The invention provides a bistable electromagnetic actuator comprising a yoke extending in part around a pivot axis of the actuator, an excitation coil supported by the yoke in order to generate control magnetic flux, a rotor movable about the pivot axis of the actuator and suitable for being held stationary in two stable angular positions as a function of the magnetic flux generated by the coil, an actuator member coupled to the rotor in order to form an assembly that can be turned, and a manual control device including a drive shaft dynamically coupled to the rotor in such a manner that turning the drive shaft causes the rotor to turn.


    Access

    Download


    Export, share and cite



    Title :

    BISTABLE ELECTROMAGNETIC ACTUATOR AND AIRCRAFT BRAKE VALVE PROVIDED WITH SUCH AN ACTUATOR


    Contributors:

    Publication date :

    2023-12-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H01F MAGNETS , Magnete / B64C AEROPLANES , Flugzeuge / F16K VALVES , Ventile



    AN ELECTROMECHANICAL ACTUATOR FOR AN AIRCRAFT CONTROL SURFACE, AND AN AIRCRAFT PROVIDED WITH SUCH AN ACTUATOR

    SENEGAS DAVID / MEHEZ JEROME / JESTIN MAXIME et al. | European Patent Office | 2016

    Free access

    Aircraft electric brake actuator assembly with line replaceable actuator brake

    HANLON CASEY / GECK KELLAN / QUITMEYER JAMES NEIL | European Patent Office | 2017

    Free access

    SPRING BRAKE ACTUATOR AND BRAKE RELEASE MECHANISM FOR SUCH SPRING BRAKE ACTUATOR

    FRANCZUK MICHAL / SZCZUPLAK LUKASZ | European Patent Office | 2023

    Free access

    AIRCRAFT BRAKE ACTUATOR ASSEMBLIES

    REHFUS KEVIN / DRENNEN DAVID / KLODE HARALD | European Patent Office | 2017

    Free access

    AIRCRAFT BRAKE ACTUATOR ASSEMBLIES

    REHFUS KEVIN / DRENNEN DAVID / KLODE HARALD | European Patent Office | 2021

    Free access