A gurney flap assembly (50) has an actuator (100) and a body (155). The body (155) has a leading edge and a trailing edge and includes a first panel (215) attaching to the actuator (100) proximate the leading edge, and a second panel (205) attaching to a first hinge (223) at the trailing edge. A second hinge (222) attaches the first and second panel (215, 205). Linear motion of an actuator output (110) is transposed to the gurney flap (150), thereby causing the gurney flap (150) to expand and deploy into the airstream on the pressure side of a wing (75).


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    Titel :

    Active gurney flap


    Weitere Titelangaben:

    Aktive Gurney-Klappe
    Volet de Gurney actif


    Beteiligte:
    BREWER PAUL R (Autor:in) / RAVAL REG R (Autor:in) / SHORCOTT STEVEN (Autor:in)

    Erscheinungsdatum :

    2016-11-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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