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14 projets européens trouvés

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 TERMINÉ 

Zero-defect manufacturing of composite parts in the aerospace industry (ZAero)

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

In the aerospace industry very high quality standards have to be met. For the manufacturing of carbon fibre parts this is currently solved through extended end-of-line inspection in combination with re-work processes to deal with defective parts. Also, in-situ visual inspection is used for quality control, which is currently causing huge productivity losses (30%-50%) during lay-up and has become a ...
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 7

 TERMINÉ 

New Enhanced Acoustic Damping Composite Materials (NEODAMP)

Date du début: 1 janv. 2016, Date de fin: 31 déc. 2018,

NEODAMP is marked in the ITD Airframe part B, oriented to highly integrated innovative structural components, for the Large Passenger Aircraft. NEODAMP will develop new prepreg composite materials for structural purposes in the aircraft, able to support structural loads and other additional functions. The project is focused on acoustic damping and complemented with electrical conductivity studies ...
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 2

 TERMINÉ 

CROR Engine Debris Impact SHielding. Design, manufacturing, simulation and Impact test preparation (REDISH)

Date du début: 1 janv. 2016, Date de fin: 30 juin 2018,

New, eco-efficient aircrafts are challenged by a demand to significantly reduce the CO2 and NOx emission. To achieve these goals, the topic manager is exploring new configurations for integrating advanced engines and propulsion concepts to the aircraft. Most of such promising concepts as the CROR-engine, Boundary Ingestion Layer (BIL), Ultra High Bypass Ratio engines (UHBR), multiple fan cannot be ...
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 2

 TERMINÉ 

Graphene-based disruptive technologies (GrapheneCore1)

Date du début: 1 avr. 2016, Date de fin: 31 mars 2018,

This project is the second in the series of EC-financed parts of the Graphene Flagship. The Graphene Flagship is a 10 year research and innovation endeavour with a total project cost of 1,000,000,000 euros, funded jointly by the European Commission and member states and associated countries. The first part of the Flagship was a 30-month Collaborative Project, Coordination and Support Action (CP-CS ...
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 158

 TERMINÉ 

Open access pilot plants for sustainable industrial scale nanocomposites manufacturing based on buckypapers, doped veils and prepregs (PLATFORM)

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

Two FP7 European projects ELECTRICAL and SARISTU aim to develop methods to manufacture CNT reinforced multifunctional composites compatible with current industrial manufacturing processes. According to the results, three CNT integration strategies appear as promising methods to be driven towards an industrial scale manufacturing process: buckypapers, CNTtreated prepreg and CNT doped nonwoven veils ...
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 13

 TERMINÉ 

ODISEO 2015

Date du début: 1 juin 2015, Date de fin: 31 mai 2017,

The Local Agency for Employment and Training of the City Council of Getafe in the framework of its activity in support of entry into the Workforce of the disadvantaged and at risk groups, this year has decided to introduce a mobility proposal within the new training program ERASMUS+. The ALEF is proposing through the ODISEO 2015 project to give the possibility to a group of young people from Getaf ...
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 28

 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 

"Development of a rapid, multifunction, automated gap filler device" (NOGAP)

Date du début: 1 juin 2013, Date de fin: 30 juin 2014,

"Natural Laminar Flow (NLF) has been identified as a key technology to contribute to the reduction of emissions in aircraft transport. However, the stringent NLF surface requirements are difficult to be reached with conventional manufacturing processes. The aim of NOGAP project is to develop a fully automated gap filler device that is able to performance in a 3D environment and achieve surface fin ...
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 2

 TERMINÉ 

Optimal tooling system design for large composite parts (OPTOCOM)

Date du début: 1 déc. 2012, Date de fin: 31 mars 2014,

"The general objective of the project is to smartly handle the overall process of the composite integrated parts production reducing costs in two ways. First, by adequately simulating the spring back produced after the curing process and providing solutions in order to reduce the costs of reworking or assembly. Secondly, by simulating the thermal model of the set tooling/compositepart/vacuum bag a ...
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 1

 TERMINÉ 

Hybrid laminates. Industrialization for aircraft nose fuselage (HYBRIA)

Date du début: 15 mars 2012, Date de fin: 14 mars 2014,

The use of composites materials for aircraft design allows integrating other differentmaterials with non-structural functions thanks to the layered structure. This layeredstructure offers the opportunity to embed damping interleaves in the CFRP laminate toimprove the vibroacoustic damping behavior of the structure. These multifunctionalstructures will result in hybrid configurations which combine ...
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 1

 TERMINÉ 

Industrialization setup of Thermoplastics in situ consolidation process (ISINTHER)

Date du début: 1 nov. 2011, Date de fin: 31 janv. 2014,

"Thermoplastics (TP) are high molecular weight polymers which, unlike thermosetting (TS) resins, do not form a rigid three-dimensional cross-linked chemical structure after processing. This allows the TP to be readily re-melted and re-formed, not the TS. Additional advantages are: chemical/impact resistance, range of temperatures, low level of moisture uptake then low hot/wet conditions degradatio ...
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 2

 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 

Fuctional laminates development. Components compatibility and feasibility assessment. Industrialization (COMPASS)

Date du début: 8 oct. 2010, Date de fin: 7 janv. 2013,

"In the pursuit of weight reduction, future structures will have to be multifunctional in the sense that a single structure fulfils various objectives and therefore it is not necessary to develop independent structures for each of the functions required by the aircraft (acoustic and vibration attenuation, mechanical properties, electrical conductivity, etc.). Therefore multifunctional laminates ne ...
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 2