A control surface actuation mechanism for moving a control surface relative to a fixed aerofoil portion of an aircraft is disclosed including an articulating support, a sliding member on the articulating support and coupled to the control surface, the sliding member arranged to slide relative to the articulating support, a track with a path for attachment on the fixed aerofoil portion, and a rigid connecting element connected to the first track and to the sliding member. The first end of the first rigid connecting element is configured to move passively along the path, as the sliding member is driven to slide relative to the articulating support by an actuator.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Control surface actuation mechanism



    Erscheinungsdatum :

    2022-01-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT CONTROL SURFACE ACTUATION MECHANISM

    BALSIGER DERICK S | Europäisches Patentamt | 2023

    Freier Zugriff

    A CONTROL SURFACE ACTUATION MECHANISM

    KURUVILLA JASON / GAJAKOSH PRADEEP / SRINIVASAMURTHY AKSHAY et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT CONTROL SURFACE ACTUATION MECHANISM

    BALSIGER DERICK S | Europäisches Patentamt | 2023

    Freier Zugriff

    A CONTROL SURFACE ACTUATION MECHANISM

    KURUVILLA JASON / GAJAKOSH PRADEEP / SRINIVASAMURTHY AKSHAY et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT CONTROL SURFACE ACTUATION MECHANISM

    BALSIGER DERICK S | Europäisches Patentamt | 2023

    Freier Zugriff