Plus de 40 projets européens trouvés
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TERMINÉ
Surface Heat Exchangers For Aero Engines 2 (SHEFAE 2)
Date du début: 1 févr. 2016, Date de fin: 31 janv. 2021,
...; High efficiency Fuel Oil Heat Exchanger; High reliability Modulating Oil Bypass Valve that is integrated within the Fuel Oil Heat Exchanger. The heat exchanger systems will be tested on the rig and Rolls-Royce demonstrator engines to validate their performance and structural capabilities. The integration of the high length to depth ratio Surface Air Cooled Oil Coolers on the engine will require ...
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3
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TERMINÉ
HOLIstic optimisation of SHIP design and operation for life cycle (HOLISHIP)
Date du début: 1 sept. 2016, Date de fin: 31 août 2020,
Most maritime products are typically associated with large investments and are seldom built in large series. Where other modes of transport benefit from the economy of series production, this is not the case for maritime products which are typically designed to refined customer requirements increasingly determined by the need for high efficiency, flexibility and low environmental impact at a compe ...
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39
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TERMINÉ
Soot Processes and Radiation in Aeronautical inNOvative combustors (SOPRANO)
Date du début: 1 sept. 2016, Date de fin: 31 août 2020,
For decades, most of the aviation research activities have been focused on the reduction of noise and NOx and CO2 emissions. However, emissions from aircraft gas turbine engines of non-volatile PM, consisting primarily of soot particles, are of international concern today. Despite the lack of knowledge toward soot formation processes and characterization in terms of mass and size, engine manufactu ...
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18
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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,
The ENCOMPASS project principally aims to create a fully digital integrated design decision support (IDDS) system to cover the whole manufacturing chain for a laser powder bed fusion (L-PBF) process encompassing all individual processes within in. The ENCOMPASS concept takes a comprehensive view of the L-PBF process chain through synergising and optimising the key stages. The integration at digita ...
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11
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TERMINÉ
EXTREME Dynamic Loading - Pushing the Boundaries of Aerospace Composite Material Structures (EXTREME)
Date du début: 1 sept. 2015, Date de fin: 31 août 2019,
The European industry is currently a world leader in aviation and to maintain its leading position and competitiveness in the dynamic global market, Europe’s industry must develop quickly and efficiently high quality products by meeting time-critical market demands and customers’ needs. Industrial competition is becoming fiercer not only from established regions, such as the USA, but from new eme ...
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14
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TERMINÉ
Low Energy And Near to zero emissions Ships (LeanShips)
Date du début: 1 mai 2015, Date de fin: 30 avr. 2019,
The specific challenge for waterborne transport call MG4.1 is, “To support developments that make new and existing vessels…more efficient and less polluting”. A sound way to support developments is, to demonstrate solutions that are sufficiently close to market so that ship owners will consider these in their future investment plans. Following this reasoning LeanShips will execute 8 demonstration ...
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49
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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
Industrial optimal design using adjoint CFD (IODA)
Date du début: 1 janv. 2015, Date de fin: 31 déc. 2018,
Adjoint-based methods have become the most interesting approach in numerical optimisation using Computational Fluid Dynamics (CFD) due to their low computational cost compared to other approaches. The development of adjoint solvers has seen significant research interest, and a number of EC projects have been funded on adjoint-based optimisation. In particular, partners of this proposal are member ...
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10
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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
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TERMINÉ
Real-time dynamic control system for laser welding (RADICLE)
Date du début: 1 févr. 2015, Date de fin: 31 janv. 2018,
...r applications. The control 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 a ...
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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,
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
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TERMINÉ
JEt noise of high bypass RatiO eNgine: Installation, advanced Modelling and mitigatiOn (JERONIMO)
Date du début: 1 nov. 2012, Date de fin: 31 août 2017,
The central goal of JERONIMO is the understanding of the physical mechanisms of ultrahigh bypass ratio (UHBR) engines with a bypass ratio (BPR) larger than 12 and the related installed jet noise with potential jet-wing interaction. The aim is to reduce uncertainties in jet noise characterisation of this novel installation configuration by wind tunnel tests and predictions and being able to derive ...
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13
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TERMINÉ
Observation Platform for Technological and Institutional Consolidation of research in Safety (OPTICS)
Date du début: 1 sept. 2013, Date de fin: 31 août 2017,
The proposed coordination action OPTICS will provide oversight of progress in research and innovation aiming to improve the safety and security of aviation in accordance with Flightpath 2050 challenges and goals, exploiting as far as possible the identified metrics, achievements, main topic areas and broad industry knowledge and expertise base established in the development industry's SRIA.OPTICS ...
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10
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TERMINÉ
FORUM on Aviation and Emissions (FORUM-AE)
Date du début: 1 juil. 2013, Date de fin: 30 juin 2017,
The FORUM-AE coordination action will create a technical specialists european network with all relevant competencies, including academic and industrial partners, linked to key environmental technical issues on aviation emissions.It will address equitably three complementary aspects: environmental impacts (air quality and climate change), technical and technological mitigation solutions (aircraft, ...
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13
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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
Work and cultural mobility programme with ZF
Date du début: 1 juin 2015, Date de fin: 31 mai 2017,
Our project is to place 5 engineering advanced apprentices from the UK with ZF in Germany. ZF is a vehicle industry company compared to Rolls-Royce which produces aero engines. The skills, knowledge and experience the apprentices will gain from working in both companies will be invaluable and will broaden their skills base. The project in ZF will allow our apprentices to learn specific skills t ...
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2
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TERMINÉ
Joint Operation for Ultra Low Emission Shipping (JOULES)
Date du début: 1 juin 2013, Date de fin: 31 mai 2017,
Reducing emissions from shipping has increasingly become a challenge over the last years, both as a counter measure against global climate change and to protect local environments and population from waste, gas emissions and noise.This challenge has been documented both in policy papers, like the Europe 2020 initiative or the Transport White Paper, and in rules and regulations issued by IMO as wel ...
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44
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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
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TERMINÉ
Adjoint-based optimisation of industrial and unsteady flows (AboutFlow)
Date du début: 1 nov. 2012, Date de fin: 31 oct. 2016,
Adjoint-based methods have become the most interesting approach in CFD optimisation due to their low computational cost compared to other approaches. The development of adjoint solvers has seen significant research interest, and a number of EC projects have been funded on adjoint-based optimisation. In particular, partners of this proposal are members of the EC FP7 project FlowHead which develops ...
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9
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TERMINÉ
Aerospace Multidisciplinarity Enabling DEsign Optimisation (AMEDEO)
Date du début: 1 oct. 2012, Date de fin: 30 sept. 2016,
"AMEDEO is a multi-disciplinary design optimisation (MDO) research training network designed to provide outstanding leadership career development for talented young researchers. Network training incorporates advanced multi-disciplinary optimisation, high fidelity simulation tools and techniques for resolving complex engineering design problems in the aerospace industry. It is complemented by a com ...
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12
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TERMINÉ
MESA - Maritime Europe Strategy Action - FOSTER Waterborne (MESA)
Date du début: 1 sept. 2013, Date de fin: 31 août 2016,
Maritime Europe Strategy Action (MESA – FOSTER WATERBORNE), main strategic objective (in line with WATERBORNE-TP) is to strengthen the effectiveness of the research and innovation capacities of the European maritime industry, by:- Optimization of the European maritime RDI strategies- Improvement of the stakeholders network, of the dissemination, of the use of the research results, and increasing t ...
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32
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TERMINÉ
Accelerated Metallurgy - the accelerated discovery of alloy formulations using combinatorial principles (AccMet)
Date du début: 15 juin 2011, Date de fin: 14 juin 2016,
"The core concept of Accelerated Metallurgy is to deliver an integrated pilot-scale facility for the combinatorial synthesis and testing of many thousands of unexplored alloy formulations. This facility would be the first of its kind in the world and would represent a significant advance for metallurgy. The novel technology that enables this HTT facility is based on automated, direct laser deposit ...
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34
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TERMINÉ
Intelligent Design Methodologies for Low Pollutant Combustors for Aero-Engines (IMPACT-AE)
Date du début: 1 nov. 2011, Date de fin: 31 mai 2016,
The environmental benefits of low emissions lean burn technology in reducing NOx emissions up to 80% will only be effective when these are deployed to a large range of new aero-engine applications. While integrating and developing low emission combustion design rules, IMPACT-AE will deliver novel combustor design methodologies for advanced engine architectures and thermodynamic cycles. It will sup ...
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21
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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
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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
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TERMINÉ
Miniaturised Robotic systems for holistic in-situ Repair and maintenance works in restrained and hazardous environments (MiRoR)
Date du début: 1 févr. 2012, Date de fin: 31 janv. 2016,
MiRoR aims to develop a fundamentally novel concept of a Miniaturised Robotic Machine (Mini-RoboMach) system, that equipped with intelligence-driven and autonomous abilities, will be demonstrated for holistic in-situ repair and maintenance of large and/or intricate installations.This will be done via the following research steps:-Develop a novel concept of Mini-RoboMach, with unique complementary ...
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8
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TERMINÉ
Transition Location Effect on Shock Wave Boundary Layer Interaction (TFAST)
Date du début: 1 févr. 2012, Date de fin: 31 janv. 2016,
Vision-2020, whose objectives include the reduction of emissions and a more effective transport systems, puts severe demands on aircraft velocity and weight. These require an increased load on wings and aero-engine components. The greening of air transport systems means a reduction of drag and losses, which can be obtained by keeping laminar boundary layers on external and internal airplane parts ...
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16
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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
Graphene based thermoplastic masterbatches for conventional and additive manufacturing processes (NANOMASTER)
Date du début: 1 déc. 2011, Date de fin: 30 nov. 2015,
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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14
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TERMINÉ
Aviation Noise Research Network and Coordination (X-NOISE EV)
Date du début: 1 déc. 2010, Date de fin: 30 nov. 2015,
The X-NOISE EV Coordination Action, through its network structure and comprehensive workplan involving experts groups, scientific workshops, international cooperation seminars and a common information system, addresses the noise challenges faced by Aviation. To this end, it will more specifically:- Evaluate EU-funded projects results and assess their contribution to the state-of-the-art.- Formulat ...
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28
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TERMINÉ
Suppression Of underwater Noise Induced by Cavitation (SONIC)
Date du début: 1 oct. 2012, Date de fin: 30 sept. 2015,
The aim of the SONIC project is to develop tools to investigate and mitigate the effects of underwater noise generated by shipping, both in terms of the footprint of an individual ship (a “noise footprint”) and of the spatial distribution of sound from a large number of ships contribution to the sound (a “noise map”). The project`s first objective is to enhance the understanding of noise generated ...
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13
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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,
...process NDT development.• In-process geometrical validation.• High specification materials process development.The MERLIN consortium comprises six world leading aero engine manufacturers, Rolls-Royce is the coordinator, six renowned RTD providers and two intelligent SME’s. Impacts will include the development of high value, disruptive AM technologies capable of step changes in performance which wi ...
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16
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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
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TERMINÉ
Cost Competitive Component integration for StatiOnary Fuel Cell power (C3SOFC)
Date du début: 1 oct. 2011, Date de fin: 30 sept. 2014,
"Solid oxide fuel cells for stationary power have been researched since the late 1980s as potentially high efficiency and environmentally friendly means to generate electricity. Since that time substantial progress has been made however obstacles remain to reach industrial exploitation.For end users, the cost of electricity not only the cost of the fuel cell is of primary concern. This cost is dri ...
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6
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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
Fuel Control System Sensors and Effectors (CASE)
Date du début: 4 janv. 2011, Date de fin: 3 juil. 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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3
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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
Partnership for Numerical Acoustic Simulation of aero-engines (PARNAS)
Date du début: 1 juin 2010, Date de fin: 31 mai 2014,
The PARNAS project (1) focuses on an important industrial application (reduction of aircraft engine noise using optimized acoustic liners designed), (2) investigates fundamental mathematical aspects of the related simulation techniques (FEM, DGM, PUM), (3) builds upon three successful FP5 and FP6 research projects where some technological components have been developed and where the partners have ...
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