In order to suppress an excessive increase in the temperature of a tread section, a tire includes: a first land portion that is formed at a tread section by providing a plurality of circumferential direction grooves extending around a tire circumferential direction at an interval in a tire width direction, and that includes a plurality of first recesses provided in the tire circumferential direction of a wall face of the first land portion; and a second land portion that is formed by the circumferential direction grooves provided at the tread section, that has a wider width than the first land portion, and that includes a greater number of second recesses than a number of the first recesses, the second recesses being provided in the tire circumferential direction of a wall face of the second land portion.


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    Titel :

    AIRCRAFT TIRE


    Weitere Titelangaben:

    FLUGZEUGREIFEN
    PNEUMATIQUE D'AERONEF


    Beteiligte:
    SAKIYAMA TOMOTAKA (Autor:in) / OKITA YOHEI (Autor:in)

    Erscheinungsdatum :

    2018-03-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60C VEHICLE TYRES , Fahrzeugreifen



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