A system and method of controlling aircraft brakes in an aircraft that includes a brake pedal and an electric brake actuator. An aircraft operational state is determined and an application force that is supplied to the brake pedal is determined. When the determined aircraft operational state is a ground-idle state and the determined application force is greater than a set force magnitude, an actuator brake is moved to engage the electric brake actuator and the electric brake actuator is de-energized.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft electric brake actuation system and method


    Beteiligte:
    HANLON CASEY (Autor:in) / QUITMEYER JAMES NEIL (Autor:in) / BLUNT ALLAN (Autor:in)

    Erscheinungsdatum :

    13.09.2016


    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



    Aircraft electric brake actuation system and method

    HANLON CASEY / QUITMEYER JAMES NEIL / BLUNT ALLAN | Europäisches Patentamt | 2016

    Freier Zugriff

    Electric Motor Powered Brake Actuation System

    Brown, A.K. / Woodiwiss, K.A. / Wilson, R.K. | SAE Technical Papers | 1984


    Electric Motor Powered Brake Actuation System

    Brown,A.K. / Wilson,R.K. / Woodiwiss,K.A. et al. | Kraftfahrwesen | 1984


    Brake actuation system

    BEER WILHELM / STAUZEBACH BIANCA / SCHLITT PATRICK et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    BRAKE ACTUATION SYSTEM

    BEER WILHELM / STAUZEBACH BIANCA / SCHLITT PATRICK et al. | Europäisches Patentamt | 2016

    Freier Zugriff