A wing leading-edge device is proposed, comprising a flow body having a front side, a back side and a plurality of ribs arranged in ribs, wherein at least one of the ribs is a load introduction rib comprising at least one first lug for coupling with a drive mechanism, further comprising a second load path component, which comprises at least one second lug, wherein the second load path component is at least connected to the load introduction rib, such that a second opening of the at least one second lug is co-axial with a first opening of the at least one first lug.


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    Title :

    A WING LEADING-EDGE DEVICE AND A WING HAVING SUCH A WING LEADING-EDGE DEVICE


    Additional title:

    FLÜGELVORDERKANTENVORRICHTUNG UND FLÜGEL MIT SOLCH EINER FLÜGELVORDERKANTENVORRICHTUNG
    DISPOSITIF DE BORD D'ATTAQUE D'AILE ET AILE DOTÉE D'UN TEL DISPOSITIF DE BORD D'ATTAQUE D'AILE


    Contributors:

    Publication date :

    2020-09-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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