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4 European Projects Found

Searched on 125080 European Projects

 FINISHED 

More Affordable Aircraft structure through eXtended, Integrated, and Mature nUmerical Sizing (MAAXIMUS)

Start date: Apr 1, 2008, End date: Sep 30, 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

 FINISHED 

Smart Intelligent Aircraft Structures (SARISTU)

Start date: Sep 1, 2011, End date: Aug 31, 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

 FINISHED 

All Condition Operations and Innovative Cockpit Infrastructure (ALICIA)

Start date: Sep 1, 2009, End date: Aug 31, 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

 FINISHED 

Dynamics in Aircraft Engineering Design and Analysis for Light Optimized Structures (DAEDALOS)

Start date: Nov 1, 2010, End date: Apr 30, 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