A flight control surface actuation system includes a rotary actuator having an output part configured to rotate about an axis (R-R), a connecting rod for connecting a flight control surface to the rotary actuator, and a connection mechanism connecting a first end of the connecting rod to the output part such that rotation of the output part about the axis causes at least part of the connection rod to rotate about the axis. The connection mechanism comprises a connection structure fixed to the output part and an engagement part mounted for rotation about a longitudinal axis. The engagement part extends through the connecting rod and is fixed to it. A position sensor is arranged to measure the angular displacement of the first end of the connecting rod about the axis.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FLIGHT CONTROL SURFACE ACTUATION SYSTEM


    Beteiligte:
    POTIER KARL (Autor:in) / MEDINA RAPHAEL (Autor:in) / RICARD QUENTIN (Autor:in)

    Erscheinungsdatum :

    03.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    FLIGHT CONTROL SURFACE ACTUATION SYSTEM

    POTIER KARL / MEDINA RAPHAEL / RICARD QUENTIN | Europäisches Patentamt | 2024

    Freier Zugriff

    Actuation system for flight control surface

    BRADY MICHAEL / WINKELMANN CHRISTOPH | Europäisches Patentamt | 2017

    Freier Zugriff

    Flight Control Actuation System

    P. T. Wingett / L. T. Gaines / P. S. Evans et al. | NTIS | 2004


    Flight control actuation system

    Wingett, Paul T. / Gaines, Louie T. / Evans, Paul S. et al. | NTRS | 2004


    Flight control actuation system

    Wingett, Paul T. / Gaines, Louie T. / Evans, Paul S. et al. | NTRS | 2006