8 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Engine Module Validators (ENOVAL)
Date du début: 1 oct. 2013, Date de fin: 30 sept. 2017,
The ENOVAL project will provide the next step of engine technologies to achieve and surpass the ACARE 2020 goals on the way towards Flightpath 2050. ENOVAL completes the European 7th Framework Programme (FP7) roadmap of Level 2 aero engine projects. ENOVAL will focus on the low pressure system of ultra-high by-pass ratio propulsion systems (12 < BPR < 20) in conjunction with ultra high overall pre ...
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37
Participants partenaires
TERMINÉ
INTElligent FIXtures for the manufacturing of low rigidity components (INTEFIX)
Date du début: 1 juil. 2013, Date de fin: 30 juin 2016,
In the manufacturing industry, the machining of medium and big size parts with the required and suitable precision is a challenge, especially in high added value products manufactured in small or single-unit batches made of high performance materials like in aeronautic, space or energy sectors, where conventional process engineering and test/error methods are not completely efficient.INTEFIX aims ...
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33
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TERMINÉ
Research on Core Noise Reduction (RECORD)
Date du début: 1 janv. 2013, Date de fin: 31 déc. 2015,
In order to achieve the greening of the European air transport with the deployment of low emission and low noise propulsion systems the reduction of core noise plays an important role. The ability to design low core noise aero-engines requires the development of reliable prediction tools. This development demands extensive research with dedicated experimental test cases and sophisticated numerical ...
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21
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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
Participants partenaires
TERMINÉ
Flutter-Free Turbomachinery Blades (FUTURE)
Date du début: 1 juil. 2008, Date de fin: 30 juin 2013,
"FUTURE brings together European and international well reputed centres-of-excellence in order to reach major scientific & technical objectives in striving towards flutter-free turbomachine blades. By advancing the state-of-the-art in flutter prediction capabilities and design rules, the FUTURE project will lead to benefits in terms of decreased development cost, reduced weight and fuel consumptio ...
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26
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TERMINÉ
"Knowledge for Ignition, Acoustics and Instabilities" (KIAI)
Date du début: 1 mai 2009, Date de fin: 30 avr. 2013,
"For the time being, the European engine industry does not have at its disposal methodologies adapted to predict the unsteady behaviour of low NOx combustors. Consequently and in order to be able to set up the development of low NOx technologies, KIAI will deliver reliable unstationary CFD tools which will allow a deep comprehension of unsteady phenomena. The main objective of the KIAI project is ...
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18
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TERMINÉ
valiDation of Radical Engine Architecture systeMs (DREAM)
Date du début: 1 févr. 2008, Date de fin: 31 janv. 2012,
"Since the publication of the ACARE goals, the commercial and political pressure to reduce CO2 has increased considerably. DREAM is the response of the aero-engine community to this pressure. The first major DREAM objective is to design, integrate and validate new engine concepts based on open rotor contra-rotating architectures to reduce fuel consumption and CO2 emissions 7% beyond the ACARE 2020 ...
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46
Participants partenaires
TERMINÉ
Engine and turbine combustion of bioliquids for combined heat and power production (Bioliquids-CHP)
Date du début: 1 janv. 2009, Date de fin: 31 déc. 2011,
The combustion of plant oils in diesel engines, whether or not after esterification to “biodiesel”, is possible but for the future less desirable because they are derived from food crops (first generation biofuels). Fast pyrolysis liquids derived from ligno-cellulosic materials (second generation biofuel type), are superior in terms of sustainability. Combustion in prime movers like turbines or en ...
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