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31 projets européens trouvés

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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

 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

 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 

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 

Innovative counter rotating fan system for high bypass ratio aircraft engine (COBRA)

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

The purpose of COBRA is to use technology breakthroughs to overcome the insufficient noise performance of the counter-rotating fan tested in VITAL FP6 Program. This will be achieved through exploring higher by-pass ratio (15-25) resulting in much lower blade tip speed and blades count. The designs shall comply also with higher or equal aerodynamic efficiency compare to the VITAL ouputs.COBRA is s ...
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 9

 TERMINÉ 

High Altitude Ice Crystals (HAIC)

Date du début: 1 août 2012, Date de fin: 31 janv. 2017,

Commercial aircraft have been experiencing in-service events while flying in the vicinity of deep convective clouds since at least the early 1990s. Heated probes and engines are the areas of air-craft most prone to mixed phase and glaciated icing threat. In anticipation of regulation changes regarding mixed phase and glaciated icing conditions, the HAIC project will provide the necessary Acceptabl ...
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 40

 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 

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

 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 

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

 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

 TERMINÉ 

Hybrid Silicide-Based Lightweight Components for Turbine and Energy Applications (HYSOP)

Date du début: 1 oct. 2010, Date de fin: 31 mars 2015,

"HYSOP’s goal is to develop solutions for manufacturing lightweight high temperature (HT) turbine components and to design new coating systems (protection against oxidation, water vapour and CMAS).Nb/Nb5Si3 and Si3N4/MoSi2 composites are lightweight HT materials (density < 6.5~7 and < 5.6 g/cm3, respect.) with application potential above 1300°C making them candidates for advanced aero-engine compo ...
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 11

 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 

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 

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 

Noise Impact of aircraft with Novel engine configurations in mid- to High Altitude operations (NINHA)

Date du début: 1 oct. 2010, Date de fin: 30 sept. 2013,

"The introduction of aircraft with advanced counter-rotating open rotor (CROR) powerplants will improve specific fuel consumption by 10-15% relative to equivalent turbofans. The NINHA project will assess whether noise issues away from airports (i.e. during high altitude operations) will hazard the introduction of this new generation of powerplants designed to improve fuel burn and reduce CO2 emiss ...
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 9

 TERMINÉ 

Weather hazards for aeronautics (WEZARD)

Date du début: 1 juil. 2011, Date de fin: 30 juin 2013,

"On April 14th, 2010, the eruption of the Eyjafjallajökull volcano and the accompanying cloud of volcanic ash forced most countries in northern Europe to shut their airspace, grounding more than 100,000 flights, affected an estimated 10 million travellers and had a financial impact of 5 bn US$ over a seven day period. This event revealed to what extent our society and economy rely on the availabi ...
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 13

 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 

"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

 TERMINÉ 

Community Oriented Solutions to Minimise aircraft noise Annoyance (COSMA)

Date du début: 1 juin 2009, Date de fin: 31 mars 2013,

"COSMA aims to develop engineering criteria for aircraft design and operations in order to reduce the annoyance within airport communities due to aircraft exterior noise. By today, such criteria do not exist since aircraft noise engineering has historically focused on achieving ever lower noise levels for individual events and at close distance from the runway. Within the frame of a unique approac ...
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 21

 TERMINÉ 

Tool Suite for Environmental and Economic Aviation Modelling for Policy Analysis (TEAM_Play)

Date du début: 1 déc. 2010, Date de fin: 31 mars 2013,

A large set of policy issues in the field of aviation and environment is discussed in ICAO/CAEP and on European level. Currently, the most urgent requirements are the capability of modelling noise, NOx stringencies and greenhouse gases in relation to the Kyoto protocol as well as related agreements together with their respective effects. Careful analysis of the complex interdependencies between ai ...
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 19

 TERMINÉ 

Technologies Enhancement for Clean Combustion in Aero-engines (TECC-AE)

Date du début: 1 juil. 2008, Date de fin: 31 déc. 2012,

"Due to continuous efforts through past and ongoing European projects, lean combustion by means of internally staged injectors now appears to be the promising technology for obtaining the required emission reductions compatible with a sustainable growth of aviation transport. (cf ACARE 2020) Recognising that putting into service such a technology as soon as possible is the only way to effectively ...
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 18

 TERMINÉ 

Useful PLASMa for AEROdynamic control (PLASMAERO)

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

"PLASMAERO seeks to demonstrate how surface & spark discharge plasma actuators could be used to control aircraft aerodynamic flow. This will be achieved through an enhanced understanding of their physical characteristics and an in-depth study of how they may be optimised to influence the air flow properties. The project will run for 36 months and will show the advantages and notably the ease of im ...
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 11

 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 

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

 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 

Conditions of success for R&T Open options through a Platform of communications and for Expressing Recommendation Actions to Team-up Europe and U.S (COOPERATEUS)

Date du début: 15 août 2010, Date de fin: 14 oct. 2012,

"COOPERATEUS is a European Project within the Framework Programme 7 (Research / Aeronautics and Air Transport) aiming at establishing an initial framework, data base and network, in order to facilitate and enhance the cooperation in R&T activities between the two largest world players in aeronautics, i.e. the USA and Europe. It will introduce a more structured dialogue to identify the similarities ...
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 11

 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 

Alternative Fuels and Biofuels for Aircraft Development (ALFA-BIRD)

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

"ALFA-BIRD aims at developing the use of alternative fuels in aeronautics. In a context where the price of oil is increasing and with impact of fossil fuels on climate change, the sustainable growth of the civil aviation is conditioned by the respect of the environment. In this context, using biofuels and alternative fuels in aeronautics is a great challenge, since the operational constraints (e.g ...
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 24

 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