13 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Improving the crashworthiness of composite transportation structures (ICONIC)
Date du début: 1 oct. 2016, Date de fin: 30 sept. 2020,
The European aerospace, automotive, and rail industries are committed to improving their energy efficiency to meet targets set within the EU’s climate, energy and transport policies. This is motivating the increased use of lightweight composite materials in lieu of heavier metallics. To implement this transition, these industries must reach, at least, the same level of crash performance achieved w ...
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9
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TERMINÉ
Additive Manufacturing Aiming Towards Zero Waste & Efficient Production of High-Tech Metal Products (AMAZE)
Date du début: 1 janv. 2013, Date de fin: 30 juin 2017,
The overarching goal of AMAZE is to rapidly produce large defect-free additively-manufactured (AM) metallic components up to 2 metres in size, ideally with close to zero waste, for use in the following high-tech sectors namely: aeronautics, space, automotive, nuclear fusion and tooling.Four pilot-scale industrial AM factories will be established and enhanced, thereby giving EU manufacturers and en ...
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29
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TERMINÉ
Large 3-shaft Demonstrator - Aeroengine intake acoustic liner technology development (ALTD)
Date du début: 3 oct. 2011, Date de fin: 2 oct. 2016,
A large role in the efficiency of the overall engine is played by the fan and bypass system. Lightweight, effective acoustic liners will be required to meet both the weight and noise emissions requirements. This presents an opportunity to develop the state of the art in intake liner acoustic and mechanical design and to test this liner in the engine environment.This proposal is to partake in the a ...
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3
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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
LOw COst Manufacturing and Assembly of Composite and Hybrid Structures (LOCOMACHS)
Date du début: 1 sept. 2012, Date de fin: 31 août 2016,
The continued use of composite materials in the aerospace industry has been addressed in several past research projects which have focused on new design solutions and composite manufacturing processes. However an area which has been given much less attention up until now is how to achieve a time and cost effective lean assembly production system. The current airframe assembly process of composite ...
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33
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TERMINÉ
Enabling Next Generation Composite Manufacturing by In-Situ Structural Evaluation and Process Adjustment (ECOMISE)
Date du début: 1 sept. 2013, Date de fin: 31 août 2016,
Within current composite part development and manufacturing processes a disproportional high effort is implied in order to find optimal process parameters and to meet required qualities and tolerances of high performance light weight structures.The ECOMISE project proposes a breakthrough production system to enable next generation of thermoset composite manufacturing and post-processing. Within th ...
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11
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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
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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
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
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TERMINÉ
NOVEL AERONAUTICAL MULTIFUNCTIONAL COMPOSITE STRUCTURES WITH BULK ELECTRICAL CONDUCTIVITY AND SELF-SENSING CAPABILITIES (ELECTRICAL)
Date du début: 1 oct. 2010, Date de fin: 30 juin 2014,
"Aircraft structures appear to be strategic components to be manufactured in composite materials for reducing weight, although new questions regarding electrical conductivity have arisen such as static discharge, electrical bonding and grounding, interference shielding and current return through the structure.These functions can be met by the use of technologies based on nanocomposites, which inde ...
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14
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TERMINÉ
Simulation Based Solutions for Industrial Manufacture of Large Infusion Composite Parts (INFUCOMP)
Date du début: 1 oct. 2009, Date de fin: 30 sept. 2013,
"Today, advanced composites use either layers of plies impregnated with resin (pre-pregs) to form a laminate, or Liquid Composites Moulding (e.g. RTM) of dry textiles. Prepreg composites give superior mechanical properties due to toughened resins and high fibre content, but suffer from high material costs, limited shapeability, complex, expensive and time consuming manufacturing, and limited mater ...
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15
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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
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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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