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27 projets européens trouvés

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 TERMINÉ 

High-Speed Experimental Fly Vehicles - International (HEXAFLY-INT)

Date du début: 1 avr. 2014, Date de fin: 31 mars 2019,

The HEXAFLY-INT project aims to flight test an experimental vehicle above Mach 7 to verify its potential for a high aerodynamic efficiency during a free-flight while guaranteeing a large internal volume. The feasibility for a 3m long vehicle was demonstrated during the European L0 precursor project HEXAFLY. Its realization will now be enabled on an international scale underlining the need for glob ...
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 11

 TERMINÉ 

"""2nd Generation Active Wing“ – Active Flow- Loads & Noise control on next generation wing" (AFLONEXT)

Date du début: 1 juin 2013, Date de fin: 31 mai 2018,

AFLoNext is a four year EC L2 project with the objective of proving and maturing highly promising flow control technologies for novel aircraft configurations to achieve a quantum leap in improving aircraft’s performance and thus reducing the environmental footprint. The project consortium is composed by forty European partners from fifteen countries. The work has been broken down into seven work p ...
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 41

 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

 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 

Air Transport Network – Next Generation (AIRTN-NEXTGEN)

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

The action will continue the network established under previous AirTN projects enlarging it to create a platform of networking and communication between national organisations and governmental institutions supporting research and innovation in the EU Member States and Associated Countries to the EU Framework Programme in the field of Aviation (e.g. Aeronautics and Air Transport - AAT).The successf ...
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 10

 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

 TERMINÉ 

Uncertainty Management for Robust Industrial Design in Aeronautics (UMRIDA)

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

Virtual prototyping (VP) is a key technology for environmental friendly and cost effective design in the aircraft industry. However, the underlying analysis and simulation tools (for loads, stresses, emissions, noise), are currently applied with a unique set of input data and model variables, although realistic operating conditions are a superposition of numerous uncertainties under which the indu ...
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 22

 TERMINÉ 

Efficient Systems and Propulsion for Small Aircraft (ESPOSA)

Date du début: 1 oct. 2011, Date de fin: 30 juin 2016,

The ESPOSA project will develop and integrate novel design and manufacture technologies for a range of small gas turbine engines up to approx. 1000 kW to provide aircraft manufacturers with better choice of modern propulsion units. It will also deal with engine related systems which contribute to the overall propulsion unit efficiency, safety and pilot workload reduction. Through the newly develop ...
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 45

 TERMINÉ 

GReener Aeronautics International Networking-2 (GRAIN 2)

Date du début: 1 oct. 2013, Date de fin: 31 mai 2016,

As mentioned in the Executive Summary of the Strategic Research & Innovation Agenda, Aviation has an important role to play in reducing greenhouse gas emissions as well as noise and local air quality issues. The continuous increase of air passenger transport generates an increasing use of hydrocarbon fuel with excessive emission of CO2 and NOX (greenhouse gases, pollutants and noise). It is well k ...
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 25

 TERMINÉ 

ACTUATION 2015: Modular Electro Mechanical Actuators for ACARE 2020 Aircraft and Helicopters (ACTUATION2015)

Date du début: 1 nov. 2011, Date de fin: 30 avr. 2016,

The All-Electric Aircraft is a major target for the next generation of aircraft to lower consumption of non-propulsive power and thus fuel burn. To eliminate hydraulic circuits, pumps and reservoirs, Electro Mechanical Actuators (EMA) are mandatory but now need to meet cost, reliability and weight requirements from the airframers.ACTUATION2015 aims to develop and validate a common set of standard ...
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 56

 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

 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 

Integrated Ground and on-Board system for Support of the Aircraft Safe Take-off and Landing (GABRIEL)

Date du début: 1 sept. 2011, Date de fin: 31 août 2014,

"The future air transport system will be confronted with new challenges: it must be safer, greener and more effective than the current system. There will be more global industrial competition and fossil fuel reserves will diminish leading to increased fuel prices. New radical ideas, methods and technologies are needed to respond to these challenges and to keep Europe world leader in aviation. One ...
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 12

 TERMINÉ 

AEROdynamic Surfaces by advanced MUltifunctional COatings (AEROMUCO)

Date du début: 1 janv. 2011, Date de fin: 30 avr. 2014,

"The main objective of the AEROMUCO project is to develop and evaluate a number of alternative – and highly innovative – active and passive multi-functional surface protection systems for future generation of aircraft, leading to a significant improvement in fuel efficiency and a reduction in CO2 and NOx emissions. Two technological routes to achieve this goal will be explored:• The reduction of t ...
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 12

 TERMINÉ 

cOoperation with Russia in the field of advanced engIne NOise COntrol based on plasma actuators (ORINOCO)

Date du début: 1 août 2010, Date de fin: 31 janv. 2014,

"In the domain of civilian aeronautics, the increasing noise restrictions around airports are a challenging problem for aircraft and engine manufacturers. Despite significant progresses since the definition of ACARE objectives, jet noise remains the main source of noise for an aircraft at take-off and many works have been dedicated to its understanding and its reduction. First generation of noise ...
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 13

 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

 TERMINÉ 

Air Cargo Technology Road Map (CargoMap)

Date du début: 1 oct. 2011, Date de fin: 31 déc. 2013,

The Air Cargo technology Roadmap proposal focuses on the future role of air freight and the definition of a technology roadmap for future cargo aircraft responding to end user requirements and environmental needs. In order to improve seamless flow of goods, Inter-and Co-modality approaches will be considered within the SESAR operational concept.Main issues of the CARGO Map (CSA-SA) proposal are:• ...
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 7

 TERMINÉ 

4 Dimension Contracts - Guidance and Control (4DCO-GC)

Date du début: 1 nov. 2010, Date de fin: 31 oct. 2013,

"The 4DCo-GC project aims at exploring the concept of ""4D Contract guidance and control of the aircraft"" as a step change in air transport operations by providing a more radical and environmentally efficient solution for the management of the airspace. Scientific objectives of 4DCo-GC are to:- model 4D contract concepts (strategic, tactical and emergency levels)- develop algorithms (strategic, t ...
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 13

 TERMINÉ 

Canadian Networking Aeronautics Project for Europe (CANNAPE)

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

"The proposal creates a platform for enhancing aeronautics and air transport research and development cooperation between the EU and Canada, and to explore the potential for and to promote the participation of Canadian stakeholders with their European counterparts in common activities. The objectives for CANNAPE are:• To explore the potential for enhancing EU and Canadian cooperation through anal ...
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 20

 TERMINÉ 

"Design, Simulation and Flight Reynolds Number Testing for Advanced High-Lift Solutions" (DESIREH)

Date du début: 1 mars 2009, Date de fin: 30 juin 2013,

"DeSiReH focus on both, the numerical design tools and the experimental measurement techniques for cryogenic conditions, with the objective to improve the industrial design process for laminar wings in terms of product quality, efficiency, and development cost reduction. The work focuses on the design of high lift devices. DeSiReH addresses the following quantified objectives which will make a sig ...
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 21

 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 

Generic Linking of Finite Element based Models (glFEM)

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

"AREA 7.1.4.1 aims to ensure cost efficiency in air transport focussing on reduction of aircraft acquisition costs. Innovative solutions and technologies must result in lower lead time and costs of the aircraft from design to production, with a more competitive supply chain. The current proposal relates to topic AAT2008.4.1.1: ""Design Systems and Tools"". For this topic it is stated in the Work ...
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 8

 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

 TERMINÉ 

Smart High Lift Devices for Next Generation Wings (SADE)

Date du début: 1 mai 2008, Date de fin: 31 oct. 2012,

"All aerodynamic concepts for significant reduction of drag such as laminarisation require slim high-aspect-ratio wings. However, state-of-the-art high lift systems will suffer from the reduced construction space and do not cope with the required surface quality. Thus, SADE (Smart High Lift Devices for Next Generation Wings) develops suitable 'morphing' high lift devices: The seamless 'smart leadi ...
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 13

 TERMINÉ 

Technologies for Safe and Controlled Martian Entry (SACOMAR)

Date du début: 1 janv. 2011, Date de fin: 30 juin 2012,

"The main objective of the study is the experimental and numerical study of gas surface interaction phenomena in the high enthalpy flow field behind the bow shock in front of a model at Martian entry flow conditions. The improvement of physical modelling using experimental data and its implementation into the CFD codes is essential to understand and interpret the physical processes. At the end the ...
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 8

 TERMINÉ 

EXTreme ICing Environement (EXTICE)

Date du début: 1 juin 2008, Date de fin: 31 mai 2012,

"More recent aircraft incidents and accidents have highlighted the existence of icing cloud characteristics beyond the actual certification envelope defined by the JAR/FAR Appendix C, which accounts for an icing envelope characterized by water droplet diameters up to 50 μm (so-called cloud droplet). The main concern is the presence of super-cooled large droplets (SLD) such as freezing drizzle, in ...
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 14

 TERMINÉ 

Aerodynamic loads estimation at extremes of the flight envelope (ALEF)

Date du début: 1 mai 2009, Date de fin: 30 avr. 2012,

"ALEF's objective is to enable the European aeronautical industry to create complete aerodynamic models of their aircraft based on numerical simulation approaches within the respective development processes. I.e. ALEF will kick-off a paradigm shift from greater confidence in experimentally measured loads data to greater confidence in computational results. Beyond the scope of ALEF this paradigm sh ...
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 20