An aircraft braking system comprising: a first group (Ga) of actuators and a second group (Gb) of actuators. A first control module (105a) is adapted, in a nominal mode, to control the first group, and in a reconfigured mode, to control the first group and the second group. A second control module (105b) is adapted, in a nominal mode, to control the second group, and in a reconfigured mode, to control the first group and the second group. A monitoring unit adapted is adapted to monitor the first control module and the second control module, and to put the first control module into the reconfigured mode of operation when the monitoring unit detects a failure of the second control module, and to put the second control module into the reconfigured mode when the monitoring unit detects a failure of the first control module.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT BRAKING SYSTEM HAVING A HIGH LEVEL OF AVAILABILITY


    Contributors:

    Publication date :

    2018-01-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft braking system having a high level of availability

    BONIGEN FRANCOIS / FRANK DAVID / PIERRA RAPHAEL et al. | European Patent Office | 2020

    Free access

    Aircraft braking control system, undercarriage, aircraft and aircraft braking method

    HEISS ALEXANDER / ASHLEY BIDMEAD / HEBBORN ANDREW | European Patent Office | 2022

    Free access

    AIRCRAFT BRAKING SYSTEM

    BILL ANDREW | European Patent Office | 2024

    Free access

    AIRCRAFT BRAKING SYSTEM

    GALE JULIAN / BIDMEAD ASHLEY / HEBBORN ANDREW | European Patent Office | 2023

    Free access

    Aircraft braking system

    HOWELL GEORGE | European Patent Office | 2022

    Free access