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    ENHANCED RADIAL AIRCRAFT TIRE
    2.
    发明申请
    ENHANCED RADIAL AIRCRAFT TIRE 有权
    增强径向飞机轮胎

    公开(公告)号：US20100024948A1

    公开(公告)日：2010-02-04

    申请号：US12261172

    申请日：2008-10-30

    Applicant: Walter Kevin Westgate ,  Yuvaraj Senthil Arumugam ,  Robert John Gartland

    Inventor： Walter Kevin Westgate ,  Yuvaraj Senthil Arumugam ,  Robert John Gartland

    IPC: B60C9/02 ,  C08L77/00

    CPC classification number: B60C9/08 ,  B60C9/0042 ,  B60C9/005 ,  B60C9/20 ,  B60C2200/02 ,  D02G3/48 ,  Y10S57/902 ,  Y10T152/10783 ,  Y10T152/10855 ,  Y10T152/10873

    Abstract: This invention disclosed a pneumatic tire for use on aircrafts having a tread, a crown reinforcement, and a radial carcass reinforcement. The carcass reinforcement has at least one axially inner ply of textile cord wound around a pair of bead cores, at least one axially inner ply being wound around the bead core in each bead from inside to the outside forming outside turn-ups and at least one axially outer ply of textile cords extending from bead to bead along the turn-ups of the at least one axially inner ply. Each bead has an elastomeric apex filler. The at least one axially inner ply or at least one axially outer ply has merged cords having a percent elongation at break of 12% to less than 20% and a break strength greater than 1050 N with a linear density of greater than 9,000 dtex. The preferred cord has fibers of polyamide and nylon. The cord fiber of polyamide is an aromatic polyamide 3300/2 construction. The cord fiber of nylon is a 1880/1 nylon construction. The preferred cord construction is 6.7 (A)+4.5 (N)/6.7 TPI. The cord reinforcement is preferably used in the ply layers or strips of the crown reinforcement as well.

    Abstract translation: 本发明公开了一种用于具有胎面，胎冠加强件和径向胎体增强件的飞机上的充气轮胎。 所述胎体增强件具有缠绕在一对胎圈芯上的至少一个轴向内部的纺织帘线，至少一个轴向内层在每个胎圈内缠绕在每个胎圈中，形成从室外到室外的至少一个 沿着所述至少一个轴向内层的卷边延伸的从胎圈到胎圈的纺织帘线的轴向外层。 每个珠粒具有弹性顶点填料。 所述至少一个轴向内层或至少一个轴向外层具有合并帘线，所述帘线的断裂伸长百分率为12％至小于20％，断裂强度大于1050N，线密度大于9,000dtex。 优选的帘线具有聚酰胺和尼龙的纤维。 聚酰胺的帘线纤维是芳香族聚酰胺3300/2结构。 尼龙绳索纤维是1880/1尼龙结构。 优选的帘线结构为6.7（A）+ 4.5（N）/6.7TPI。 帘线加强件也优选用于胎冠加强件的帘布层或条带中。

    METHOD OF MANUFACTURING A MERGED CORD
    6.
    发明申请
    METHOD OF MANUFACTURING A MERGED CORD 审中-公开
    制造合金线的方法

    公开(公告)号：US20120186218A1

    公开(公告)日：2012-07-26

    申请号：US13438025

    申请日：2012-04-03

    Applicant: Walter Kevin Westgate ,  Yuvaraj Senthil Arumugam ,  Robert John Gartland

    Inventor： Walter Kevin Westgate ,  Yuvaraj Senthil Arumugam ,  Robert John Gartland

    IPC: D02G3/02

    CPC classification number: B60C9/08 ,  B60C9/0042 ,  B60C9/005 ,  B60C9/20 ,  B60C2200/02 ,  D02G3/48 ,  Y10S57/902 ,  Y10T152/10783 ,  Y10T152/10855 ,  Y10T152/10873

    Abstract: A pneumatic tire for use on aircraft has a tread, a crown reinforcement, and a radial carcass reinforcement having at least one axially inner ply of textile cords wound around a pair of bead cores, at least one axially inner ply being wound around the bead core in each bead from inside to the outside forming outside turn-ups and at least one axially outer ply of textile cords extending from bead to bead along the turn-ups of the at least one axially inner ply. The at least one axially inner ply or at least one axially outer ply has merged cords having a percent elongation at break of 12% to less than 20% and a break strength greater than 1050 N with a linear density of greater than 9,000 dtex. Merged cord reinforcement is preferably used in the ply layers or strips of the crown reinforcement as well.

    Abstract translation: 用于飞机上的充气轮胎具有胎面，胎冠加强件和径向胎体加强件，其具有围绕一对胎圈芯缠绕的至少一个轴向内部的纺织帘线，至少一个轴向内层缠绕在胎圈芯 在从内到外的每个胎圈中，形成外露头和沿着至少一个轴向内层的卷边从胎圈延伸到胎圈的纺织帘线的至少一个轴向外层。 所述至少一个轴向内层或至少一个轴向外层具有合并帘线，所述帘线的断裂伸长百分率为12％至小于20％，断裂强度大于1050N，线密度大于9,000dtex。 合并帘线加固也优选用于冠部加强件的帘布层或条带中。

    Radial tire for aircraft with specified merged cords
    7.
    发明授权
    Radial tire for aircraft with specified merged cords 有权
    具有指定合并线的飞机的径向轮胎

    公开(公告)号：US08210223B2

    公开(公告)日：2012-07-03

    申请号：US12261172

    申请日：2008-10-30

    Applicant: Walter Kevin Westgate ,  Yuvaraj Senthil Arumugam ,  Robert John Gartland

    Inventor： Walter Kevin Westgate ,  Yuvaraj Senthil Arumugam ,  Robert John Gartland

    IPC: B60C9/22 ,  B60C9/20 ,  B60C9/18 ,  B60C9/00 ,  D02G3/04 ,  D02G3/28 ,  D02G3/38 ,  D02G3/48

    CPC classification number: B60C9/08 ,  B60C9/0042 ,  B60C9/005 ,  B60C9/20 ,  B60C2200/02 ,  D02G3/48 ,  Y10S57/902 ,  Y10T152/10783 ,  Y10T152/10855 ,  Y10T152/10873

    Abstract: A pneumatic tire for use on aircraft has a tread, a crown reinforcement, and a radial carcass reinforcement having at least one axially inner ply of textile cords wound around a pair of bead cores, at least one axially inner ply being wound around the bead core in each bead from inside to the outside forming outside turn-ups and at least one axially outer ply of textile cords extending from bead to bead along the turn-ups of the at least one axially inner ply. The at least one axially inner ply or at least one axially outer ply has merged cords having a percent elongation at break of 12% to less than 20% and a break strength greater than 1050 N with a linear density of greater than 9,000 dtex. Merged cord reinforcement is preferably used in the ply layers or strips of the crown reinforcement as well.

    Abstract translation: 用于飞行器的充气轮胎具有胎面，胎冠加强件和径向胎体加强件，其具有围绕一对胎圈芯缠绕的至少一个轴向内部的纺织帘线，至少一个轴向内层缠绕在胎圈芯 在从内到外的每个胎圈中，形成外露头和沿着至少一个轴向内层的卷边从胎圈延伸到胎圈的纺织帘线的至少一个轴向外层。 所述至少一个轴向内层或至少一个轴向外层具有合并帘线，所述帘线的断裂伸长百分率为12％至小于20％，断裂强度大于1050N，线密度大于9,000dtex。 合并帘线加固也优选用于冠部加强件的帘布层或条带中。

    Radial tire for aircraft with specified merged cords
    8.
    发明授权
    Radial tire for aircraft with specified merged cords 有权
    具有指定合并线的飞机的径向轮胎

    公开(公告)号：US07484545B2

    公开(公告)日：2009-02-03

    申请号：US11312879

    申请日：2005-12-20

    Applicant: Walter Kevin Westgate ,  Yuvaraj Senthil Arumugam ,  Robert John Gartland

    Inventor： Walter Kevin Westgate ,  Yuvaraj Senthil Arumugam ,  Robert John Gartland

    IPC: B60C9/08 ,  B60C9/04 ,  B60C9/02 ,  B60C9/00 ,  B60C9/20 ,  D02G3/04 ,  D02G3/28 ,  D02G3/38 ,  D02G3/48

    CPC classification number: B60C9/08 ,  B60C9/0042 ,  B60C9/005 ,  B60C9/20 ,  B60C2200/02 ,  D02G3/48 ,  Y10S57/902 ,  Y10T152/10783 ,  Y10T152/10855 ,  Y10T152/10873

    Abstract: A pneumatic tire for use on aircraft has a tread, a crown reinforcement, and a radial carcass reinforcement having at least one axially inner ply of textile cords wound around a pair of bead cores, at least one axially inner ply being wound around the bead core in each bead from inside to the outside forming outside turn-ups and at least one axially outer ply of textile cords extending from bead to bead along the turn-ups of the at least one axially inner ply. The at least one axially inner ply or at least one axially outer ply has merged cords having a percent elongation at break of 12% to less than 20% and a break strength greater than 1050 N with a linear density of greater than 9,000 dtex. Merged cord reinforcement is preferably used in the ply layers or strips of the crown reinforcement as well.

    Abstract translation: 用于飞行器的充气轮胎具有胎面，胎冠加强件和径向胎体加强件，其具有围绕一对胎圈芯缠绕的至少一个轴向内部的纺织帘线，至少一个轴向内层缠绕在胎圈芯 在从内到外的每个胎圈中，形成外露头和沿着至少一个轴向内层的卷边从胎圈延伸到胎圈的纺织帘线的至少一个轴向外层。 所述至少一个轴向内层或至少一个轴向外层具有合并帘线，所述帘线的断裂伸长百分率为12％至小于20％，断裂强度大于1050N，线密度大于9,000dtex。 合并帘线加固也优选用于冠部加强件的帘布层或条带中。

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