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5 European Projects Found

Searched on 125080 European Projects

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The aims of the NanoMaster project are to reduce the amount of plastic used to make a component by 50% and hence reduce component weight by 50%, at the same time as imparting electrical and thermal functionality. This will be achieved by developing the next generation of graphene-reinforced nano-intermediate that can be used in existing high-throughput plastic component production processes.Graphe ...
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Fuel Control System Sensors and Effectors (CASE)

Start date: Jan 4, 2011, End date: Jul 3, 2014,

This abstract highlights the approach taken to meeting the technical requirements of the call, the partnership with two SMEs, the European dimension of the proposal, and the inclusion of universities and specialist sub-contractors.AEC has identified specific technologies (eddy current and ultrasonic acoustic sensors, and piezoelectric actuators) as having significant potential for new forms of imp ...
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High Temperature Electronics (HiTME)

Start date: Jan 4, 2011, End date: Apr 3, 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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Lean Burn Control System Verification Rig (LeVeR)

Start date: Jan 3, 2012, End date: Jan 2, 2014,

The objective of this project is to provide a novel, fully operational and commissioned test facility for the system verification of the new, highly complex lean burn engine control system necessary for more fuel efficient medium and large aero-engine system applications. This validation facility does not exist today and capability will include interaction with the donor-engine fuel system with no ...
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High Efficiency Fuel Pumping (AdEPT)

Start date: Jan 4, 2011, End date: Jan 3, 2013,

The concept of this project is the TRL 6 demonstration of a high speed, light weight, large capacity variable displacement piston pump for medium and large aero-engine fuel system applications, capable of high efficiency performance at fuel flows of up to 40,000 pounds per hour and pressures up to 2200 pounds per square inch.Piston pumps currently find application on the fuel systems of small and ...
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