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17 projets européens trouvés

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 TERMINÉ 

Increased Safety and robust certification for ditching of aircrafts and helicopters (SARAH)

Date du début: 1 oct. 2016, Date de fin: 30 sept. 2019,

SARAH is concerned with establishing novel holistic, simulation-based approaches to the analysis of aircraft ditching. It is build up from a consortium of experts from OEM industries, experienced suppliers of simulation technologies, established research institutions and representatives of the certification authorities. Results of SARAH are expected to support a performance-based regulation and ce...
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 12

 TERMINÉ 

PROJET PILOTE FRANCO ALLEMAND POUR UN ERASMUS DES APPRENTIS

Date du début: 1 juin 2016, Date de fin: 31 mai 2018,

Traduction non réalisée par manque de temps.
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 2

 TERMINÉ 

Coordination Action Pro “Production, Avionics, Design” on Cost-efficiency in Aeronautics (CAPPADOCIA)

Date du début: 1 oct. 2013, Date de fin: 30 sept. 2017,

The Advisory Council for Aeronautics Research in Europe is the European Technology Platform for Aeronautics and Air Transport (AAT) that provides guidance for the future of the European aeronautics research. ACARE previous roadmap, the Strategic Research Agenda, was highly of inspiration for EC work programme elaboration on Aeronautics and Aviation. In 2011 the European Commission published the Fl...
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 10

 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 

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 

Cost Effective Reinforcement of Fastener Areas in Composites (CERFAC)

Date du début: 1 oct. 2010, Date de fin: 31 déc. 2014,

"CERFAC’s major challenge is the design and manufacturing of strong and cost-efficient joints for high performance CFRP aero-structures.In particular, transfer of distributed loading along rivets lines in the assembly of flat or curved thin-walled stiffened panels, and introduction of concentrated loads for connecting lugs with thicker laminates are special & frequent problems. Hence, CERFAC focus...
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 15

 TERMINÉ 

Heavy Payload Helicoper for Last Mile Rescue (HELI4RESCUE)

Date du début: 1 août 2012, Date de fin: 30 juin 2014,

The proposal addresses the possibility for Civil Security operators to use large air transport systems for deploying heavy loads on crisis sites (last mile). It investigates in particular the deployment in civil missions of systems which are now targeted only for military use. A broad range of European Civil Security users will be involved in developing appropriate requirements for offering transp...
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 5

 TERMINÉ 

HIRF Synthetic Environment (HIRF SE)

Date du début: 1 déc. 2008, Date de fin: 31 mai 2013,

"The HIRF SE research project has the goal of providing the aeronautics industry with a framework which can be used during the development phase to mitigate the EM aspects. In addition it will provide a considerable reduction in the certification/qualification tests required on air vehicle. The HIRF SE main objectives can be summarized by the two followings items: • Full validated and integrated s...
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 45

 TERMINÉ 

Development of technology building blocks For structural health monitoring sensing devices in aeronautics (TRIADE)

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

"NEEDS and CONCEPTS: Structural Health Monitoring (SHM) will be very important for Aeronautics. A study from Goodrich stated: "Structural Health Monitoring shows a great potential in terms of cost savings coming from the benefits it would have on inspections which are currently about 25% of the Life Cycle Cost of an airline". Some applications are intended to explore the “out-of-flight domain” con...
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 16

 TERMINÉ 

Industrialization of Manufacturing Technologies for Composite Profiles for Aerospace Applications (IMac-Pro)

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

Main aim of the project is the development of a complete, integrated process chain for the cost effective serial production of various aerospace CFRP stiffener profiles. The production is foreseen in the two steps: Preform manufacturing and infiltration / curing. The project will focus on complex profile geometries with variable cross sections, single or multiple curvature and integrated load int...
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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 

Advanced Turbulence Simulation for Aerodynamic Application Challenges (ATAAC)

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

"The ATAAC project aims at improvements to Computational Fluid Dynamics (CFD) methods for aerodynamic flows used in today’s aeronautical industry. The accuracy of these is limited by insufficient capabilities of the turbulence modelling / simulation approaches available, especially at the high Reynolds numbers typical of real-life flows. As LES will not be affordable for such flows in the next 4 d...
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 22

 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

 TERMINÉ 

Strengthening the industries’ competitive position by the development of a logistical and technological system for “spare parts” that is based on on-demand production (DirectSpare)

Date du début: 1 févr. 2009, Date de fin: 31 janv. 2012,

The proposal offers a solution for the growing quantity of product types on the market requiring enormous warehouses to keep stock for spare parts, with corresponding high costs and complex logistics. This emerging problem is caused by the continuously decreasing product life time, decreasing time-to-market and increasing regulatory affairs. A solution is foreseen using Rapid Manufacturing (RM) ...
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 17

 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

 TERMINÉ 

AIRCRAFT INTEGRATED STRUCTURAL HEALTH ASSESSMENT II (AISHA II)

Date du début: 1 mai 2008, Date de fin: 31 oct. 2011,

"The safe use of complex engineering structures such as aircrafts can only be guaranteed when efficient means of damage assessment are in place. Whereas the design of civil structures is nowadays based on a damage tolerance approach and time based inspection cycles, it is envisaged that the large cost associated with this approach can be drastically reduced by switching to a condition based mainte...
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 14