4 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Forming and Modular Integration of Thermoplastics (FORMIT)
Date du début: 1 déc. 2016, Date de fin: 30 nov. 2017,
The main objective of FORMIT is to develop a modular tooling to integrate a wing upper skin and an external wing leading edge with several T-Shape and omega stringers. Skins will be laminated on the integration tool by Topic Manager with Automated Fiber Placement technology and stringer will be produced with an innovative continuous forming process patented by Applus. Both structures will be made ...
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2
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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 ...
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3
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TERMINÉ
Thermal and electrical Mock-ups for Thermal Management of a Ground Integration Test Rig (TEMGIR)
Date du début: 1 oct. 2014, Date de fin: 31 juil. 2016,
The TEMGIR project is for the design and development of Thermal and Electrical Mock-ups for the validation of the thermal behaviour in the electrical air systems architecture at aircraft level.TEMGIR will provide a thermal model of an aircraft with both electrical and thermal behaviour, which will be able to develop any relevant condition and scenarios within the different flight phases. The TEMGI ...
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4
Participants partenaires
TERMINÉ
PRECISSION OUTER WING ASSEMBLY DEVICES (PROUD)
Date du début: 4 sept. 2011, Date de fin: 3 févr. 2016,
The proposal approach innovative solutions for the design and manufacturing of the tooling needed for the assembly of two different kinds of configuration for the outer wings within a Smart Fixed Wing Aircraft. The PROUD proposal, understand that the main requirement for this wing structural part is based on their high dimensional stability and tight geometrical tolerances to compliance with surfa ...
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