An actuating system for an aircraft having an electromechanical actuator (25) comprising a non-volatile memory (60) wherein stored data (61) including configuration data (62) specific to the electromechanical actuator is stored. The system also includes a control unit (22) using the configuration data to implement a servo-control loop, the output signal of which is a digital signal controlling the electric motor of the electromechanical actuator and at least one digital transmission channel (50) connecting the control unit and the electromechanical actuator.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Field of electric actuating systems aboard aircrafts


    Beteiligte:

    Erscheinungsdatum :

    17.07.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL




    AIRCRAFTS OEPRATING SYSTEM AIRCRAFTS OF AIRCRAFTS OPERATING SYSTEM AND OPERATIONG METHOD OF AIRCRAFTS

    HWANG SUN YU / LIM SEUNG HAN / HONG JIN SUNG et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    INTEGRATED ELECTRIC PROPULSION SYSTEM FOR ELECTRIC AIRCRAFTS

    HUANG JINSONG / DAI ZEHUA / ZHA ZHENYU et al. | Europäisches Patentamt | 2024

    Freier Zugriff