7 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Avionics Systems Hosted on a distributed modular electronics Large scale dEmonstrator for multiple tYpe of aircraft (ASHLEY)
Date du début: 1 oct. 2013, Date de fin: 30 sept. 2017,
...ibution.• Development of an efficient system designer oriented IMA2G Tooling Framework solution that remains compliant with IMA2G industrial and certification constraints.• Development of a generation of digital i.e. smart sensors based on new advanced photonics technologies.ASHLEY innovations will be supported by advanced processes, methods and tools for an efficient implementation in the future ...
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39
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TERMINÉ
All Condition Operations and Innovative Cockpit Infrastructure (ALICIA)
Date du début: 1 sept. 2009, Date de fin: 31 août 2014,
...kload and improving overall aircraft safety. All Conditions Operations, other challenging applications and the desire for reduced crew will mean that the crew station interface will be challenged beyond the reach of the current state-of-the-art. Accordingly, a radical rethink is required to manage the escalating complexity whilst simultaneously enhancing safety and controlling through life cost. ...
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42
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TERMINÉ
Development of High Temperature Survival Electronic Devices for Engine Control Systems (HIGHTECS)
Date du début: 1 janv. 2010, Date de fin: 31 juil. 2013,
...tform with fir for purpose functionality that can be deployed close to the sensors and integrated into a miniature multi-chip module. The unit will be designed to provide signal conditioning for a range of sensor outputs and managing the signal to enable high integrity digital signal tranmission to the FADEC/EHMS units. The target long temperature of operation is 250oC for up to 5 years."
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3
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TERMINÉ
Open Rotor Engines Advanced Technologies II (OREAT II)
Date du début: 1 déc. 2011, Date de fin: 31 juil. 2013,
... introduction of more fuel-efficient propulsion systems, one of which is the Open Rotor Engine concept. Unlike turbofans, open rotors must vary blade pitch to accommodate power and aircraft speed range, so a key element to the viability of the concept is the actuation and control of the blade pitch via the Pitch Change Mechanism (PCM). GE Company Polska, Warsaw Institute of Aviation and GE Aviati ...
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3
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TERMINÉ
SCAlable & ReconfigurabLe Electronics plaTforms and Tools (SCARLETT)
Date du début: 1 mai 2008, Date de fin: 30 avr. 2012,
"The first generation of Integrated Modular Avionics (IMA1G) has been researched via European funded research projects; PAMELA, NEVADA and VICTORIA. This technology supported a revolutionary step away from federated architectures and their classical bespoke electronics to a modular architecture with common resources. IMA1G was introduced to the market on the A380, A400M and B787 aircraft. IMA1G re ...
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39
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TERMINÉ
valiDation of Radical Engine Architecture systeMs (DREAM)
Date du début: 1 févr. 2008, Date de fin: 31 janv. 2012,
... reduction per operation point for the engine alone compared to the Year 2000 engine reference. These breakthroughs will be achieved by designing and rig testing: – Innovative engine concepts – a geared and a direct drive contra-rotating open rotor (unducted propulsion system) – Enabling architectures with novel active and passive engine systems to reduce vibrations These technologies will support ...
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46
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TERMINÉ
Open Rotor Engines Advanced Technologies for rotor blade pitch change mechanism (OREAT)
Date du début: 1 janv. 2010, Date de fin: 30 sept. 2011,
"Pitch Change Mechanism Conceptual and Preliminary Design Activities. A principal contributor to affordable and sustainable public air transportation will be the introduction of more fuel-efficient propulsion systems, one of which is the Open Rotor Engine concept. Unlike turbofans, open rotors must vary blade pitch to accommodate power and aircraft speed range, so a key element to the viability of ...
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