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1. 发明申请

US20100147434A1 AIRCRAFT RADIAL TIRE 有权
标题翻译：飞机径向轮胎
公开(公告)号：US20100147434A1
公开(公告)日：2010-06-17
申请号：US12334897
申请日：2008-12-15
申请人： Kiyoshi Ueyoko , Clarence Byrd Alsobrook , Badal Das
发明人： Kiyoshi Ueyoko , Clarence Byrd Alsobrook , Badal Das
IPC分类号： B60C9/18 , B60C9/00
CPC分类号： B60C3/04 , B60C15/024 , B60C15/04 , B60C15/06 , B60C15/0607 , B60C2015/0614 , B60C2015/0617 , B60C2015/0621 , B60C2200/02 , Y10T152/10783 , Y10T152/10792 , Y10T152/10819 , Y10T152/10828
摘要： 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.
摘要翻译：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。

2. 发明授权

US08376011B2 Aircraft radial tire 有权
标题翻译：飞机子午线轮胎
公开(公告)号：US08376011B2
公开(公告)日：2013-02-19
申请号：US12334897
申请日：2008-12-15
申请人： Kiyoshi Ueyoko , Clarence Byrd Alsobrook , Badal Das
发明人： Kiyoshi Ueyoko , Clarence Byrd Alsobrook , Badal Das
IPC分类号： B60C15/024
CPC分类号： B60C3/04 , B60C15/024 , B60C15/04 , B60C15/06 , B60C15/0607 , B60C2015/0614 , B60C2015/0617 , B60C2015/0621 , B60C2200/02 , Y10T152/10783 , Y10T152/10792 , Y10T152/10819 , Y10T152/10828
摘要： 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.
摘要翻译：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。

3. 发明授权

US08967213B2 Aircraft tire 有权
标题翻译：飞机轮胎
公开(公告)号：US08967213B2
公开(公告)日：2015-03-03
申请号：US13716665
申请日：2012-12-17
申请人： Kiyoshi Ueyoko , Badal Das
发明人： Kiyoshi Ueyoko , Badal Das
IPC分类号： B60C9/18 , B60C9/26 , B60C9/28
CPC分类号： B60C9/28 , B60C9/185 , B60C9/2009 , B60C9/263 , B60C2009/1842 , B60C2009/2038 , B60C2009/2041 , B60C2200/02 , Y10T152/10765 , Y10T152/10801
摘要： A pneumatic tire having a carcass and a belt reinforcing structure wherein the belt reinforcing structure is a composite belt structure having at least one radially inner spiral layer and at least one zigzag belt reinforcing structure located radially outward of said spiral layer. The zigzag belt width is preferably wider than the spiral layer.
摘要翻译：一种具有胎体和带束加强结构的充气轮胎，其中所述带束加强结构是具有至少一个径向内螺旋层和位于所述螺旋层的径向外侧的至少一个之字形带加强结构的复合带结构。曲折带宽度优选比螺旋层宽。

4. 发明申请

US20120097312A1 REDUCED WEIGHT AIRCRAFT TIRE 审中-公开
标题翻译：减轻重量的飞机轮胎
公开(公告)号：US20120097312A1
公开(公告)日：2012-04-26
申请号：US12910161
申请日：2010-10-22
申请人： Kiyoshi Ueyoko , Badal Das
发明人： Kiyoshi Ueyoko , Badal Das
IPC分类号： B60C9/02
CPC分类号： B60C15/0027 , B60C15/0018 , B60C15/0072 , B60C15/06 , B60C2015/009 , B60C2200/02
摘要： A pneumatic tire is disclosed having a carcass and a belt reinforcing structure, the carcass comprising at least two inner plies which are wound around a annular bead member from axially inside of the annular bead member toward axially outside thereof and extends radially outward towards the crown to form respective turnup portions; At least one of the inner plies does not wrap around the annular bead member and has a terminal end which has a radial location between a first plane and a second plane, wherein the first plane is tangent to the outer radial surface of the annular bead member and parallel to the tire axis of rotation, and the second plane is tangent to the inner radial surface of the annular bead member and parallel to the axis of rotation of the tire, the carcass further comprising at least two outer plies which extend radially inward from the crown and axially outward of the annular bead member and further extend axially outward and are wrapped around the bead terminating in endings.
摘要翻译：公开了一种具有胎体和带束加强结构的充气轮胎，胎体包括至少两个内层，其从环形胎圈构件的轴向内部朝向轴向外侧缠绕在环形胎圈构件上，并且朝向冠向径向向外延伸，形成相应的翻转部分; 所述内层中的至少一个不环绕所述环形胎圈构件并且具有在第一平面和第二平面之间具有径向位置的终端，其中所述第一平面与所述环形胎圈构件的所述外径向表面相切，并且平行于所述轮胎的旋转轴线，并且所述第二平面与所述环形胎圈构件的所述内部径向表面相切并且平行于所述轮胎的旋转轴线，所述胎体还包括至少两个外层，冠部并且环形胎圈构件的轴向向外并且进一步沿轴向向外延伸并围绕胎圈缠绕，终止于端部。

5. 发明申请

US20130139942A1 AIRCRAFT TIRE 有权
标题翻译：飞机轮胎
公开(公告)号：US20130139942A1
公开(公告)日：2013-06-06
申请号：US13716665
申请日：2012-12-17
申请人： Kiyoshi Ueyoko , Badal Das
发明人： Kiyoshi Ueyoko , Badal Das
IPC分类号： B60C9/28
CPC分类号： B60C9/28 , B60C9/185 , B60C9/2009 , B60C9/263 , B60C2009/1842 , B60C2009/2038 , B60C2009/2041 , B60C2200/02 , Y10T152/10765 , Y10T152/10801
摘要： A pneumatic tire having a carcass and a belt reinforcing structure wherein the belt reinforcing structure is a composite belt structure having at least one radially inner spiral layer and at least one zigzag belt reinforcing structure located radially outward of said spiral layer. The zigzag belt width is preferably wider than the spiral layer.
摘要翻译：一种具有胎体和带束加强结构的充气轮胎，其中所述带束加强结构是具有至少一个径向内螺旋层和位于所述螺旋层的径向外侧的至少一个之字形带加强结构的复合带结构。曲折带宽度优选比螺旋层宽。

6. 发明申请

US20090308518A1 RADIAL AIRCRAFT TIRE 有权
标题翻译：径向飞机轮胎
公开(公告)号：US20090308518A1
公开(公告)日：2009-12-17
申请号：US12137830
申请日：2008-06-12
申请人： Kiyoshi Ueyoko
发明人： Kiyoshi Ueyoko
IPC分类号： B60C15/06
CPC分类号： B60C15/06 , B60C2200/02 , Y10T152/10783 , Y10T152/10837
摘要： 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.
摘要翻译：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。

7. 发明申请

US20070113944A1 Pneumatic tire 审中-公开
标题翻译：气动轮胎
公开(公告)号：US20070113944A1
公开(公告)日：2007-05-24
申请号：US11655846
申请日：2007-01-22
申请人： Kiyoshi Ueyoko , Minoru Nishi , Kazuki Numata
发明人： Kiyoshi Ueyoko , Minoru Nishi , Kazuki Numata
IPC分类号： B60C15/06
CPC分类号： B60C15/0027 , B60C5/14 , B60C5/142 , B60C15/06 , B60C15/0607 , B60C2015/0614 , B60C2200/06 , Y10T152/10828 , Y10T152/10846
摘要： 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.
摘要翻译：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。

8. 发明申请

US20050274444A1 Aircraft tire with improved bead structure 审中-公开
标题翻译：具有改善珠粒结构的飞机轮胎
公开(公告)号：US20050274444A1
公开(公告)日：2005-12-15
申请号：US10374015
申请日：2003-02-25
申请人： Kiyoshi Ueyoko , Robert Boehlefeld , John Slivka
发明人： Kiyoshi Ueyoko , Robert Boehlefeld , John Slivka
IPC分类号： B60C15/00 , B60C15/06 , B60C19/00
CPC分类号： B60C15/0072 , B60C15/0018 , B60C15/06 , B60C15/0632 , B60C2200/02 , Y10T152/10828 , Y10T152/10837
摘要： 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.
摘要翻译：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。

9. 发明授权

US06736178B2 Pneumatic tire with specified bead portion 失效
公开(公告)号：US06736178B2
公开(公告)日：2004-05-18
申请号：US09888513
申请日：2001-06-26
申请人： Yoshio Ohara , Yukio Endo , Kiyoshi Ueyoko , Kazuki Numata , Ikuji Ikeda
发明人： Yoshio Ohara , Yukio Endo , Kiyoshi Ueyoko , Kazuki Numata , Ikuji Ikeda
IPC分类号： B60C1500
CPC分类号： B60C15/04 , B29D2030/481 , B60C1/0008 , B60C15/06 , B60C2015/044 , Y10T152/10819 , Y10T152/10837 , Y10T152/10846
摘要： A pneumatic tire comprises a carcass ply extending between bead portions and is turned up around a bead core in each bead portion to form two turnup portions and a main portion therebetween; each of the turnup portion extends radially outwardly and adjoins the main portion from a certain height above the bead core; a space is surrounded by the carcass ply main portion, and each turnup portion and the bead core is filled with a small size bead apex rubber or a gas; and the bead portion is provided between the carcass ply and the bead core with a bead core cover for preventing the carcass cords from direct contacting with the bead core.

10. 发明授权

US06508285B2 Pneumatic tire 失效
标题翻译：气动轮胎
公开(公告)号：US06508285B2
公开(公告)日：2003-01-21
申请号：US09739031
申请日：2000-12-14
申请人： Kiyoshi Ueyoko
发明人： Kiyoshi Ueyoko
IPC分类号： B60C1500
CPC分类号： B60C15/0036 , B60C13/00 , B60C13/003 , B60C15/0027 , B60C15/024 , Y10T152/10495 , Y10T152/10819
摘要： 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).
摘要翻译：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。

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