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22 projets européens trouvés

Recherche sur 125080 projets européens

 TERMINÉ 

Multipurpose test rig for transmissions gearboxes. (MUTR)

Date du début: 1 sept. 2016, Date de fin: 30 avr. 2020,

Objective of this proposal is to design, manufacture, test and support the adaptation of the test rig used to develop the Drive System for Compound Rotorcraft Demonstrator in the frame of IADP FRC.Based on the topic description published in this call our proposal suppose interconnection of the lateral rotor gearboxes via vertical transmission shafting, supported on two or three auxiliary bearing h ...
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 1

 TERMINÉ 

Aerospace propeller useful for diesel engines with extreme excitation of vibrations (ARGOS)

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

The project proposal is aimed at light weight and efficient jet-fuel aerospace propulsion units based on reciprocating engines. Aerospace propellers useful for jet-fuel reciprocating direct drive engines suffer by extreme excitation of vibrations. The objective of the project proposal is to design and test a new propeller useful for such operational conditions. The objective will be achieved by th ...
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 3

 TERMINÉ 

More electric, advanced hydromechanics propeller control components. (PROPCONEL)

Date du début: 12 sept. 2016, Date de fin: 11 sept. 2019,

The project proposal is aimed in category of Business Aviation/Short Range turboprop engines. The baseline core of ARDIDEN3 will be improved with focus, first of all upon combustion chamber for higher altitude operation, specific turbine and propulsive exhaust and specific control system. This way it will better fit with turboprop application. For this purpose the ARDIDEN3 core will be integrated ...
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 2

 TERMINÉ 

Future Sky Safety

Date du début: 1 janv. 2015, Date de fin: 31 déc. 2018,

The EC Flight Path 2050 vision aims to achieve the highest levels of safety to ensure that passengers and freight as well as the air transport system and its infrastructure are protected. However, trends in safety performance over the last decade indicate that the ACARE Vision 2020 safety goal of an 80% reduction of the accident rate is not being achieved. A stronger focus on safety is required. T ...
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 32

 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 

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 

CreAting NonconventionAl Laminates (CANAL)

Date du début: 1 sept. 2013, Date de fin: 31 août 2016,

The purpose of the CANAL project is to develop new Non-Conventional Laminate (NCL) configurations using Dry Fibre Placement (DFP) and the establishment of engineering tools to ensure implementation of the technology in the aerospace industry and other industries, such as automotive that can benefit from rapid and cost effective production of complex shaped and high-performance composite parts. Whe ...
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 10

 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 

Boltless assembling Of Primary Aerospace Composite Structures (BOPACS)

Date du début: 1 sept. 2012, Date de fin: 29 févr. 2016,

"The main challenge of the BOPACS project is to reduce the weight and costs of primary aerospace structures by developing bolt free adhesive bonded joints that comply with the airworthiness requirements.Until today thin walled composite primary aerospace structures are joined by using a large number of fasteners. Bolt free joining would considerably contribute to the weight and cost reduction of a ...
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 14

 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 

IMPROVING THE AIRCRAFT SAFETY BY SELF HEALING STRUCTURE AND PROTECTING NANOFILLERS (IASS)

Date du début: 1 sept. 2012, Date de fin: 31 août 2015,

Inspection and Maintenance are important aspects when considering the availability of aircraft for revenue flights. Modern airframe design is exploiting new exciting developments in materials and structures to construct ever more efficient air vehicle able to enable ‘smart’ maintenance including self-repair capabilities. The improvement in the aircraft safety by self-healing structures and protect ...
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 10

 TERMINÉ 

Investigation of novel vertical take-off and landing (VTOL) aircraft concept, designed for operations in urban areas (ANULOID)

Date du début: 1 avr. 2013, Date de fin: 31 mars 2015,

Principal objective of proposed project is computational and experimental investigation of novel concept of VTOL aircraft with nickname „Anuloid“ regarding its flight properties and flying qualities, and compare „Anuloid“ to helicopters, tilt rotor aircraft, or other VTOL aircraft concepts, in relation to potential utilization for transport missions in urban areas.
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 5

 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 

Detection of kissing bonds in friction stir welds in aero structures (StirScan)

Date du début: 1 déc. 2012, Date de fin: 30 nov. 2014,

The proposed StirScan project will develop a NDT system in order to address the challenging problem of detecting kissing bonds in Friction Stir Welds (FSW). FSW is a relatively new joining technique for aluminium alloys which offers good joint performance and excellent reproducibility – this is of significant interest to the aerospace sector, where fatigue performance is particular crucial. Howeve ...
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 8

 TERMINÉ 

Packaging of futuRe Integrated ModulAr Electronics (PRIMAE)

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

"Affordable transport for the citizen relies on innovative solutions and technologies that will result in lower costs and lead-time of the aircraft and its systems. In this area, the packaging of on-board computers is an important contributor.The Packaging of futuRe Integrated ModulAr Electronics (PRIMAE) objective is to develop a new flexible, robust and open aeronautical packaging for the next g ...
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 20

 TERMINÉ 

Contribution to Analysis of Rotor Hub Drag Reduction (CARD)

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

"A major source of helicopter drag, about 30% of the total, is from the rotor hub. It is important that the drag generated by a helicopter, and hence emissions, is reduced. This research programme is to be undertaken to investigate this subject and investigate potential techniques to achieve reductions in hub drag. A wind tunnel test programme is to be carried out to provide a large, high-quali ...
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 3

 TERMINÉ 

Innovative Manufacturing of complex Ti sheet components (INMA)

Date du début: 1 sept. 2010, Date de fin: 30 juin 2014,

"The INMA project aims at developing an intelligent knowledge-based (KB) flexible manufacturing technology for titanium shaping that will lead to drastically reduce current aircraft development costs incurred by the fabrication of complex titanium sheet components with a minimal environmental impact. In particular, this project aims at strengthening European aircraft industry competitiveness, by t ...
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 11

 TERMINÉ 

Innovative Material Synergies & Composite Processing Strategies (IMS&CPS)

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

Mutation of transport industry to carbon fibre reinforced polymer (CFRC) is now ineluctable in order to reduce our mobility environmental imprint. This sector is at a turn of its conversion from metal to composite, which should impose a radical rethinking of the whole supply chain. Combined developments of materials and matched processes is the main strategy of IMS&CPS project, only such a concert ...
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 16

 TERMINÉ 

Demonstration of LIDAR Based Wake Vortex Detection System Incorporating an Atmospheric Hazard Map (GREEN-WAKE)

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

"Wake vortex and wind shear are major causes of accidents and injury to passenger and crew of all aircraft types. There has been little protection and the main way of mitigating accidents has been to have mandatory separation times that affect the operating performance of airports. The objective of GREEN-WAKE is to develop and validate innovative technologies that will detect the Hazards and thus ...
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 14

 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 

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 

Strain Monitoring in Composite Stiffened Panels Using Sensors (STRAINMON)

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

"STRAINMON aims to develop and establish a methodology for the strain monitoring of composite fuselage stiffened panels using embedded and/or bonded Fiber-Optic Bragg Grating (FOBG) sensors and strain gauges. The proposed work-programme of STRAINMON is summarized as follows:1. Definition of the FOBG system requirements and specifications based on the nature of the problem and the available technol ...
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 2