Objetivo 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. Ámbito científico engineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftengineering and technologynanotechnologynano-materialsengineering and technologymaterials engineeringcompositescarbon fibers Programa(s) FP7-JTI - Specific Programme "Cooperation": Joint Technology Initiatives Tema(s) JTI-CS-2011-3-GRA-01-039 - Hybrid laminates Industrialization for a/c nose fuselage/cockpit Convocatoria de propuestas SP1-JTI-CS-2011-03 Consulte otros proyectos de esta convocatoria Régimen de financiación JTI-CS - Joint Technology Initiatives - Clean Sky Coordinador FUNDACION PARA LA INVESTIGACION, DESARROLLO Y APLICACION DE MATERIALES COMPUESTOS Aportación de la UE € 216 362,00 Dirección Avda Rita Levi Montalcini (Tecnogetafe) 29 28906 Getafe España Ver en el mapa Región Comunidad de Madrid Comunidad de Madrid Madrid Tipo de actividad Research Organisations Contacto administrativo Sofia Delgado Labrandero (Mrs.) Enlaces Contactar con la organización Opens in new window Sitio web Opens in new window Coste total Sin datos