled (HYPERMAC)
Date du début: 1 mai 2014, Date de fin: 31 août 2016,
The development of a more electrical aircraft is a technological transition applied or envisioned for almost all the systems in the aircrafts and helicopters. Together with the electrification of aircraft actuation systems, also the implementation of an electric propulsion can lead to many advantages in terms of reduced specific consumption, noise reduction, weight and volume saving. Anyway this t ...
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3
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TERMINÉ
Health On Line Monitoring for Electro-mechanical actuator Safety (HOLMES)
Date du début: 1 nov. 2013, Date de fin: 30 juin 2016,
... to meet these requirements is the implementation of advanced health monitoring systems. Use of sensors for the detection of failures has been successfully proved by the research community, including Umbra, but the challenge of the HOLMES project is to rely on components that are basic on an EMA like electric motors, position sensors, motor commutation devices without additional sensing on the int ...
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2
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TERMINÉ
Disconnect device for jam tolerant linear actuators (FASTDISC)
Date du début: 1 févr. 2013, Date de fin: 30 juin 2016,
...n and Industrial Design of the University of Stuttgart (IKTD) has research experience in and expert knowledge on the development of fast operating connect/disconnect devices.- The Italian company Umbra (Umbra) is a highly competent manufacturer and supplier of components for the aerospace industry like ballscrews, actuators and EMA drives.- The German company PyroGlobe is a highly competent manufa ...
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4
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TERMINÉ
Drivetrain Rolling Elements in Aeronautics, Design and Sizing for (DREADS)
Date du début: 1 févr. 2013, Date de fin: 30 juin 2016,
In the scope of the development of a more electrical aircraft, this subject aims at the development and the experimental validation of a reliable sizing method for mechanical transmission elements, specifically screw drives and thrust bearings of aeronautic flight control actuation system. In fact the replacement of the hydraulic with electric devices promises many advantages but we have to pay at ...
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3
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TERMINÉ
ACTUATION 2015: Modular Electro Mechanical Actuators for ACARE 2020 Aircraft and Helicopters (ACTUATION2015)
Date du début: 1 nov. 2011, Date de fin: 30 avr. 2016,
The All-Electric Aircraft is a major target for the next generation of aircraft to lower consumption of non-propulsive power and thus fuel burn. To eliminate hydraulic circuits, pumps and reservoirs, Electro Mechanical Actuators (EMA) are mandatory but now need to meet cost, reliability and weight requirements from the airframers.ACTUATION2015 aims to develop and validate a common set of standard ...
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