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 TERMINÉ 

Engine Breakthrough Components and Subsystems (E-BREAK)

Date du début: 1 oct. 2012, Date de fin: 31 mars 2017,

Future aero engines will need to be more efficient and contribute to the reduction on environmental impact of air transportation. They must reach some standards of performance by reducing emissions and creating some savings on operation costs.EIMG consortium has launched since several years some initiatives to develop future engines in the frame of the European Committee research programmes.Within ...
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 48

 TERMINÉ 

Fuel Injector Research for Sustainable Transport (FIRST)

Date du début: 1 déc. 2010, Date de fin: 30 nov. 2014,

FIRST will deliver key enabling technologies for combustion emission reduction by developing improved design tools and techniques for modelling and controlling fuel sprays and soot.Aviation’s environmental impact must be reduced to allow sustainable growth to benefit European industry and society. This is captured in ACARE’s 2020 goals of reducing CO2 by 50%, NOx by 80% and in SRA1/2 proposed redu ...
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 22

 TERMINÉ 

Engine Representative Internal Cooling Knowledge and Applications (ERICKA)

Date du début: 1 juil. 2009, Date de fin: 30 juin 2014,

"The goal of ERICKA is to directly contribute to reductions in aircraft engine fuel consumption with a targeted contribution of 1% reduction in SFC relative to engines currently in service. The fuel efficiency of a jet engine used for aircraft propulsion is dependent on the performance of many key engine components. One of the most important is the turbine whose efficiency has a large influence ...
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 20

 TERMINÉ 

Engine LUBrication SYStem technologies (ELUBSYS)

Date du début: 1 juin 2009, Date de fin: 30 nov. 2012,

"In aeronautics, gas turbine engines are equipped with lubrication systems whose function is to cool and lubricate the highly loaded rolling bearings and gearboxes. Current lubrication systems are based on architectures and technologies that have not much evolved for the last 30 years and that, despite advances made on components, have reached their technological limit. Future aero-engine requirem ...
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