An aircraft brake control system for controlling a plurality of brakeable wheels of a landing gear. Each brakeable wheel includes a brake actuator and a wheel speed sensor. The system includes a controller configured to receive aircraft control parameters and provide brake commands to the brake actuator of each wheel. The controller being configured to activate pre-retraction braking in response to an aircraft control parameter indicating that landing gear retraction is required and execute a functional brake test during pre-retraction braking.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft brake control system


    Publication date :

    2019-09-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



    AIRCRAFT BRAKE CONTROL SYSTEM

    CUESTA CASTRO CARLOS / HEBBORN ANDREW | European Patent Office | 2022

    Free access

    AIRCRAFT BRAKE CONTROL SYSTEM

    HAYES ALEXANDER / BIDMEAD ASHLEY / HEBBORN ANDREW | European Patent Office | 2024

    Free access

    AIRCRAFT BRAKE CONTROL SYSTEM

    CUESTA CASTRO CARLOS / HEBBORN ANDREW | European Patent Office | 2024

    Free access

    AIRCRAFT BRAKE CONTROL SYSTEM

    HAYES ALEXANDER / BIDMEAD ASHLEY / STORME THIERRY et al. | European Patent Office | 2022

    Free access

    AIRCRAFT BRAKE CONTROL SYSTEM

    CUESTA CASTRO CARLOS / HEBBORN ANDREW | European Patent Office | 2021

    Free access