8 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Flutter Free FLight Envelope eXpansion for ecOnomical Performance improvement (FLEXOP)
Date du début: 1 juin 2015, Date de fin: 30 nov. 2018,
The FLEXOP project is about developing multidisciplinary aircraft design capabilities for Europe that will increase competitiveness with emerging markets -particularly in terms of aircraft development costs. A closer coupling of wing aeroelasticity and flight control systems in the design process opens new opportunities to explore previously unviable designs. Common methods and tools across the di ...
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10
Participants partenaires
TERMINÉ
Inspection Sensor and Evaluation Criteria for Assessing the Inner Surface Quality of Holes in CFRP Parts (HScan)
Date du début: 1 janv. 2016, Date de fin: 31 mars 2018,
The extended use of CFRP parts in aircraft construction (e.g. Airbus A350) requires improved process technologies for the drilling of holes in carbon fibre composites. For the assembly of hull components than 10.000 holes need to be drilled. This project aims at the development of a machine-vision-based inspection tool for the inspection of the inner surface of bores and at the definition of the r ...
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2
Participants partenaires
TERMINÉ
In situ manufactured carbon-thermoplast curved stiffened panel (INSCAPE)
Date du début: 1 janv. 2016, Date de fin: 30 juin 2017,
INSCAPE (In situ manufactured carbon-thermoplast curved stiffened panel) main objective is to enhance the automated thermoplastic fiber placement process and machine to manufacture an in situ consolidated double-curved structure including in situ joining of stiffener and skin laminate.Taking the state-of-the-art into consideration, the proposed project will focus on using and enhancing the possibi ...
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4
Participants partenaires
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
Participants partenaires
TERMINÉ
Validation of Advanced, Collaborative Robotics for Industrial Applications (VALERI)
Date du début: 1 nov. 2012, Date de fin: 31 oct. 2015,
Description
Mobile manipulator for assisting human workers in aerospace production tasks
The VALERI project proposes the development and validation of a mobile manipulator for assisting human workers in aerospace production tasks. In the current production environment, specialized and stationary r ...
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8
Participants partenaires
TERMINÉ
Quantitative inspection of complex composite aeronautic parts using advanced X-ray techniques (QUICOM)
Date du début: 1 oct. 2012, Date de fin: 30 sept. 2015,
Recent years have seen a rapidly growing demand from aeronautic industry regarding function-oriented, highly integrated, energy-efficient and lightweight structures. In advanced composites a promising material was found, which integrates these characteristics allowing for continuously elevating the complexity of new components concerning shape and internal structure. The consequences of this incre ...
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12
Participants partenaires
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
Participants partenaires
TERMINÉ
Development of an optimized large scale engine CFRP annulus filler (ORCA)
Date du début: 23 août 2010, Date de fin: 22 févr. 2013,
"This proposal describes the effort planned by the partners FACC AG, Austria & University of applied sciences (UAS) Rapperswil, Switzerland, for the development of a CFRP annulus filler.Production process will be an advanced preform concept with folding techniques and integration of all connection parts, injected with resin by an improved RTM process.Part development will start with material tests ...
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