4 projets européens trouvés
Recherche sur 125080 projets européens
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
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
All Condition Operations and Innovative Cockpit Infrastructure (ALICIA)
Date du début: 1 sept. 2009, Date de fin: 31 août 2014,
"ALICIA addresses the ACARE objective of increasing time efficiency within the future air transport system. The aim will be to develop a new and scalable cockpit application which can extend operations of aircraft in degraded conditions – “All Conditions Operations”. A key objective will be to deliver an extensible application that can be applied to many aircraft types. This will necessarily enta ...
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42
Participants partenaires
TERMINÉ
Dynamics in Aircraft Engineering Design and Analysis for Light Optimized Structures (DAEDALOS)
Date du début: 1 nov. 2010, Date de fin: 30 avr. 2014,
"Today’s design and certification procedures of aircrafts are mainly based on conservative static loading which leads to additional weight and, potentially, to a structurally unsafe aircraft. The overall objective of the DAEDALOS project is to develop methods and procedures to determine dynamical loads considering the effects of dynamic buckling, material damping and mechanical hysteresis during a ...
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