A wing leading edge device is proposed, comprising a flow body having a front side, which is delimited by a first spanwise edge and a second spanwise edge, a back side, which is delimited by the first spanwise edge and the second spanwise edge, a front skin arranged on the front side, a back skin arranged on the back side, and at least one stiffening arrangement between the front skin and the back skin in the region of the first spanwise edge, wherein the front skin extends continuously and free from interruptions between the first spanwise edge and the second spanwise edge and covers the at least one stiffening arrangement.


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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 :

    2020-09-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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