Obiettivo 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. Campo scientifico engineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftengineering and technologynanotechnologynano-materialsengineering and technologymaterials engineeringcompositescarbon fibers Programma(i) FP7-JTI - Specific Programme "Cooperation": Joint Technology Initiatives Argomento(i) JTI-CS-2011-3-GRA-01-039 - Hybrid laminates Industrialization for a/c nose fuselage/cockpit Invito a presentare proposte SP1-JTI-CS-2011-03 Vedi altri progetti per questo bando Meccanismo di finanziamento JTI-CS - Joint Technology Initiatives - Clean Sky Coordinatore FUNDACION PARA LA INVESTIGACION, DESARROLLO Y APLICACION DE MATERIALES COMPUESTOS Contributo UE € 216 362,00 Indirizzo Avda Rita Levi Montalcini (Tecnogetafe) 29 28906 Getafe Spagna Mostra sulla mappa Regione Comunidad de Madrid Comunidad de Madrid Madrid Tipo di attività Research Organisations Contatto amministrativo Sofia Delgado Labrandero (Mrs.) Collegamenti Contatta l’organizzazione Opens in new window Sito web Opens in new window Costo totale Nessun dato
