Actuator for aerospace vehicle comprising an actuating element (4), a motor (1) with a rotor (2), a first rotating element (51), a second rotating element (61), a first and second angle sensor (52, 62) for measuring a first and second angle of the first and second rotating element (51, 61) and an actuator control (7) configured to control the motor (1), based on a current output position of the actuating element (4) and based on the current rotor angle, wherein the current output position of the actuating element (4) and the current angle of the rotor (2) of a current control loop are determined based on the first angle, if the second angle sensor fails, and based on the second angle, if the first angle sensor fails.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ELECTROMECHANICAL ACTUATOR FAIL OPERATIONAL SENSING SYSTEM BASED ON TWO ANGULAR SENSORS


    Beteiligte:

    Erscheinungsdatum :

    03.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64C AEROPLANES , Flugzeuge



    ELECTROMECHANICAL ACTUATOR WITH OPERATIONAL SENSORS

    SERRAND MAXIME / MEDINA RAPHAEL / MENANTEAU PATRICE | Europäisches Patentamt | 2025

    Freier Zugriff

    FAIL-SAFE ELECTROMECHANICAL ACTUATOR

    LARSON LOWELL VAN LUND / MOORE CHRISTOPHER A | Europäisches Patentamt | 2016

    Freier Zugriff

    FAIL-SAFE ELECTROMECHANICAL ACTUATOR

    LARSON LOWELL VAN LUND / MOORE CHRISTOPHER A | Europäisches Patentamt | 2019

    Freier Zugriff

    Fail-safe electromechanical actuator

    LARSON LOWELL VAN LUND / MOORE CHRISTOPHER A | Europäisches Patentamt | 2018

    Freier Zugriff

    Fail-Safe Electromechanical braking actuator for railway vehicle

    KIM MIN SOO / CHOI MOON WON / OH SEH CHAN | Europäisches Patentamt | 2018

    Freier Zugriff