Aircraft tire
    1.
    发明授权

    公开(公告)号:US09821609B2

    公开(公告)日:2017-11-21

    申请号:US14783436

    申请日:2014-04-02

    Inventor: Takeshi Yano

    Abstract: An object is to, in an aircraft tire, promote heat dissipation from circumferential direction grooves of a tread and improve durability of the tire. Plural circumferential direction grooves (central side circumferential direction grooves (14), edge portion side circumferential direction grooves (16)) that extend in a tire circumferential direction are formed in a tread (12). In a tire circumferential direction cross-section, a groove bottom (18) of at least one of the circumferential direction grooves has a wave shape having amplitude in a tire radial direction.

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