Aircraft tire
    51.
    发明公开
    Aircraft tire 失效
    Flugzeugreifen。

    公开(公告)号:EP0307340A1

    公开(公告)日:1989-03-15

    申请号:EP88630159.7

    申请日:1988-09-07

    IPC分类号: B60C11/03

    摘要: A tire (10) suitable for use on an aircraft equipped with cambered landing gear has a symmetrical carcass structure (11) and belt structure (12) but has an asymmetrical tread portion (16). On one side of a central groove (17) the tread portion is devoid of any grooves, but on the other side of the central groove a number of grooves (18,19) extend circumferentially about the tread.

    摘要翻译: 适用于装有弧形起落架的飞机的轮胎(10)具有对称的胎体结构(11)和带束结构(12),但具有不对称的胎面部分(16)。 在中心凹槽(17)的一侧,胎面部分没有任何凹槽,但是在中心凹槽的另一侧上,许多凹槽(18,19)围绕胎面周向延伸。

    Airplane tyre
    53.
    发明公开
    Airplane tyre 失效
    Flugzeugreifen。

    公开(公告)号:EP0174147A2

    公开(公告)日:1986-03-12

    申请号:EP85306051.5

    申请日:1985-08-27

    IPC分类号: B60C9/00 B60C15/06 B60C9/20

    摘要: A tyre for an airplane having a carcass comprising carcass reinforcement (2, 3) with edges turned up around bead cores (1) and the cords at 60 to 90°, a tread reinforcement belt (5) at 0 to 30° and a band (8) over the belt wherein the cords of the carcass (2, 3) and the belt (5) comprise organic material cords having a modulus of tensile elasticity not greater than 5000 kg/mm 2. The band cords preferably have a higher modulus of tensile elasticity and may also be of organic fibres. The cord angles of the band (8) are in the range of 0 to 5°.
    The belt (5) may have folded edges. The tyre may include bead apices (7) between the carcass reinforcement (2, 3) and the folded up portions (2a, 3a). Preferred materials for the apex and fabric topping compounds are also provided as are rubber cushion pieces (6) adjacent to the belt (5).

    摘要翻译: 一种用于飞机的具有胎体的轮胎,包括胎圈加强件(2,3),边缘在胎圈芯(1)周围翻转,帘线在60至90度处,胎面增强带(5)在0至30度,带 (8),其中胎体(2,3)和带(5)的帘线包括拉伸弹性模量不大于5000kg / mm 2的有机材料帘线。 带束帘线优选具有较高的拉伸弹性模量,并且也可以是有机纤维。 带(8)的帘线角在0〜5°的范围内。 皮带(5)可以具有折叠边缘。 轮胎可以包括在胎体增强件(2,3)和折叠部分(2a,3a)之间的胎圈顶点(7)。 还提供了用于顶点和织物顶部化合物的优选材料,即邻近带(5)的橡胶垫片(6)。

    BANDE DE ROULEMENT POUR PNEUMATIQUE D'AVION
    54.
    发明公开

    公开(公告)号:EP3377335A1

    公开(公告)日:2018-09-26

    申请号:EP16809504.0

    申请日:2016-11-18

    IPC分类号: B60C1/00 C08L23/16

    摘要: The present invention relates to an aircraft tyre and, in particular, the tread thereof. The tread (2), of axial width L, comprises: a middle portion (3) having an axial width LC that is at least equal to 50% and at most equal to 80% of the axial width L, formed by a middle rubber composition; and two side portions (41, 42) positioned axially on each side of the middle portion (3), each side portion having an axial width (LS1, LS2) that is at least equal to 10% and at most equal to 25% of the axial width L, and each being formed by a side rubber composition. According to the invention, the middle rubber composition comprises at least 50 phr of a middle-portion first diene elastomer, at most 70 phr of a middle-portion reinforcing filler, and a cross-linking system, said middle-portion first diene elastomer being a terpolymer of ethylene, of an α-olefin, and of a non-conjugated diene, and the side rubber composition of each side portion comprises at least 50 phr of a side-portion first diene elastomer, a concentration of side-portion reinforcing filler that is at least equal to the concentration of middle-portion reinforcing filler and a cross-linking system, said side-portion first diene elastomer being a terpolymer of ethylene, of an α-olefin, and of a non-conjugated diene.

    AIRCRAFT TIRE PRESSURE SENSOR RESONANT LOOP LINK

    公开(公告)号:EP3186098B1

    公开(公告)日:2018-06-20

    申请号:EP15760334.1

    申请日:2015-08-24

    申请人: Eldec Corporation

    IPC分类号: B60C23/04

    CPC分类号: B60C23/043 B60C2200/02

    摘要: The aircraft tire pressure resonant loop link assembly electromagnetically couples a magnetic field between a wheel axle electromagnetic adapter transformer primary coil and a tire pressure sensor receiver coil for powering a tire pressure sensor, and includes a pair of spaced apart electrically conductive connecting arms, a single electrically conductive primary loop electrically connected to first ends of the connecting arms mounted adjacent to a secondary tire pressure sensor coil, and a circuit including a resonant tuning capacitor and a secondary coil with one or more electrically conductive loops at second ends of the connecting arms. The tire pressure sensor coil pair includes a transformer core, and secondary resonant coil pair also includes a transformer core.

    AIRCRAFT TIRE
    59.
    发明授权
    AIRCRAFT TIRE 有权
    飞机轮胎

    公开(公告)号:EP2990232B1

    公开(公告)日:2018-03-21

    申请号:EP14788818.4

    申请日:2014-04-15

    IPC分类号: B60C11/04 B60C11/03 B60C11/13

    摘要: 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.

    PNEUMATIC TIRE
    60.
    发明授权

    公开(公告)号:EP2669097B1

    公开(公告)日:2018-03-14

    申请号:EP12739407.0

    申请日:2012-01-19

    发明人: YANO, Takeshi

    IPC分类号: B60C11/00 B60C9/08

    摘要: Provided is a pneumatic tire, which is configured to be in a tire posture where the tire is assembled to an applicable rim (R) to be once filled to a specified internal pressure which is then reduced to a pressure capable of allowing the tire (1) to maintain its shape, has a land portion surface of an intermediate land portion (20, 21) positioned inward in the tire radial direction relative to a virtual arc ( A ) circumscribing at least part of each of a land portion surface at the center position (C) of the center land portion (17) and a land portion surface of a shoulder land portion (18, 19), in a cross section in the tire width direction, so that a step depth ´ of the land portion surface of the intermediate land portion (20, 21) relative to the virtual arc ( A ) satisfies the following relation across the entire area of the land portion surface of the intermediate land portion (20, 21) in the tire width direction; r / 400 ‰¤ ´ ‰¤ r /100, where r is the tire radius from the tire center axis at the center position (C) of the center land portion (17).