5 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Production and Analysis Evolution For Lattice Related Barrel Elements Under Operations With Advanced Robustness (POLARBEAR)
Date du début: 1 déc. 2013, Date de fin: 30 nov. 2016,
The PoLaRBEAR (Production and Analysis Evolution For Lattice Related Barrel Elements Under Operations With Advanced Robustness) project focuses on reliable novel composite aircraft structures based on geodesic technology aiming at a significant higher Robustness and Technology Readiness Level (TRL).While the global structural behavior of composite geodesic structures is investigated and understood ...
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13
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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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13
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TERMINÉ
Advanced Lattice Structures for Composite Airframes (ALaSCA)
Date du début: 1 déc. 2010, Date de fin: 30 nov. 2013,
The ALaSCA project focuses on maximum weight and cost reduction significant in airframes by developing manufacture-optimized lattice fuselage structures fulfilling fundamental aspects of airworthiness.The idea behind the ALaSCA project is to perform a comprehensive investigation starting with the beneficial geodesic design well-proven in space technology and transferring it to composite aircraft f ...
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13
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TERMINÉ
Generic Linking of Finite Element based Models (glFEM)
Date du début: 1 sept. 2009, Date de fin: 31 déc. 2012,
"AREA 7.1.4.1 aims to ensure cost efficiency in air transport focussing on reduction of aircraft acquisition costs. Innovative solutions and technologies must result in lower lead time and costs of the aircraft from design to production, with a more competitive supply chain. The current proposal relates to topic AAT2008.4.1.1: ""Design Systems and Tools"". For this topic it is stated in the Work ...
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8
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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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