Rechercher des projets européens

24 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

 TERMINÉ 

Additive Manufacturing Optimization and Simulation Platform for repairing and re-manufacturing of aerospace components (AMOS)

Date du début: 1 févr. 2016, Date de fin: 31 janv. 2020,

... will be investigated to establish an across-the-board comparative study. The data collected through this comprehensive comparative study will be extremely valuable for the OEMs of this project (i.e. GKN, PWC, and HDI) to understand the pros and cons of these DED systems and will help them to select suitable repair and re-manufacturing strategies. The tests conducted in this research are also extr ...
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 4

 TERMINÉ 

Production harmonizEd Reconfiguration of Flexible Robots and Machinery (PERFoRM)

Date du début: 1 oct. 2015, Date de fin: 30 sept. 2018,

PERFoRM - Production harmonizEd Reconfiguration of Flexible Robots and Machinery aims to the conceptual transformation of existing Production Systems towards plug&produce production systems in order to achieve a flexible manufacturing environments based on rapid and seamless reconfiguration of machinery and robots as response to operational or business events.These objectives require research acti ...
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 18

 TERMINÉ 

Ultra Low emission Technology Innovations for Mid-century Aircraft Turbine Engines (ULTIMATE)

Date du début: 1 sept. 2015, Date de fin: 31 août 2018,

With the ULTIMATE project five experienced research groups and four major European engine manufacturers will develop innovative propulsion systems to fulfill the SRIA 2050 key challenges. One of the most challenging targets is the 75% reduction in energy consumption and CO2-emissions. Technologies currently at TRL 3-5, cannot achieve this aim. It is estimated that around a 30% reduction must come ...
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 11

 TERMINÉ 

Real-time dynamic control system for laser welding (RADICLE)

Date du début: 1 févr. 2015, Date de fin: 31 janv. 2018,

...ontrol system will include pre- and post-welding measurement as well as in-process monitoring, control and fault prevention / fixing. The project has 4 large, end-user partners - Rolls-Royce, Alstom, GKN and CRF (FIAT) therefore the impact of RADICLE is expected to be very large.The overall impacts of successful implementation of the RADICLE technology through our consortium and the wider welding ...
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 12

 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

 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

 TERMINÉ 

Efficient ice protection Systems and simulation Techniques Of ice Release on propulsive systeMs (STORM)

Date du début: 1 oct. 2013, Date de fin: 31 mars 2017,

Icing conditions are one of the most severe for aircraft and engines as experienced in the certification process and in-service events. Certification tests are never simple because icing phenomena is a very complex domain and designers have access to a very low level of prediction capability compare to other fields, mainly relying on a very fragmented knowledge based on empirical past experience. ...
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 15

 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 

Self-Healing Thermal Barrier Coatings (SAMBA)

Date du début: 1 mars 2013, Date de fin: 28 févr. 2017,

"This project deals with the creation of a new, unique self-healing thermal barrier coating (TBC) for turbines and other thermally loaded structures in order to realize a significant extension of the lifetime of critical high-temperature components. The concept is based on novel Al2O3 coated Mo-Si particles embedded in the TBC layer, typically consisting of yttria-stabilised zirconia. As the curre ...
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 9

 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

 TERMINÉ 

Thermal Overall Integrated Conception of Aircraft (TOICA)

Date du début: 1 sept. 2013, Date de fin: 30 sept. 2016,

Thermal behaviour of aircraft has recently become a crucial subject due to many factors: increasing number of complex systems required by modern, more electric, commercial aircraft, the introduction of hotter engines with higher by-pass ratios, the increased use of composite material in aircraft structures, or the confinement of highly dissipative equipment and systems in smaller areas to earn spa ...
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 34

 TERMINÉ 

LOw COst Manufacturing and Assembly of Composite and Hybrid Structures (LOCOMACHS)

Date du début: 1 sept. 2012, Date de fin: 31 août 2016,

The continued use of composite materials in the aerospace industry has been addressed in several past research projects which have focused on new design solutions and composite manufacturing processes. However an area which has been given much less attention up until now is how to achieve a time and cost effective lean assembly production system. The current airframe assembly process of composite ...
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 33

 TERMINÉ 

Sensors Towards Advanced Monitoring and Control of Gas Turbine Engines (STARGATE)

Date du début: 1 nov. 2012, Date de fin: 29 févr. 2016,

The headline objective of this project is to develop a suite of advanced sensors, instrumentation and related systems in order to contribute to the development of the next generation of green and efficient gas turbine engines (AAT.2012.1.1-3&4).Sensors are a vital enabling technology for gas turbines and are critical to validation of design tools, new products, engine control, and health monitorin ...
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 16

 TERMINÉ 

Surface Heat Exchangers for Aero-Engines (SHEFAE)

Date du début: 1 févr. 2013, Date de fin: 31 janv. 2016,

"The Project aim is to develop and demonstrate an advanced structural surface cooler mounted in an appropriate core fairing composite structure. Currently surface coolers are an integral feature of advanced turbofan engine designs. They contribute to achieving the best engine performance by maintaining oil and fuel temperatures within defined limits and by virtue of their mounting on the inside of ...
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 6

 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

 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

 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

 TERMINÉ 

imProved reliabIlity inspeCtion of Aeronautic structure through Simulation Supported POD (PICASSO)

Date du début: 1 juil. 2009, Date de fin: 31 déc. 2012,

"With aging engines and the increase of air traffic in the next 20 years, a central challenge in the aeronautical industry will concern the increase of the efficiency of maintenance which still represents around 20% of an operator’s indirect operating costs. This challenge is particularly important for metallic parts within the engine aircraft industry, because of the criticity of rotative compone ...
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 14

 TERMINÉ 

Advanced flexible automation cell (FLEXA)

Date du début: 1 juin 2008, Date de fin: 30 nov. 2012,

"Truly flexible automation of -low volume, -high value per part components, -managing quality assurance aspect throughout the value chain is a key research area for the manufacturing and production community in Europe. The FLEXA project has identified key elements for delivering advancement in this area. The key areas of research will be; cell design solutions in line with product design decisions ...
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 17

 TERMINÉ 

Collaborative & Robust Engineering using Simulation Capability Enabling Next Design Optimisation (CRESCENDO)

Date du début: 1 mai 2009, Date de fin: 31 oct. 2012,

"The IMG4 project CRESCENDO addresses the Vision 2020 objectives for the aeronautical industry by contributing significantly to the fulfilment of three specific targets of the aeronautical industry’s Strategic Research Agenda. CRESCENDO will develop the foundations for the Behavioural Digital Aircraft (BDA), taking experience and results from VIVACE, and integrating these into a federative system ...
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 59

 TERMINÉ 

Adaptive and Passive Flow Control for Fan Broadband Noise Reduction (FLOCON)

Date du début: 1 sept. 2008, Date de fin: 31 août 2012,

"Air traffic is predicted to grow by 5% per year in the short and medium term. Technology ad-vances are required to achieve this growth without unacceptable levels of noise. FLOCON addresses this issue by reducing fan noise at source through the development of innovative concepts based on flow control technologies. FLOCON is aimed primarily at reducing fan broadband noise. This is one of the most ...
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 17

 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

 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