4 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Innovative Wind Conversion Systems (10-20MW) for Offshore Applications (INNWIND.EU)
Date du début: 1 nov. 2012, Date de fin: 31 oct. 2017,
The overall objectives of the INNWIND.EU project are the high performance innovative design of a beyond-state-of-the-art 10-20MW offshore wind turbine and hardware demonstrators of some of the critical components. These ambitious primary objectives lead to a set of secondary objectives, which are the specific innovations, new concepts, new technologies and proof of concepts at the sub system and t ...
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29
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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
New Robust DESIgn Guideline for Imperfection Sensitive COmposite Launcher Structures (DESICOS)
Date du début: 1 févr. 2012, Date de fin: 31 juil. 2015,
"European Space industry demand for lighter and cheaper launcher transport systems. The proposed project DESICOS contributes to these aims by a new design approach for imperfection sensitive composite launcher structures, exploiting the worst imperfection idea efficiently: the Single Perturbation Load Approach. Currently, imperfection sensitive shell structures prone to buckling are designed accor ...
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13
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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