The invention relates to a leading-edge device (1) for an aerodynamic component (120). The leading-edge device (1) comprises a first skin element (10) having an inner surface (11) and an aerodynamic outer surface (12), and further comprises a second skin element (20) having an inner surface (21) and an aerodynamic outer surface (22). The leading-edge device (1) further comprises a first coupling element (13) protruding from the inner surface (11) of the first skin element (10) and a second coupling element (23) protruding from the inner surface (21) of the second skin element (20). The first and second coupling elements (13, 23) are coupled to each other in a coupling region (30). The first skin element (10) and the first coupling element (13) are formed as a single-piece structure. The invention also relates to a method for manufacturing a leading-edge device (1) for an aerodynamic component (100).


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    Title :

    LEADING EDGE DEVICE FOR AN AERODYNAMIC COMPONENT AND METHOD FOR MANUFACTURING A LEADING-EDGE DEVICE FOR AN AERODYNAMIC COMPONENT


    Additional title:

    VORDERKANTENVORRICHTUNG FÜR EIN AERODYNAMISCHES BAUTEIL UND VERFAHREN ZUR HERSTELLUNG EINER VORDERKANTENVORRICHTUNG FÜR EIN AERODYNAMISCHES BAUTEIL
    DISPOSITIF DE BORD D'ATTAQUE POUR UN COMPOSANT AÉRODYNAMIQUE ET PROCÉDÉ DE FABRICATION D'UN DISPOSITIF DE BORD D'ATTAQUE POUR UN COMPOSANT AÉRODYNAMIQUE


    Contributors:

    Publication date :

    2025-03-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge