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 TERMINÉ 
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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 56

 TERMINÉ 
"HYPOTHESIS is a focused RTD project that will investigate the feasibility of a High Temperature Intelligent High Integrated Power Electronics Module for aeronautic applications based on fast switching semiconductors, most probably using Silicon Carbide technology for the first generation power modules. The recent release of 1200V SiC power transistors (MOSFET’s, JFET’s…) with strongly improved sw ...
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 1

 TERMINÉ 

Smart Silicon on Insulator Sensing Systems Operating at High Temperature (SOI-HITS)

Date du début: 1 sept. 2011, Date de fin: 31 déc. 2014,

SOI-HITS is an ambitious, innovative and timely STREP project that will enable significant energy consumption savings and reduce waste in processes such as: combustion in domestic boilers; oil & gas storage and transportation; CO2 capture and sequestration. It aims to deliver at least 15% saving of energy consumption in domestic boiler industry (~40 million domestic boilers in the EU with a growth ...
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 8

 TERMINÉ 

High Temperature Electronics (HiTME)

Date du début: 4 janv. 2011, Date de fin: 3 avr. 2014,

The migration of electronic control units from the engine fan-case to the core would be considered a huge benefit for the engine designer, reducing interconnection complexity and system weight, simplifying assembly and maintenance and providing key nacelle aerodynamic and bypass flow improvements.However, today’s engine control electronics, typically mounted on the engine fan-case, operates to a m ...
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 4

 TERMINÉ 
"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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