An aerodynamic control surface assembly includes a structure (2) with an aerodynamic surface (8) and a curved aerodynamic control surface (20) configured to move between an extended (24) and a retracted position (22). The aerodynamic control surface is arranged to deploy through an aperture (18) in the aerodynamic surface and into an oncoming airflow (A). An actuation mechanism (52, 152, 252) coupled to the aerodynamic control surface (20) moves the aerodynamic control surface (20) between extended and retracted positions. The actuation mechanism (52, 152, 252) is configured such that the control surface (20) follows a curved kinematic path (40, 140, 240) as the control surface moves between the extended (24) and retracted positions (22). The actuation mechanism (52, 152, 252) remains fully behind the aerodynamic surface (8) throughout the movement of the aerodynamic control surface (20) between the extended (24) and retracted positions (22).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AERODYNAMIC CONTROL SURFACE


    Beteiligte:
    HEALY DAREN (Autor:in)

    Erscheinungsdatum :

    01.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AERODYNAMIC CONTROL SURFACE

    HEALY DAREN | Europäisches Patentamt | 2023

    Freier Zugriff

    Aerodynamic control surface

    HEALY DAREN | Europäisches Patentamt | 2024

    Freier Zugriff

    AERODYNAMIC CONTROL SURFACE

    PETROV ALBERT VASILEVICH / BOGATYREV VLADIMIR VALEREVICH | Europäisches Patentamt | 2017

    Freier Zugriff

    Aerodynamic control surface

    DAREN HEALY | Europäisches Patentamt | 2023

    Freier Zugriff

    Aerodynamic control surface assembly

    DAREN HEALY | Europäisches Patentamt | 2023

    Freier Zugriff