An aircraft emergency brake system includes a modulating emergency/parking brake valve in fluid communication with and disposed between a pressure source and a wheel brake and a lever assembly operatively connected with the brake valve. The emergency brake system is operative in first and second stages. The lever assembly includes a handle, a lock mechanism and an unlock mechanism. The handle is movable between a non-actuated position and a fully-actuated position. The brake pressure provided to the wheel brake through the brake valve depends on a position of the handle. The lock mechanism is operatively connected with the handle to obstruct the handle from moving from the first stage to the second stage. The unlock mechanism is disposed on the handle to unlock the lock mechanism allowing movement of the handle to the second stage position from the first stage position.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft brake system


    Contributors:

    Publication date :

    2015-08-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05G CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY , Steuer- oder Regelvorrichtungen oder Steuer- oder Regelsysteme gekennzeichnet ausschließlich durch mechanische Einzelheiten / B64C AEROPLANES , Flugzeuge



    AIRCRAFT BRAKE SYSTEM

    ARSENAULT TYLER / MASTROCOLA NAISON E / GEORGIN MARC et al. | European Patent Office | 2022

    Free access

    AIRCRAFT BRAKE SYSTEM

    GEORGIN MARC | European Patent Office | 2024

    Free access

    AIRCRAFT BRAKE SYSTEM

    GEORGIN MARC | European Patent Office | 2023

    Free access

    Aircraft brake system

    GEORGIN MARC | European Patent Office | 2024

    Free access

    AIRCRAFT BRAKE SYSTEM

    ARSENAULT TYLER / MASTROCOLA NAISON E / GEORGIN MARC et al. | European Patent Office | 2021

    Free access