An electromechanical rotary actuator includes a drive member, a motor disposed inside and directly coupled to the drive member, and an output arm. The motor has a rotor configured toward an outside of the motor and directly coupled to an input of the drive member and a stator configured toward an inside of the motor and positioned inside the rotor. The output arm is disposed about the motor and is drivably connected to the drive member. The output arm defines an arcuate opening.


    Access

    Download


    Export, share and cite



    Title :

    Electromechanical hinge-line rotary actuator


    Contributors:

    Publication date :

    2020-09-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    ELECTROMECHANICAL HINGE-LINE ROTARY ACTUATOR

    VAN DE VEIRE NICHOLAS R / BALSIGER DERICK S | European Patent Office | 2019

    Free access

    ELECTROMECHANICAL HINGE-LINE ROTARY ACTUATOR

    VAN DE VEIRE NICHOLAS R / BALSIGER DERICK S | European Patent Office | 2022

    Free access

    ELECTROMECHANICAL HINGE-LINE ROTARY ACTUATOR

    VAN DE VEIRE NICHOLAS R / BALSIGER DERICK S | European Patent Office | 2018

    Free access

    Electromechanical rotary actuator

    Smith, S. P. / Mcmahon, W. J. | NTRS | 1995


    Electromechanical Rotary Actuator

    United States / National Aeronautics and Space Administration| Lockheed Missiles and Space Company | British Library Conference Proceedings | 1995