The present invention relates to a leading edge (1) for aircraft made of composite material, characterized in that it comprises on its inner face a metallic-type reinforcement (2) firmly adhered to the mentioned inner face of the leading edge (1) arranged such that it confers the leading edge (1) with better capacity to adapt to deformability and greater absorption of energy due to impacts. The invention also relates to a method of manufacturing a leading edge (1) with a metallic reinforcement (2) for aircraft made of composite material.


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    Titel :

    LEADING EDGE FOR AIRCRAFT MADE OF REINFORCED COMPOSITE MATERIAL


    Weitere Titelangaben:

    AUS EINEM VERSTÄRKTEN VERBUNDWERKSTOFF HERGESTELLTE VORDERKANTE FÜR EIN FLUGZEUG
    BORD D'ATTAQUE POUR AVION FAIT DE MATÉRIAU COMPOSITE RENFORCÉ



    Erscheinungsdatum :

    07.03.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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