12 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Towards Industrial LES/DNS in Aeronautics – Paving the Way for Future Accurate CFD (TILDA)
Date du début: 1 mai 2015, Date de fin: 30 avr. 2018,
The ability to simulate aerodynamic flows using CFD methods has progressed rapidly over the last decades and has given rise to a change in design processes in aeronautics already. But more improvement is necessary to overcome the (still) existing lack in confidence in CFD usage, based on turbulence modelling. The TILDA project will offer methods and approaches combining advanced and efficient high ...
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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
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
More Affordable Aircraft structure through eXtended, Integrated, and Mature nUmerical Sizing (MAAXIMUS)
Date du début: 1 avr. 2008, Date de fin: 30 sept. 2016,
Even though composite materials are more and more used in modern airframes, many significant improvements are still achievable. Firstly, the substitution of the assembly of many small composite parts by a single one-shot large part provides additional weight reduction. Secondly, the final assembly line process must be adapted to composite properties (lack of ductility, stiffness). Thirdly, if the ...
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60
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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
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TERMINÉ
Smart Intelligent Aircraft Structures (SARISTU)
Date du début: 1 sept. 2011, Date de fin: 31 août 2015,
The project proposal concerns the challenges posed by the physical integration of smart intelligentstructural concepts. It addresses aircraft weight and operational cost reductions as well as animprovement in the flight profile specific aerodynamic performance.This concerns material concepts enabling a conformal, controlled distortion of aerodynamicallyimportant surfaces, material concepts enablin ...
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68
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TERMINÉ
Awareness and Transfer of Innovation in composite materials (Composites)
Date du début: 6 oct. 2008, Date de fin: 30 déc. 2014,
This project aims to reinforce innovation and technology transfer amongst companies in NWE. in order to provide support and assistance throughout the period of profound industrial change linked to the arrival of composite materials. The aim is to rely on the “technological centres of excellence” and on the dynamics that they have created in their area of expertise. whilst providing a favourable cl ...
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13
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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
Industrialisation of High-Order Methods – A Top-Down Approach (IDIHOM)
Date du début: 1 oct. 2010, Date de fin: 31 mars 2014,
"The proposed IDIHOM project is motivated by the increasing demand of the European aerospace industries to advance their CFD-aided design procedure and analysis by using accurate and fast numerical methods, so-called high-order methods. They will be assessed and improved in a top-down approach by utilising industrially relevant complex test cases, so-called application challenges in the general ar ...
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21
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TERMINÉ
Long-Term Advanced Propulsion Concepts and Technologies II (LAPCAT-II)
Date du début: 1 oct. 2008, Date de fin: 31 déc. 2013,
"Lacpat II is a logical follow-up of the previous EC-project which has as objective to reduce antipodal flights to less than 2 to 4 hours. Among the several studied vehicles, only two novel aircraft for a Mach 5 and 8 flight are retained in the present proposal. Starting from the available Mach 5 vehicle and its related precooled turboramjet, assumed performance figures of different components ...
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16
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TERMINÉ
Future High-Altitude High-Speed Transport 20XX (FAST20XX)
Date du début: 1 déc. 2009, Date de fin: 30 nov. 2012,
"The current project aims at the investigation and development of technologies and steps necessary for approaches to conquer the grey zone between aeronautics and space in Europe, and thus to set the foundation of a new paradigm for transportation in the long term. The underlying concepts considered are a) a European space plane based on an airplane launch approach to advance European know how in ...
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17
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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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