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    • 1. 发明授权
    • Heavy duty pneumatic tire including narrow rib
    • 重型充气轮胎包括窄肋
    • US6112787A
    • 2000-09-05
    • US887224
    • 1997-07-02
    • Tetsuhiro FukumotoYukihide OuyaKiyoshi Ueyoko
    • Tetsuhiro FukumotoYukihide OuyaKiyoshi Ueyoko
    • B60C11/03B60C11/04B60C11/12B60C11/13B60C105/00
    • B60C11/042B60C11/047Y10S152/03
    • A heavy duty pneumatic tire having improved resistance to uneven tread wear includes a tread portion provided with an axially outer longitudinal main groove and an axially inner longitudinal narrow groove, each extending circumferentially about the tire to define a narrow rib therebetween, the axially inner edge of the narrow rib being chamfered by a slope. In the tire meridian section, the slope is straight or concave. The axial width of the axially inner longitudinal narrow groove is in the range of from 0.5 to 2.5 mm. The axial width (W3) of the slope measured between the upper and lower edges thereof is in the range of from 0.3 to 0.8 times the axial width (W2) of the narrow rib, and the radial height (H2) of the slope measured between the upper and lower edges is in the range of from 0.3 to 0.8 times the depth (H1) of the axially inner longitudinal narrow groove.
    • 具有改进的抵抗不均匀胎面磨损的重型充气轮胎包括设置有轴向外部纵向主槽和轴向内部纵向窄槽的胎面部分,每个胎面部分围绕轮胎圆周地延伸以在其间限定窄肋, 窄肋被斜坡倒角。 在轮胎子午线部分,斜坡是直的或凹的。 轴向内纵向窄槽的轴向宽度在0.5至2.5mm的范围内。 在其上边缘和下边缘之间测量的斜率的轴向宽度(W3)在窄肋的轴向宽度(W2)的0.3至0.8倍的范围内,并且斜率之间的径向高度(H2) 上边缘和下边缘在轴向内纵向窄槽的深度(H1)的0.3至0.8倍的范围内。
    • 3. 发明申请
    • AIRCRAFT RADIAL TIRE
    • 飞机径向轮胎
    • US20100147434A1
    • 2010-06-17
    • US12334897
    • 2008-12-15
    • Kiyoshi UeyokoClarence Byrd AlsobrookBadal Das
    • Kiyoshi UeyokoClarence Byrd AlsobrookBadal Das
    • B60C9/18B60C9/00
    • B60C3/04B60C15/024B60C15/04B60C15/06B60C15/0607B60C2015/0614B60C2015/0617B60C2015/0621B60C2200/02Y10T152/10783Y10T152/10792Y10T152/10819Y10T152/10828
    • A pneumatic radial aircraft tire is described having a B/A ranging between 60-70%, wherein B is the width of the tire between the wheel flange, and A is the inflated tire width under rated pressure. The tire may further optionally include a tire bead portion having a Ra/Fr1 relationship which ranges from about 1 to about 2.1, wherein: Ra is the tire heel radius at uninflated and in an new and unused condition, and Fr1 is the wheel flange elliptical radius at the heel section of the tire. The tire may further optionally include a SW/TS ratio which ranges from about 0.1 to about 0.5, wherein SW is the chafer gauge at area A, TS is the total sidewall rubber gauge at area A, wherein A is defined as the region in the sidewall that has a lower radial endpoint defined by the point of contact between the flange and the tire at inflated, unloaded condition, and an upper radial endpoint Ah defined by the tire wheel flange point of contact when the tire is at inflated, and at 100% rated load.
    • 描述了一种B / A范围在60-70%之间的气动径向飞行器轮胎,其中B是车轮凸缘之间的轮胎宽度,A是额定压力下的充气轮胎宽度。 轮胎还可以任选地包括具有从约1到约2.1的Ra / Fr1关系的轮胎胎圈部分,其中:Ra是未膨胀和新的和未使用状态下的轮胎胎跟半径,并且Fr1是车轮凸缘椭圆形 在轮胎的脚跟部分的半径。 轮胎还可以任选地包括范围为约0.1至约0.5的SW / TS比,其中SW是区域A处的胎圈包布计,TS是区域A处的总侧壁橡胶规,其中A定义为 侧壁,其具有由膨胀,无负载状态下的凸缘和轮胎之间的接触点限定的较低径向端点,以及当轮胎膨胀时由轮胎轮凸缘接触点限定的上径向端点Ah,并且在100 %额定负载。
    • 4. 发明申请
    • RADIAL AIRCRAFT TIRE
    • 径向飞机轮胎
    • US20090308518A1
    • 2009-12-17
    • US12137830
    • 2008-06-12
    • Kiyoshi Ueyoko
    • Kiyoshi Ueyoko
    • B60C15/06
    • B60C15/06B60C2200/02Y10T152/10783Y10T152/10837
    • A pneumatic tire 200 for mounting on an aircraft wheel 202 for use on an aircraft has a radial carcass and flipper reinforcement 7. The tire 200 has a pair of bead cores 82, a number of at least two or more axially inner plies 3A, 3B and 3C greater than or equal to, extending between the bead cores 82, a crown reinforcement 77 radially outward of the plies having a maximum belt width BW, and at least one flipper reinforcement 7 wrapped around each bead core 82. Each bead core 82 has a radially extending cross sectional length B. The radial carcass plies 3A through 3F are preferably made of textile reinforcing elements or cords. Each flipper reinforcement 7, similarly, is reinforced by textile reinforcing elements or cords. Each flipper reinforcement 7 has an axially inner end 7I and an axially outer end 7E. The axially outer end is turned up not higher than 1.4 times the cross sectional length B of the bead cores 82 as measured radially outwardly from the bottom of the bead core perpendicular to the axis of tire rotation. Each flipper reinforcement 7 extends along an inner surface of the bead core 82 to the axially inner end 7I located in an area that is between 0.01 BW to 0.25 BW as measured from the belt edge 78 toward a centerline of the tire 200 preferably in the range of 0.05 BW to 0.125 BW.
    • 用于安装在用于飞机上的飞行器轮202上的充气轮胎200具有径向胎体和脚蹬加强件7.轮胎200具有一对胎圈芯82,多个至少两个或更多个轴向内层3A,3B 和3C大于或等于,在胎圈芯82之间延伸,具有最大带宽BW的层的径向向外的胎冠加强件77和缠绕在每个胎圈芯82周围的至少一个胎圈加强件7.每个胎圈芯82具有 径向延伸的横截面长度B.径向胎体帘布层3A至3F优选地由织物增强元件或帘线制成。 类似地,每个挡板加强件7都被织物增强元件或帘线增强。 每个挡板加强件7具有轴向内端部7I和轴向外端部7E。 沿胎圈芯的底部垂直于轮胎旋转的轴线径向向外测量的轴向外端向上升高不超过胎圈芯82的横截面长度B的1.4倍。 每个导板加强件7沿着胎圈芯82的内表面延伸到位于从带边缘78朝向轮胎200的中心线测量的在0.01 BW至0.25 BW之​​间的区域中的轴向内端7I,优选在该范围内 0.05 BW至0.125 BW。
    • 5. 发明申请
    • Pneumatic tire
    • 气动轮胎
    • US20070113944A1
    • 2007-05-24
    • US11655846
    • 2007-01-22
    • Kiyoshi UeyokoMinoru NishiKazuki Numata
    • Kiyoshi UeyokoMinoru NishiKazuki Numata
    • B60C15/06
    • B60C15/0027B60C5/14B60C5/142B60C15/06B60C15/0607B60C2015/0614B60C2200/06Y10T152/10828Y10T152/10846
    • A pneumatic tire comprises a tread portion, a pair of sidewall portions, a pair of bead portions, a bead core disposed in each bead portion, a carcass comprising a ply of carcass cords extending between the bead portions through the tread portion and sidewall portions and turned up around the bead core in each bead portion, and an inner liner made of air-impermeable rubber extending on the tire cavity side of the carcass from one of the bead portions to the other. The radially inner end of the inner liner is located radially inside the radially innermost end of the carcass. In a radial region between the radially innermost end of the carcass and the radially outermost end of the bead core, the thickness of the inner liner is not less than 0.15 time but not more than 4.0 times the cross section diameter of the carcass cord.
    • 充气轮胎包括胎面部分,一对侧壁部分,一对胎圈部分,设置在每个胎圈部分中的胎圈芯,胎体,其包括通过胎面部分和侧壁部分在胎圈部分之间延伸的胎体帘布层层, 在每个胎圈部分中的胎圈芯圈周围,以及由不透气橡胶制成的内衬,其从胎圈部分之一延伸到胎体的轮胎腔侧。 内衬的径向内端位于胎体径向最内端的径向内侧。 在胎体的径向最内端和胎圈芯的径向最外端之间的径向区域中,内衬的厚度不小于胎体帘线的横截面直径的0.15倍但不超过4.0倍。
    • 6. 发明申请
    • Aircraft tire with improved bead structure
    • 具有改善珠粒结构的飞机轮胎
    • US20050274444A1
    • 2005-12-15
    • US10374015
    • 2003-02-25
    • Kiyoshi UeyokoRobert BoehlefeldJohn Slivka
    • Kiyoshi UeyokoRobert BoehlefeldJohn Slivka
    • B60C15/00B60C15/06B60C19/00
    • B60C15/0072B60C15/0018B60C15/06B60C15/0632B60C2200/02Y10T152/10828Y10T152/10837
    • A pneumatic radial ply tire 100 for use on aircraft has a radial reinforced carcass 20 having at least one axially inner ply 2A, 2B, 2C and 2D of textile cords 21 wound around a pair of bead cores 33. The improved bead structure 30 has a woven chipper, a radially inner end EI and axially outer end EE. The axially outer portion of the chipper is embedded in rubber chafer material above the bead base surface and inward of the bead flange surface. The axially outer end EE is terminated radially below the top of the bead core, preferably between the center and the top of the bead core 33 and the radially inner end is turned radially toward the bead core and is terminated between the bead core and the bead base. Preferably the chipper is formed of a square woven material of nylon 6, 6 or similar textile material.
    • 在飞行器上使用的气动径向帘布层轮胎100具有径向增强的胎体20,其具有围绕一对胎圈芯33缠绕的纺织帘线21的至少一个轴向内层2 A,2 B,2 C和2 D。 改进的胎圈结构30具有编织切片机,径向内端E 1和轴向外端E E。 切屑机的轴向外部部分嵌入胎圈基部表面上方的橡胶胎圈包布材料和胎圈凸缘表面的内侧。 轴向外端E E E被径向地在胎圈芯的顶部下方终止,优选地在胎圈芯33的中心和顶部之间,并且径向内端径向朝向胎圈芯转动,并且是 终止于珠芯和珠基之间。 优选地,切片机由尼龙6,6或类似纺织材料的方形编织材料形成。
    • 8. 发明授权
    • Pneumatic tire
    • 气动轮胎
    • US06508285B2
    • 2003-01-21
    • US09739031
    • 2000-12-14
    • Kiyoshi Ueyoko
    • Kiyoshi Ueyoko
    • B60C1500
    • B60C15/0036B60C13/00B60C13/003B60C15/0027B60C15/024Y10T152/10495Y10T152/10819
    • In a standard state of a tire, a contour of the tire side surface has a triangular portion projecting outside from a norm arc, which is a arc passing through a maximum width point P1 of a tire and tangentially contacting with the flange, and a portion recessing from the norm arc. The height (h1) of a maximum projecting point of the triangular projecting portion from a bead base line is 0.85˜1.15 times of the height (h0) of the end of a carcass folded portion. The height (h2) of a maximum recessing point of the recessing portion is smaller than the height (h1), and is 0.30˜0.90 times of the height (h0). A maximum boss distance (q1) from the norm arc and the maximum recess distance (q2) from the norm arc are respectively 0.001˜0.040 times of the tire cross section width (W).
    • 在轮胎的标准状态下,轮胎侧面的轮廓具有三角形部分,该三角形部分从通过轮胎的最大宽度点P1并与凸缘切向接触的弧线的范围弧向外突出, 从规范弧度下降。 三角形突出部从胎圈基线的最大突出点的高度(h1)是胎体折叠部的端部的高度(h0)的0.85〜1.15倍。 凹陷部的最大凹陷点的高度(h2)小于高度(h1),为高度(h0)的0.30〜0.90倍。 与标准弧的最大凸起距离(q1)和距离范围弧的最大凹陷距离(q2)分别为轮胎横截面宽度(W)的0.001〜0.040倍。