A braking system architecture for aircraft, the architecture comprising: a brake including friction members and electromechanical actuators for exerting a braking torque on the wheel; a computer situated in the fuselage of the aircraft and arranged to produce first control signals; and a junction box situated on the undercarriage, the junction box being connected to the computer and to the electromechanical actuators, the junction box being configured to receive the first control signals and to use the first control signals to produce second control signals for application to the electromechanical actuators in order to control the electromechanical actuators.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Braking system architecture for aircraft


    Beteiligte:
    GOYEZ BRIAN (Autor:in) / ONFROY DOMINIQUE (Autor:in) / FREY OLIVIER (Autor:in)

    Erscheinungsdatum :

    08.03.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



    AIRCRAFT BRAKING SYSTEM ARCHITECTURE

    ONFROY DOMINIQUE / FREY OLIVIER / GOYEZ BRIAN | Europäisches Patentamt | 2020

    Freier Zugriff

    Aircraft braking system architecture

    ONFROY DOMINIQUE / FREY OLIVIER / GOYEZ BRIAN | Europäisches Patentamt | 2024

    Freier Zugriff

    BRAKING SYSTEM ARCHITECTURE FOR AIRCRAFT

    GOYEZ BRIAN / ONFROY DOMINIQUE / FREY OLIVIER | Europäisches Patentamt | 2020

    Freier Zugriff

    BRAKING SYSTEM ARCHITECTURE FOR AIRCRAFT

    GOYEZ BRIAN / ONFROY DOMINIQUE / FREY OLIVIER | Europäisches Patentamt | 2020

    Freier Zugriff

    Braking system architecture for aircraft

    GOYEZ BRIAN / ONFROY DOMINIQUE / FREY OLIVIER | Europäisches Patentamt | 2020

    Freier Zugriff