16 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Validation of improved turbomachinery noise prediction models and development of novel design methods for fan stages with reduced broadband noise (TurboNoiseBB)
Date du début: 1 sept. 2016, Date de fin: 29 févr. 2020,
TurboNoiseBB aims to deliver reliable prediction methodologies and noise reduction technologies in order to allow European Aerospace industries:• to design low-noise aircraft to meet society’s needs for more environmentally friendly air transport• to win global leadership for European aeronautics with a competitive supply chain.The project is focusing on fan broadband (BB) noise sources and will o ...
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15
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TERMINÉ
ENgineering COMPASS (ENCOMPASS)
Date du début: 1 oct. 2016, Date de fin: 30 sept. 2019,
... reductions in production costs, materials wastage, and over-processing. This will lead to higher economic and environmental sustainability of manufacturing, and re-inforce the EU’s position in industrial leadership in laser based AM.
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11
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TERMINÉ
Efficient Manufacturing for Aerospace Components USing Additive Manufacturing, Net Shape HIP and Investment Casting (EMUSIC)
Date du début: 1 avr. 2016, Date de fin: 31 mars 2019,
This proposal is in response to the call for International Cooperation in Aeronautics with China, MG-1.10-2015 under Horizon 2020 “Enhanced Additive Manufacturing of Metal Components and Resource Efficient Manufacturing Processes for Aerospace Applications”. The objectives are to develop the manufacturing processes identified in the call: (i) Additive manufacturing (AM); (ii) Near Net Shape Hot I ...
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12
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TERMINÉ
Engine Module Validators (ENOVAL)
Date du début: 1 oct. 2013, Date de fin: 30 sept. 2017,
...BREAK for system technologies for enabling ultra high OPR engines, and OPENAIR for noise reduction technologies. Finally, ENOVAL will prepare the way towards maturing the technology and preparing industrialisation in coordination with past and existing aero-engine initiatives in Europe at FP7 and national levels.
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37
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TERMINÉ
Low Emissions Core-Engine Technologies (LEMCOTEC)
Date du début: 1 oct. 2011, Date de fin: 30 juin 2017,
The main objective of the LEMCOTEC project will be the improvement of core-engine thermal efficiency by increasing the overall pressure ratio (OPR) to up to 70 leading to a further reduction of CO2. Since NOx increases with OPR, combustion technologies have to be further developed, at the same time, to at least compensate for this effect. The project will attain and exceed the ACARE targets for 20 ...
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39
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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
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TERMINÉ
Full Aero-thermal Combustor-Turbine interactiOn Research (FACTOR)
Date du début: 1 déc. 2010, Date de fin: 30 nov. 2016,
To achieve lower Specific Fuel Consumption (SFC) and CO2/NOx emissions, modern turbomachineries operate at high velocities and high temperature conditions. The lack of confidence in the prediction of combustor-turbine interactions leads to apply extra safety margins on components design. Therefore, the understanding of combustor-turbine flow field interactions is mandatory to preserve High Pressur ...
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24
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
Development of Aero Engine Component Manufacture using Laser Additive Manufacturing (MERLIN)
Date du début: 1 janv. 2011, Date de fin: 31 déc. 2014,
The concept of the MERLIN project is to reduce the environmental impact of air transport using Additive Manufacturing (AM) techniques in the manufacture of civil aero engines. MERLIN will develop AM techniques, at the level 1 stage, to allow environmental benefits including near 100% material utilisation, current buy to fly ratios result in massive amounts of waste, no toxic chemical usage and no ...
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16
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TERMINÉ
OPtimisation for low Environmental Noise impact AIRcraft (OPENAIR)
Date du début: 1 avr. 2009, Date de fin: 30 sept. 2014,
Reducing noise from aircraft operations perceived by airport neighbouring communities is a major challenge facing the aircraft manufacturing industry, social society and the air transport business. By adopting a whole aircraft approach based on the latest developments in active / adaptive technologies, flow control techniques and advances in computational aero-acoustics applied to the major causes ...
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51
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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
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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
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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20
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TERMINÉ
Adaptive Control of Manufacturing Processes for a New Generation of Jet Engine Components (ACCENT)
Date du début: 1 juil. 2008, Date de fin: 31 mai 2012,
"ACCENT addresses the relevance to the call 7.1: “Aeronautics and Air Transport” by “Improving Cost efficiency” and quality of safety critical aircraft engine components. The manufacture of safety critical rotating components in modern aero engines is by nature very conservative. In order to achieve the required engine performance, thermal and mechanical stresses are pushed to the maximum, which i ...
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14
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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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