A landing gear tire traction control system and methods are presented. An outer tire of an aircraft wheel is depressurized to a depressurized state in response to a non-optimal aircraft landing condition. An inner rotor of the aircraft wheel contacts the outer tire in response to the depressurized state, and a plurality of traction studs are deployed to protrude from the outer tire in response to the inner rotor contacting the outer tire.


    Access

    Download


    Export, share and cite



    Title :

    CONTROLLED LANDING GEAR TIRE TRACTION SYSTEM


    Additional title:

    GESTEUERTES REIFENTRAKTIONSSYSTEM FÜR EIN FAHRWERK
    SYSTÈME DE TRACTION COMMANDÉ DE PNEU DE TRAIN D'ATTERRISSAGE


    Contributors:

    Publication date :

    2018-01-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B60C VEHICLE TYRES , Fahrzeugreifen



    High traction on demand aircraft landing gear system

    BARMICHEV SERGEY / BOREN KELLY L / BROWN STEPHEN T | European Patent Office | 2016

    Free access

    Aircraft landing gear tire replacement frame

    BIAN HONGNING / LI YONGMING / KONG XINYI et al. | European Patent Office | 2023

    Free access

    Aircraft landing gear tire anti-abrasion device

    WEI XIAOHUI / GAN YU / FANG XINGBO et al. | European Patent Office | 2021

    Free access

    TIRE MODELS IN AIRCRAFT LANDING GEAR SIMULATION

    van Slagmaat, M.T.P. | Taylor & Francis Verlag | 1992