The device (100) has a control module (120) delivering control and position signals of an actuator (110), determined according to control messages received from a flight control managing system of an aircraft. A monitoring module (130) delivers the position signals and receives the control messages. A position sensor (112) i.e. Hall effect sensor, provides information relative to rotational positioning of a rotor of a brushless electric motor (111). Position of the actuator is determined by the control module based on initial position data provided by the monitoring module.


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    Title :

    DISPOSITIF SÉCURISÉ DE SURVEILLANCE ET DE COMMANDE POUR ACTIONNEUR DE PILOTAGE D'UN AÉRONEF


    Additional title:

    SECURED SURVEILLANCE AND CONTROL DEVICE FOR AN AIRCRAFT HANDLING ACTUATOR
    GESICHERTE VORRICHTUNG ZUR ÜBERWACHUNG UND STEUERUNG FÜR EIN FLUGZEUGSTEUERUNG-STELLGLIED


    Contributors:

    Publication date :

    2019-02-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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