6 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
WING STRUCTURAL TEST DEVELOPMENT METHOD (WISDOM)
Date du début: 14 janv. 2013, Date de fin: 13 déc. 2016,
The proposal approach innovative solutions for the design and manufacturing of the test rig and the definition of the method and prformance for the structural testing of two different kinds of configuration for the outer wings within a Smart Fixed Wing Aircraft.The WISDOM proposal, understand that the test philosophy is to demonstrate that major components tests can be performed on flight test air ...
Voir le projet
3
Participants partenaires
TERMINÉ
Development of Electric Smart Actuator for gas turbine engines (E-SEMA)
Date du début: 1 avr. 2012, Date de fin: 31 oct. 2014,
"The E-SEMA project will design, manufacture and test an innovative concept of light, reliable and smart electrical actuator for an inlet guide vane or stator vane application of gas turbine engines that will be capable of interfacing and connecting to the engine control unit in a plug-and-play manner. This innovative concept of smart electrical actuator will be based on a multi-disciplinary appro ...
Voir le projet
6
Participants partenaires
TERMINÉ
Development and Optimization of THz NDT on Aeronautics Composite Multi-layered Structure (DOTNAC)
Date du début: 1 sept. 2010, Date de fin: 31 août 2013,
"Modern aircraft structures have to comply with severe requirements: they have to be light as well as safe. These requirements lead to an increased use of composite materials in the aircraft industry. However, new materials also require new techniques in order to inspect aircraft components during production in a non-destructive way.The primary goal of the DOTNAC project is to develop a safe, con ...
Voir le projet
10
Participants partenaires
TERMINÉ
Development of high power density electrical actuators (HP-SMART EMA)
Date du début: 1 janv. 2010, Date de fin: 30 juin 2013,
"The HP-SMART-EMA project will develop and test an innovative concept of extremely light, reliable and smart electrical actuator for control systems of turbine engines that will be capable of interfacing and connecting to the engine / turbine control unit in a plug-and-play manner. This innovative concept of smart electrical actuators will be based on a multi-disciplinary approach that will consid ...
Voir le projet
6
Participants partenaires
TERMINÉ
Full-field Advanced Non Destructive Technique for On-line Thermo-Mechanical Measurements on Aeronautical Structures (FANTOM)
Date du début: 1 déc. 2008, Date de fin: 31 mai 2012,
"The increasing use of composites, sandwich and lightweight structures and parts in new airplanes leads to a need of adapted Non Destructive Testing techniques for such new materials. Various NDT techniques are currently used for flaw detection or mechanical characterization during the development of aerostructures. There is a constant need for improved inspection methods; with increased reliabili ...
Voir le projet
6
Participants partenaires
TERMINÉ
AIRCRAFT INTEGRATED STRUCTURAL HEALTH ASSESSMENT II (AISHA II)
Date du début: 1 mai 2008, Date de fin: 31 oct. 2011,
"The safe use of complex engineering structures such as aircrafts can only be guaranteed when efficient means of damage assessment are in place. Whereas the design of civil structures is nowadays based on a damage tolerance approach and time based inspection cycles, it is envisaged that the large cost associated with this approach can be drastically reduced by switching to a condition based mainte ...
Voir le projet