An aircraft tire having improved wear properties is provided. The tire includes a belt reinforcement structure that provides a flatter crown and reduces localized tensions. The belt reinforcement structure includes at least four hybrid belt plies having free ends that are positioned radially inward of at least one non-hybrid belt ply. The hybrid belt plies allow for reductions in the overall mass of the tire and improved thermal properties while still meeting requirements for burst pressure and size for aircraft tires.


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    Titel :

    AIRCRAFT TIRE


    Beteiligte:
    CRESS RONALD (Autor:in) / SCHOENMAKER JASON JOHN (Autor:in) / MAUCK SHANNON MARTELL (Autor:in) / KEEFE BRIAN (Autor:in) / DAVIS WAYNE (Autor:in)

    Erscheinungsdatum :

    31.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60C VEHICLE TYRES , Fahrzeugreifen



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