A mechanical synchronization device for a distributed system. A plurality of actuators actuate movement of control surface components of an aircraft. Each actuator has a first end coupled to a structure of the aircraft and a second end coupled to a control surface component, and a drive path from a motion provider to the control surface component, the control surface component being configured to move along the respective drive path. A power module controller is operable to simultaneously output motor drive power from a power module through an electrical bus to at least two of the motion providers in a synchronous or nearly synchronous manner to actuate movement of control surface components. The mechanical synchronization device is between at least two of the actuators and transfers torque between the actuators to maintain symmetry between the actuators. A load limiting device may limit the power transferred through the mechanical synchronization device.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Synchronization system for distributed electromechanical actuation system


    Beteiligte:
    POLCUCH ERIC A (Autor:in) / BOUMAN DAVID J (Autor:in)

    Erscheinungsdatum :

    2023-03-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16H Getriebe , GEARING



    SYNCHRONIZATION SYSTEM FOR DISTRIBUTED ELECTROMECHANICAL ACTUATION SYSTEM

    POLCUCH ERIC A / BOUMAN DAVID J | Europäisches Patentamt | 2020

    Freier Zugriff

    POSITION SYNCHRONIZATION OF AEROSPACE ELECTROMECHANICAL ACTUATORS FOR DISTRIBUTED ELECTRICAL ACTUATION SYSTEM

    Fu, J. / Mare, J.-C. / Fu, Y. | British Library Conference Proceedings | 2018


    DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION

    VIJAY ASHISH / CEPIC ADNAN / JOSYULA ANIL PRASAD et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Distributed landing gear system architecture for electromechanical actuation

    VIJAY ASHISH / CEPIC ADNAN / JOSYULA ANIL PRASAD et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    DISTRIBUTED LANDING GEAR SYSTEM ARCHITECTURE FOR ELECTROMECHANICAL ACTUATION

    VIJAY ASHISH / CEPIC ADNAN / JOSYULA ANIL PRASAD et al. | Europäisches Patentamt | 2021

    Freier Zugriff