A traction-on-demand landing gear tire 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 tire 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 tire contacting the outer tire.


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    Titel :

    High traction on demand aircraft landing gear system


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

    Erscheinungsdatum :

    2016-10-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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