An electric braking system for an aircraft. The system includes: an electro-mechanical brake actuator (EMAbrake) proximate a wheel of the aircraft, the EMAbrake including a motor; an electro-mechanical actuator controller (EMAC) including a motor controller for generating a drive signal for the EMAbrake; a braking control unit (BCU) for generating a braking force command signal for the EMAC during a normal mode of operation; and an emergency braking control unit (eBCU) for generating a braking force command signal for the EMAC during an emergency operating mode. The eBCU is disposed together with the EMAC in a common line replaceable unit (LRU).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft electric braking system


    Beteiligte:
    GEORGE IORDANIDIS (Autor:in) / JOHN REES (Autor:in)

    Erscheinungsdatum :

    03.06.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft electric braking system

    IORDANIDIS GEORGE / REES JOHN | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT ELECTRIC BRAKING SYSTEM

    IORDANIDIS GEORGE / REES JOHN | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft electric braking system

    JOHN REES / GEORGE IORDANIDIS | Europäisches Patentamt | 2015

    Freier Zugriff

    AIRCRAFT ELECTRIC BRAKING SYSTEM

    IORDANIDIS GEORGE / REES JOHN | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft electric braking system

    IORDANIDIS GEORGE / REES JOHN | Europäisches Patentamt | 2015

    Freier Zugriff