A actuator arrangement is disclosed in which the high-lift device support that supports and guides movement of a high-lift device, such as a flap, is in axial alignment with a control actuator assembly that controls one or more control surfaces. This allows a single support fairing to be sufficient for covering both the track member and the control actuator assembly and allowing for reduced drag and weight.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ACTUATOR ARRANGEMENT AND WING ASSEMBLY FOR AN AIRCRAFT


    Beteiligte:
    ANDREANI LUC (Autor:in) / LORENZ FLORIAN (Autor:in)

    Erscheinungsdatum :

    30.11.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    ACTUATOR ARRANGEMENT AND WING ASSEMBLY FOR AN AIRCRAFT

    ANDREANI LUC / LORENZ FLORIAN | Europäisches Patentamt | 2023

    Freier Zugriff

    Actuator arrangement for a wing assembly of an aircraft

    ANDREANI LUC / LORENZ FLORIAN | Europäisches Patentamt | 2025

    Freier Zugriff



    Actuator device for wing assembly of aircraft, wing assembly and aircraft

    ANDREANI LUCI / LORENZ FLORIAN | Europäisches Patentamt | 2023

    Freier Zugriff