An actuator monitoring circuit 1 which is mounted in an airplane and monitors an actuator 30 having a piston (output portion) calculates the moving distance of the piston, and outputs, when the moving distance exceeds a predetermined threshold, an approaching notification signal 78s and a progression notification signal 79s to notify the excess over the threshold.


    Access

    Download


    Export, share and cite



    Title :

    Actuator monitoring circuit, controller, and actuator unit


    Contributors:

    Publication date :

    2016-10-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / G06G Analogrechner , ANALOGUE COMPUTERS / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte



    Actuator monitoring circuit, controller, and actuator unit

    KOIZUMI TAKASHI / USUI HIROSHI / YASUDA KIYOSHI | European Patent Office | 2019

    Free access

    ACTUATOR CONTROLLER

    SWANSON JON D / DAREJEH HADI | European Patent Office | 2017

    Free access

    ACTUATOR CONTROLLER

    NAGAO TAKASHI / KATSUYAMA TATSUJI | European Patent Office | 2016

    Free access

    ACTUATOR CONTROLLER

    SWANSON JON DAREL / DAREJEH HADI | European Patent Office | 2017

    Free access

    Electromechanical actuator and actuator unit

    HIRAI MASANORI | European Patent Office | 2017

    Free access