专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US07950430B2 Pneumatic aviation tire 有权
标题翻译：气动航空轮胎
公开(公告)号：US07950430B2
公开(公告)日：2011-05-31
申请号：US11697353
申请日：2007-04-06
申请人： Roel Domingo Villanueva , John Joseph Slivka
发明人： Roel Domingo Villanueva , John Joseph Slivka
IPC分类号： B60C9/18 , B60C9/20 , B60C9/22
CPC分类号： B60C9/2204 , Y10T152/10765 , Y10T152/10783
摘要： Pneumatic tires for aircraft service having a belt package with shoulder reinforcement. The tire includes a belt reinforcing structure or belt package having multiple cut belts, multiple spiral wound belt layers positioned radially between the cut belts and the tread, and multiple spiral wound shoulder layers proximate the shoulder. The spiral wound belt layers and the spiral wound shoulder layers are formed by a continuous cord-reinforced strip having a strip width. The spiral wound belt layers are characterized by a first winding pitch of approximately one strip width per revolution and the spiral wound shoulder layers are characterized by a second winding pitch of less than one strip width per revolution. Alternatively, the spiral wound shoulder layers may be formed with a tiered arrangement by shifting the starting location for successive spiral wound belt layers laterally so that the side edges are not coincident.
摘要翻译：用于飞机服务的气动轮胎具有带肩带加强件的皮带包装。轮胎包括具有多个切割带的带束加强结构或带束包，位于切割带和胎面之间的径向位置的多个螺旋缠绕带束层和靠近肩部的多个螺旋缠绕肩部层。螺旋缠绕带层和螺旋缠绕肩层由具有条带宽度的连续帘线加强条形成。螺旋卷绕带层的特征在于每转大约一个带宽的第一卷绕间距，并且螺旋缠绕肩层的特征在于每转小于一个带宽的第二卷绕间距。或者，螺旋缠绕肩层可以通过横向移动用于连续螺旋卷绕带束层的起始位置使得侧边缘不重合而形成为分层布置。

2. 发明授权

US07216684B2 Pneumatic aviation tire 有权
标题翻译：气动航空轮胎
公开(公告)号：US07216684B2
公开(公告)日：2007-05-15
申请号：US10747835
申请日：2003-12-29
申请人： Roel Domingo Villanueva , John Joseph Slivka
发明人： Roel Domingo Villanueva , John Joseph Slivka
IPC分类号： B60C9/20 , B29D30/16 , B29D30/38
CPC分类号： B60C9/2204 , Y10T152/10765 , Y10T152/10783
摘要： Pneumatic tires for aircraft service having a belt package with shoulder reinforcement. The tire includes a belt reinforcing structure or belt package having multiple cut belts, multiple spiral wound belt layers positioned radially between the cut belts and the tread, and multiple spiral wound shoulder layers proximate the shoulder. The spiral wound belt layers and the spiral wound shoulder layers are formed by a continuous cord-reinforced strip having a strip width. The spiral wound belt layers are characterized by a first winding pitch of approximately one strip width per revolution and the spiral wound shoulder layers are characterized by a second winding pitch of less than one strip width per revolution. Alternatively, the spiral wound shoulder layers may be formed with a tiered arrangement by shifting the starting location for successive spiral wound belt layers laterally so that the side edges are not coincident.
摘要翻译：用于飞机服务的气动轮胎具有带肩带加强件的皮带包装。轮胎包括具有多个切割带的带束加强结构或带束包，位于切割带和胎面之间的径向位置的多个螺旋缠绕带束层和靠近肩部的多个螺旋缠绕肩部层。螺旋缠绕带层和螺旋缠绕肩层由具有条带宽度的连续帘线加强条形成。螺旋卷绕带层的特征在于每转大约一个带宽的第一卷绕间距，并且螺旋缠绕肩层的特征在于每转小于一个带宽的第二卷绕间距。或者，螺旋缠绕肩层可以通过横向移动用于连续螺旋卷绕带束层的起始位置使得侧边缘不重合而形成为分层布置。

3. 发明授权

US07360571B2 Pneumatic tire with composite belt structure 有权
标题翻译：气动轮胎带复合带结构
公开(公告)号：US07360571B2
公开(公告)日：2008-04-22
申请号：US10663637
申请日：2003-09-16
申请人： Kiyoshi Ueyoko , John Joseph Slivka , Roel Domingo Villanueva , Robert John Boehlefeld
发明人： Kiyoshi Ueyoko , John Joseph Slivka , Roel Domingo Villanueva , Robert John Boehlefeld
IPC分类号： B60C9/22 , B60C9/18
CPC分类号： B29D30/3035 , B29D30/70 , B60C9/2204 , B60C9/263 , B60C2200/02 , Y10T152/10783 , Y10T152/10855
摘要： A method of forming a composite belt structure for a tire is disclosed. The composite belt structure has cord reinforced layers including at least two radially outer zigzag belt layers. The cords per inch in the shoulder portion are greater than the cords per inch in the central portion as measured centered on the centerplane of the belt structure. The method discloses the steps of applying a multicord reinforced strip having a strip width SW onto a rotating crowned building drum, the strip being wound in a zigzag configuration to form at least two zigzag layers, wherein the crowned drum has non-overlapping portions of the strip placed in a central portion and extending in alternation to a pair of shoulder portions having portions of the strips overlapping to form belt layers.
摘要翻译：公开了一种形成轮胎用复合带结构体的方法。复合带结构具有帘线加强层，其包括至少两个径向外的锯齿状带层。肩部部分每英寸的帘线大于中心部分中每英寸的帘线，其中心以带状结构的中心平面为中心。该方法公开了将具有条带宽度SW的多股加强条施加到旋转的冠状成型鼓上的步骤，该条以Z字形构造缠绕以形成至少两个之字形层，其中，冠状鼓具有不重叠的部分条带放置在中心部分中并且交替地延伸到一对肩部，所述肩部的部分重叠以形成带束层。

4. 发明授权

US07467653B1 Aircraft tire with improved high speed properties 失效
标题翻译：飞机轮胎具有改进的高速性能
公开(公告)号：US07467653B1
公开(公告)日：2008-12-23
申请号：US09297589
申请日：1996-11-27
申请人： John Joseph Slivka , Thomas William Cooper , Hal Warren Stilley, Jr. , Oscar Allen Hash , Jerome Wesley Ward
发明人： John Joseph Slivka , Thomas William Cooper , Hal Warren Stilley, Jr. , Oscar Allen Hash , Jerome Wesley Ward
IPC分类号： B60C9/26 , B60C9/18
CPC分类号： B60C9/26 , B29D30/70 , B60C9/2009
摘要： An aircraft tire having a folded belt construction and a belt edge strip over the folded belt construction has improved high speed properties. The belt edge strip substantially covers the top surface and/or the bottom surface of the folded belt in addition to the folded belt edges. The folded belt construction is reinforced with high modulus materials, and the belt edge strip is reinforced with low modulus materials. In a method of the invention, plies which make up the belt reinforcement package are applied to a belt building drum while the building drum is at different diameters to minimize stresses on the belt package. In a method of building a tire of the invention, a tire carcass on a tire building drum is expanded to the belt package.
摘要翻译：在折叠带结构上具有折叠带结构和带边缘条的飞机轮胎具有改进的高速性能。除了折叠的带边缘之外，带边缘条基本上覆盖折叠带的顶表面和/或底表面。折叠带结构用高模量材料增强，带边缘带用低模量材料增强。在本发明的方法中，将构成皮带增强包装的帘布层施加到皮带成型鼓上，同时制成鼓的直径不同，以使皮带包装上的应力最小化。在制造本发明的轮胎的方法中，将轮胎成型鼓上的轮胎胎体扩展到带束包装。

5. 发明授权

US06343637B1 Pneumatic tire with breaker assembly including rubber/fabric wear strip 失效
公开(公告)号：US06343637B1
公开(公告)日：2002-02-05
申请号：US09574818
申请日：2000-05-19
申请人： John Joseph Slivka
发明人： John Joseph Slivka
IPC分类号： B60C918
CPC分类号： B60C9/18 , B60C2200/02 , Y10T152/10765
摘要： A pneumatic tire 10 for use in aircraft landing applications is provided. The tire includes a breaker assembly 20, 20A, 20B having circumferentially extending layers of cord fabric and wear strips to enhance performance. In one embodiment, the wear strips are rubber and are provided as central portions 26, 44 of breaker layers 24, 40 with cord fabric extensions 30, 48 on either side. In a second embodiment, the wear strips are thin, narrow rubber strips 72 imposed between adjacent cord fabric breaker layers 56, 60, 64, 68. In a third embodiment, the wear strips are narrow cord fabric strips 92 imposed between adjacent cord fabric layers 80, 84, 88.

6. 发明授权

US07789120B2 Tire having a composite belt structure 有权
标题翻译：轮胎具有复合带结构
公开(公告)号：US07789120B2
公开(公告)日：2010-09-07
申请号：US11103110
申请日：2005-04-11
申请人： Kiyoshi Ueyoko , John Joseph Slivka , Roel Domingo Villaneuva , Robert John Boehlefeld
发明人： Kiyoshi Ueyoko , John Joseph Slivka , Roel Domingo Villaneuva , Robert John Boehlefeld
IPC分类号： B60C9/22
CPC分类号： B60C9/263 , B60C9/2204 , Y10T152/10783
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 pair of radially outer zigzag layers and at least one spirally wound belt layer with cords inclined at an inclination of 5 degrees or less relative to the tire's centerplane and located radially inward of and adjacent to the at least two radially outer belt layers. The at least two radially outer zigzag belt layers have cords inclined at 5 degrees to 30 degrees relative to the tire's centerplane and extending in alternation to turnaround points at each lateral edge of the belt layer. At each turnaround point the cords are folded or preferably bent to change direction across the crown of the carcass thus forming a zigzag cord path.
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对径向外曲折层的至少一个螺旋缠绕带束层的复合带结构，其中线束以5度或更小的倾斜倾斜相对于轮胎的中心面并位于至少两个径向外侧带束层的径向内侧并与其相邻。所述至少两个径向外部的Z字形带层具有相对于轮胎的中心面倾斜5度至30度的帘线，并且在带束层的每个侧边缘处交替延伸至周转点。在每个周转点处，帘线被折叠或优选弯曲以改变穿过胎体冠部的方向，从而形成之字形绳路径。

7. 发明授权

US06354350B1 Pneumatic tire with breaker assembly including rubber/fabric wear strip 失效
标题翻译：具有断路器组件的气动轮胎，包括橡胶/织物耐磨条
公开(公告)号：US06354350B1
公开(公告)日：2002-03-12
申请号：US09574880
申请日：2000-05-19
申请人： John Joseph Slivka
发明人： John Joseph Slivka
IPC分类号： B60C918
CPC分类号： B60C9/18 , B60C2200/02 , Y10T152/1081
摘要： A pneumatic tire 10 for use in aircraft landing applications is provided. The tire includes a breaker assembly 20, 20A, 20B having circumferentially extending layers of cord fabric and wear strips to enhance performance. In one embodiment, the wear strips are rubber and are provided as central portions 26, 44 of breaker layers 24, 40 with cord fabric extensions 30, 48 on either side. In a second embodiment, the wear strips are thin, narrow rubber strips 72 imposed between adjacent cord fabric breaker layers 56, 60, 64, 68. In a third embodiment, the wear strips are narrow cord fabric strips 92 imposed between adjacent cord fabric layers 80, 84, 88.
摘要翻译：提供了一种用于飞机着陆应用的充气轮胎10。轮胎包括具有周向延伸的绳索织物层和耐磨条以提高性能的断路器组件20,20A，20B。在一个实施例中，磨损条是橡胶，并且被设置为具有两侧的帘线织物延伸部30,48的破碎层24,40的中心部分26,44。在第二实施例中，耐磨条是施加在相邻的帘线织物断层层56,60,64,68之间的薄而窄的橡胶条72.在第三实施例中，耐磨条是施加在相邻帘布层之间的窄帘布条带92 80，84，88。

8. 发明申请

US20130056126A1 AIRCRAFT TIRE 审中-公开
标题翻译：飞机轮胎
公开(公告)号：US20130056126A1
公开(公告)日：2013-03-07
申请号：US13225799
申请日：2011-09-06
申请人： Kiyoshi Ueyoko , Leonard James Reiter , Maure Ellen Knavish , David Charles Wagner , David Paul George , Bret Herbert Marts , John Joseph Slivka
发明人： Kiyoshi Ueyoko , Leonard James Reiter , Maure Ellen Knavish , David Charles Wagner , David Paul George , Bret Herbert Marts , John Joseph Slivka
IPC分类号： B60C15/06
CPC分类号： B60C15/0635 , B60C15/0603 , B60C15/0632 , B60C2015/009 , B60C2015/061 , B60C2015/0614 , B60C2015/0621 , B60C2200/02
摘要： A pneumatic tire in accordance with the present invention includes two annular bead portions, a carcass, and a belt reinforcement layer. The carcass extends between the bead portions through sidewall portions and a tread portion. The carcass has at least one carcass ply of parallel cords turned up about the bead portions. The belt reinforcement layer is disposed radially outside the carcass and radially inside the tread portion. Each annular bead portion includes an annular bead core having the carcass ply turned up around the bead core, a first apex disposed adjacent and radially outward of the bead core, a second apex disposed axially outward of the bead core and the carcass ply, a first chafer disposed adjacent the carcass ply and axially outward of the bead core, and a second chafer disposed adjacent and axially outward the second apex and axially inward a sidewall portion. The first apex comprises a material with a 100 percent modulus between 1.0 MPa and 6.0 MPa. The second apex comprises a material with a 100 percent modulus between 1.0 MPa and 6.0 MPa. The first chafer comprises a material with a 100 percent modulus between 2.0 MPa and 4.0 MPa. The second chafer comprises a material with a 100 percent modulus between 1.0 MPa and 6.0 MPa. The sidewall portions comprise a material with a 100 percent modulus between 1.0 MPa and 2.0 MPa.
摘要翻译：根据本发明的充气轮胎包括两个环形胎圈部分，胎体和带束层加强层。胎体通过侧壁部分和胎面部分在胎圈部分之间延伸。胎体具有至少一个围绕胎圈部分翻转的平行绳的胎体帘布层。带加强层设置在胎体的径向外侧并且在胎面部的径向内侧。每个环形胎圈部分包括环形胎圈芯，胎圈芯具有围绕胎圈芯的卷边帘布层，第一顶点与珠芯相邻并径向向外设置，第二顶点设置在胎圈芯和胎体帘布层的轴向外侧，第一顶点胎圈包布邻近胎体帘布层布置，并且位于胎圈芯的轴向外侧;以及第二胎圈包布，其与第二顶点相邻并且轴向向外设置，并且轴向向内设置侧壁部分。第一顶点包括具有1.0MPa至6.0MPa之间的100％模量的材料。第二顶点包括具有1.0MPa至6.0MPa之间的100％模量的材料。第一胎圈包布包含具有2.0MPa至4.0MPa之间的100％模量的材料。第二胎圈包布包括具有1.0MPa至6.0MPa之间的100％模量的材料。侧壁部分包括具有1.0MPa和2.0MPa之间的100％模量的材料。

9. 发明授权

US6131633A Pneumatic tire with breaker assembly including rubber/fabric wear strip 有权
标题翻译：具有断路器组件的气动轮胎，包括橡胶/织物耐磨条
公开(公告)号：US6131633A
公开(公告)日：2000-10-17
申请号：US202278
申请日：1998-11-30
申请人： John Joseph Slivka
发明人： John Joseph Slivka
IPC分类号： B60C9/18 , B60C5/00 , B60C9/20 , B60C11/24 , B60C19/00
CPC分类号： B60C9/18 , B60C2009/2041 , Y10T152/10027 , Y10T152/10765
摘要： A pneumatic tire 10 for use in aircraft landing applications is provided. The tire includes a breaker assembly 20, 20A, 20B having circumferentially extending layers of cord fabric and wear strips to enhance performance. In one embodiment, the wear strips are rubber and are provided as central portions 26, 44 of breaker layers 24, 40 with cord fabric extensions 30, 48 on either side. In a second embodiment, the wear strips are thin, narrow rubber strips 72 imposed between adjacent cord fabric breaker layers 56, 60, 64, 68. In a third embodiment, the wear strips are narrow cord fabric strips 92 imposed between adjacent cord fabric layers 80, 84, 88.
摘要翻译： PCT No.PCT / US96 / 15891 Sec。 371日期：1998年11月30日 102（e）1998年11月30日日期PCT 1996年10月4日PCT PCT。公开号WO98 / 14337 日期：1998年4月9日提供了用于飞机着陆应用的充气轮胎10。轮胎包括具有周向延伸的绳索织物层和耐磨条以提高性能的断路器组件20,20A，20B。在一个实施例中，磨损条是橡胶，并且被设置为具有两侧的帘线织物延伸部30,48的破碎层24,40的中心部分26,44。在第二实施例中，耐磨条是施加在相邻的帘线织物断层层56,60,64,68之间的薄而窄的橡胶条72.在第三实施例中，耐磨条是施加在相邻帘布层之间的窄帘布条带92 80，84，88。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式