In order to suppress excessive temperature increases in a tread part, a tire (10) comprises: first land sections (20), wherein a plurality of circumferential grooves (14) that extends in the tire circumferential direction is formed in a tread part (12), said grooves being formed at intervals in the tire width direction, and wherein a plurality of first recesses (26) is disposed on wall surfaces (20A) in the tire circumferential direction; and a second land section (18) that is wider than the first land sections (20), and wherein a greater number of second recesses (24) than the number of first recesses (26) is disposed on wall surfaces (18A) in the tire circumferential direction.


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    Titel :

    Aircraft tire


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

    Erscheinungsdatum :

    09.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60C VEHICLE TYRES , Fahrzeugreifen



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