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.


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    Title :

    SET OF ACTUATOR UNITS THAT DRIVE A CONTROL SURFACE OF AN AIRPLANE


    Additional title:

    GRUPPE VON ANTRIEBSEINHEITEN, DIE EINE STEUERFLÄCHE EINES FLUGZEUGS STEUERN
    ENSEMBLE D'UNITÉS D'ACTIONNEMENT QUI ENTRAÎNENT UNE SURFACE DE CONTRÔLE D'UN AVION


    Contributors:

    Publication date :

    2022-08-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte



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