4 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Development of key technology components for high performance electric motors (HPEM)
Date du début: 1 déc. 2012, Date de fin: 30 nov. 2014,
"HPEM technological research program proposes the integration of emerging permanent magnet motor and position sensor technologies in high power density, fault tolerant actuator designs which could be an integral part of a rotorcraft swashplate electromechanical actuation system with superior dynamic response and fault ride through capability. Innovative permanent magnet and insulating material tec ...
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1
Participant partenaire
TERMINÉ
Innovative Technological platform for Compact and Reliable Electronic integrated in Actuators and Motors (CREAM)
Date du début: 1 sept. 2009, Date de fin: 28 févr. 2013,
"The actual political, environmental and economical trends applied to air transport lead to move in the future to the All Electric Aircraft. The goal of this concept is to eliminate as many hydraulic power sources and complicated circuit of high-pressure hydraulic lines as possible. The CREAM objective is to reach new high performance and reliability capacities of Electro-Mechanical Actuators in ...
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15
Participants partenaires
TERMINÉ
Electric Motor And Sensor design and manufacture (EMAS)
Date du début: 1 avr. 2011, Date de fin: 30 juin 2012,
"EMAS proposes a technological research program enabling to develop, validate and manufacture eight actuators presenting high performance and high reliability for high speed applications under high temperature environment. Such actuators will be capable of producing 5 N.m torque under 10.000 rpm for an environmental temperature of 100 C involving low short circuit current and will be supplied by s ...
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1
Participant partenaire
TERMINÉ
ODICIS - One DIsplay for a Cockpit Interactive Solution (ODICIS)
Date du début: 1 mai 2009, Date de fin: 30 avr. 2012,
"ODICIS project aims at developing a single display cockpit and at studying its concept of use. This addresses three current major aeronautics needs: system architecture flexibility, useful surface optimization and information continuity. Therefore the project will improve the operational safety and efficiency and reduce the aircraft development cost. The first objective is to prove the technical ...
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