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.


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    Titel :

    CONTROLLED LANDING GEAR TIRE TRACTION SYSTEM


    Weitere Titelangaben:

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


    Beteiligte:
    BARMICHEV SERGEY (Autor:in) / BOREN KELLY L (Autor:in)

    Erscheinungsdatum :

    10.01.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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