Objectif The use of composites materials for aircraft design allows integrating other differentmaterials with non-structural functions thanks to the layered structure. This layeredstructure offers the opportunity to embed damping interleaves in the CFRP laminate toimprove the vibroacoustic damping behavior of the structure. These multifunctionalstructures will result in hybrid configurations which combine traditional CFRP laminate withother materials such as rubbers or nanoparticles. Therefore hybrid configurations need tobe developed and compared with current structural solutions to quantify their improvementin terms of weight savings or functionality improvement. This proposal plans tomanufacture curved (hybrid skin) panels stiffened with twisted stringers of different shapesection by co-curing in female curing tool in one-shot process. Curved panelsmanufactured will be representative of the structure that conforms the nose fuselagestiffened skin. Champ scientifique engineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftengineering and technologynanotechnologynano-materialsengineering and technologymaterials engineeringcompositescarbon fibers Programme(s) FP7-JTI - Specific Programme "Cooperation": Joint Technology Initiatives Thème(s) JTI-CS-2011-3-GRA-01-039 - Hybrid laminates Industrialization for a/c nose fuselage/cockpit Appel à propositions SP1-JTI-CS-2011-03 Voir d’autres projets de cet appel Régime de financement JTI-CS - Joint Technology Initiatives - Clean Sky Coordinateur FUNDACION PARA LA INVESTIGACION, DESARROLLO Y APLICACION DE MATERIALES COMPUESTOS Contribution de l’UE € 216 362,00 Adresse Avda Rita Levi Montalcini (Tecnogetafe) 29 28906 Getafe Espagne Voir sur la carte Région Comunidad de Madrid Comunidad de Madrid Madrid Type d’activité Research Organisations Contact administratif Sofia Delgado Labrandero (Mrs.) Liens Contacter l’organisation Opens in new window Site web Opens in new window Coût total Aucune donnée
