A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.


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    Titel :

    High-Positioned 2-Postion Variable Camber Krueger


    Beteiligte:
    SAKURAI SEIYA (Autor:in) / FOX STEPHEN J (Autor:in) / REYES VICTOR H (Autor:in)

    Erscheinungsdatum :

    2016-10-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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