AIRCRAFT TIRE
    14.
    发明授权
    AIRCRAFT TIRE 有权
    FLUGZEUGREIFEN

    公开(公告)号:EP2990222B1

    公开(公告)日:2017-03-15

    申请号:EP14789121.2

    申请日:2014-04-15

    摘要: In order to suppress the dimensions and mass of an aircraft tire from becoming uneven around the tire circumferential direction, an aircraft tire includes: a belt layer (14) provided further to a tire radial direction outer side than a carcass (12); and a sheet shaped belt protection member (20) that is wound in a tire circumferential direction TC between a tread section (22) and the belt layer (14), and that includes incision portions (36) incised in a tire width direction TW, with the incision portions (36) formed at uniform intervals in the tire circumferential direction TC.

    摘要翻译: 为了抑制飞机轮胎的尺寸和质量在轮胎周向上变得不均匀,飞机轮胎包括:比胎体(12)更靠轮胎径向外侧设置的带束层(14); 以及在胎面部(22)和带束层(14)之间沿轮胎周向TC卷绕的片状带束保护构件(20),其包括沿轮胎宽度方向TW切开的切口部(36) 其中切口部分(36)在轮胎周向方向TC上以均匀的间隔形成。

    IMPROVED BODY PLY SHAPE FOR A TIRE
    15.
    发明公开
    IMPROVED BODY PLY SHAPE FOR A TIRE 审中-公开
    VERBESSERTE KARKASSENLAGEFORMFÜREINEN REIFEN

    公开(公告)号:EP3110632A1

    公开(公告)日:2017-01-04

    申请号:EP14883965.7

    申请日:2014-02-27

    IPC分类号: B60C9/08

    摘要: A tire is provided having a body ply that is displaced from the conventional equilibrium curve along the shoulder and upper side wall region of the tire in a manner that provides more uniform inflation growth along the crown region so as to reduce differences in rigidity between the center and shoulders of the tire, reduce load sensitivity, and/or decrease the propensity for cracking. A method for designing or constructing such a tire is also provided.

    摘要翻译: 提供了一种轮胎,其具有沿着沿轮胎的肩部和上侧壁区域从常规平衡曲线移位的主体帘布层,其沿着胎冠区域提供更均匀的充气生长,以便减少中心之间的刚性差异 轮胎的肩膀,降低负荷敏感性和/或降低开裂倾向。 还提供了一种用于设计或构造这种轮胎的方法。

    PNEUMATIC TIRE
    19.
    发明公开

    公开(公告)号:EP2842765A4

    公开(公告)日:2016-05-11

    申请号:EP13780848

    申请日:2013-04-24

    申请人: BRIDGESTONE CORP

    发明人: KOZUKI KENTARO

    摘要: A pneumatic tire with improved noise performance while preserving the steering stability and rolling resistance includes, on radially outer side of the crown portion of a carcass, an inclined belt consisting of inclined belt layer(s) having cords inclined at an angle of 35° to 90°relative to the tire circumferential direction, a circumferential belt consisting of circumferential belt layer(s) having cords extending along the circumferential direction, and a tread on radially outer side of the circumferential belt. The circumferential belt includes a high rigidity region across the tire equator wherein the circumferential rigidity per unit width is higher at any location thereof than at any location in the remaining regions. The circumferential rigidity per unit width in the remaining regions is constant in the tire width direction or increases toward the high rigidity region.

    A PNEUMATIC TIRE WITH A THREE DIMENSIONAL COMPONENT
    20.
    发明公开
    A PNEUMATIC TIRE WITH A THREE DIMENSIONAL COMPONENT 审中-公开
    LUFTREIFEN MIT EINEM DREIDIMENSIONALEN BAUTEIL

    公开(公告)号:EP3015285A2

    公开(公告)日:2016-05-04

    申请号:EP15190539.5

    申请日:2015-10-20

    IPC分类号: B60C9/18 B60C15/06 B60C9/02

    摘要: A pneumatic tire (10) is disclosed comprising a carcass (22) having at least one reinforced ply (14), and a reinforcing structure (400, 500, 610, 620, 630, 640, 710, 720, 730, 740, 810, 820, 830, 840, 910, 920, 930) providing a buffer for absorbing shear strain. A tread (12) is disposed radially outward of the carcass (22) and a belt structure (16) is disposed radially between the carcass (22) and the tread (12). The reinforcing structure (400, 500, 610, 620, 630, 640, 710, 720, 730, 740, 810, 820, 830, 840, 910, 920, 930) comprises at least one layer of a three dimensional fabric (420,520,613,623,633,643,713,723,733,743,813,823,833,843,913,923, 933) including or defining a frame structure of fabric and open cells (410, 510, 611, 621, 631, 641, 711, 721, 731, 741, 811, 821, 831, 841, 911, 921, 931) defined by the frame structure.

    摘要翻译: 公开了一种充气轮胎(10),其包括具有至少一个加强层(14)的胎体(22)和加强结构(400,500,610,620,630,640,710,720,730,740,810 ,820,830,840,910,920,930)提供用于吸收剪切应变的缓冲器。 胎体(12)设置在胎体(22)的径向外侧,带状结构(16)径向设置在胎体(22)和胎面(12)之间。 加强结构(400,500,610,620,630,640,710,720,730,740,810,820,830,740,710,820,820,830,740,910,920,930,830,830,810,920,930,830,830,830,810,920,930,930,830,830,840,810,920,930,930,830,830,830,810,920,930,930,830,830,830,810,920,930,930,930,930,830,830,810,910,920,930,930,930,930,930,930,930,930,930,930,930,930,930,930,930,930,930 ,933),其包括或定义织物和开放单元(410,510,611,621,631,641,711,821,831,841,911,821,831,841,911,921,931)的框架结构,所述框架结构被定义 通过框架结构。