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1. 发明授权

US09341233B2 V-ribbed belt and method for manufacturing same 有权
标题翻译： V型肋带及其制造方法
公开(公告)号：US09341233B2
公开(公告)日：2016-05-17
申请号：US14460042
申请日：2014-08-14
申请人： THE GATES CORPORATION
发明人： Masahiro Mori , Min Gao , Lance C. Hall , Shawn Xiang Wu
IPC分类号： F16G5/08 , B29D29/08 , B29D29/10 , F16G5/20 , D03D1/00 , D03D3/02 , D03D15/00 , D03D15/08 , D04B1/22 , B29L29/00
CPC分类号： F16G5/08 , B29D29/08 , B29D29/103 , B29L2029/00 , D03D1/0094 , D03D3/02 , D03D15/0077 , D03D15/08 , D04B1/225 , D10B2201/02 , D10B2201/04 , D10B2201/06 , D10B2331/02 , D10B2331/10 , D10B2403/0312 , D10B2505/02 , F16G5/20 , Y10S264/57 , Y10S264/73 , Y10S264/77 , Y10T156/1041
摘要： A V-ribbed belt that includes a ribbed surface covered with fabric is provided. The fabric is stretchable in two predetermined directions. A method for manufacturing the V-ribbed belt is also provided. The method includes placing a belt matrix about a mandrel, placing a fabric about the external circumference of the belt matrix which wraps around the mandrel, placing the mandrel inside a shell having a plurality of grooves on the internal circumference, expanding the belt matrix and the fabric toward the internal circumference of the shell and thus pressing the fabric onto the internal circumference having the multi-ribbed structure, and curing the belt matrix with the fabric. The fabric is stretchable to accommodate itself to the multi-ribbed structure.
摘要翻译：提供了一种V形带状带，其包括被织物覆盖的肋状表面。织物在两个预定方向上是可拉伸的。还提供了一种用于制造V形肋带的方法。该方法包括将带状基体围绕心轴放置，将织物围绕围绕心轴的带矩阵的外圆周放置，将心轴放置在内圆周上具有多个凹槽的壳体中，使带状基体和织物朝向壳体的内周，从而将织物压到具有多肋结构的内圆周上，并使织物与带状基体固化。织物是可拉伸的以适应多肋结构。

2. 发明申请

US20140135161A1 V-Ribbed Belt and Method for Manufacturing Same 有权
标题翻译： V型罗带及其制造方法
公开(公告)号：US20140135161A1
公开(公告)日：2014-05-15
申请号：US14159132
申请日：2014-01-20
申请人： The Gates Corporation
发明人： Masahiro Mori , Min Gao , Lance C. Hall , Shawn Xiang Wu
IPC分类号： F16G5/20
CPC分类号： F16G5/08 , B29D29/08 , B29D29/103 , B29L2029/00 , D03D1/0094 , D03D3/02 , D03D15/0077 , D03D15/08 , D04B1/225 , D10B2201/02 , D10B2201/04 , D10B2201/06 , D10B2331/02 , D10B2331/10 , D10B2403/0312 , D10B2505/02 , F16G5/20 , Y10S264/57 , Y10S264/73 , Y10S264/77 , Y10T156/1041
摘要： A V-ribbed belt that includes a ribbed surface covered with fabric is provided. The fabric is stretchable in two predetermined directions. A method for manufacturing the V-ribbed belt is also provided. The method includes placing a belt matrix about a mandrel, placing a fabric about the external circumference of the belt matrix which wraps around the mandrel, placing the mandrel inside a shell having a plurality of grooves on the internal circumference, expanding the belt matrix and the fabric toward the internal circumference of the shell and thus pressing the fabric onto the internal circumference having the multi-ribbed structure, and curing the belt matrix with the fabric. The fabric is stretchable to accommodate itself to the multi-ribbed structure.
摘要翻译：提供了一种V形带状带，其包括被织物覆盖的肋状表面。织物在两个预定方向上是可拉伸的。还提供了一种用于制造V形肋带的方法。该方法包括将带状基体围绕心轴放置，将织物围绕围绕心轴的带矩阵的外圆周放置，将心轴放置在内圆周上具有多个凹槽的壳体中，使带状基体和织物朝向壳体的内周，从而将织物压到具有多肋结构的内圆周上，并使织物与带状基体固化。织物是可拉伸的以适应多肋结构。

3. 发明申请

US20110297325A1 PROCESS AND APPARATUS FOR PRODUCING COMPOSITE STRUCTURES 有权
标题翻译：生产复合结构的方法和装置
公开(公告)号：US20110297325A1
公开(公告)日：2011-12-08
申请号：US13210483
申请日：2011-08-16
申请人： Mahendra Maheshwari , James Joseph Velten
发明人： Mahendra Maheshwari , James Joseph Velten
IPC分类号： B29C70/00 , B32B38/00
CPC分类号： B29C70/545 , B29C43/027 , B29C43/10 , B29C2043/3655 , B29K2995/0002 , B29L2031/3076 , B29L2031/737 , Y10S264/57 , Y10S264/70 , Y10S264/78 , Y10S425/037 , Y10T156/1028 , Y10T156/1056 , Y10T156/1057 , Y10T156/1062 , Y10T156/1304
摘要： A process and apparatus for producing perforated composite structures, such as acoustic skins suitable for aircraft engine nacelle and duct components. The process includes placing a mat member, a non-impregnated fabric member, and a resin film on a tool surface so that pins disposed on the mat member project through the fabric member and resin film to define holes therein. The fabric member is between the mat member and resin film, and the fabric member and resin film define a stack that conforms to the mat member and tool surface. A caul member is then placed on the stack so that apertures in the caul member are penetrated by the pins. The stack is heated to melt the resin film and cause molten resin to infuse the fabric member and yield a resin-infused fabric stack, after which the molten resin within the resin-infused fabric stack is at least partially cured.
摘要翻译：用于生产穿孔复合结构的方法和设备，例如适用于飞机发动机机舱和管道部件的声学皮肤。该方法包括将垫子，非浸渍的织物构件和树脂膜放置在工具表面上，使得设置在垫构件上的销突出穿过织物构件和树脂膜以在其中限定孔。织物构件在垫材和树脂膜之间，织物和树脂膜限定了与垫材和工具表面一致的叠层。然后将一个止动件放置在堆叠上，使得止动件中的孔被销钉穿透。将该叠层加热熔化树脂膜，使熔融树脂注入织物，并产生树脂输入的织物叠层，此后树脂注入的织物叠层内的熔融树脂至少部分固化。

4. 发明申请

US20100173740A1 V-Ribbed Belt and Method for Manufacturing Same 有权
公开(公告)号：US20100173740A1
公开(公告)日：2010-07-08
申请号：US12722703
申请日：2010-03-12
申请人： Masahiro Mori , Min Gao , Lance C. Hall , Shawn Xiang Wu
发明人： Masahiro Mori , Min Gao , Lance C. Hall , Shawn Xiang Wu
IPC分类号： F16G5/08 , B32B38/06
CPC分类号： F16G5/08 , B29D29/08 , B29D29/103 , B29L2029/00 , D03D1/0094 , D03D3/02 , D03D15/0077 , D03D15/08 , D04B1/225 , D10B2201/02 , D10B2201/04 , D10B2201/06 , D10B2331/02 , D10B2331/10 , D10B2403/0312 , D10B2505/02 , F16G5/20 , Y10S264/57 , Y10S264/73 , Y10S264/77 , Y10T156/1041
摘要： A V-ribbed belt that includes a ribbed surface covered with fabric is provided. The fabric is stretchable in two predetermined directions. A method for manufacturing the V-ribbed belt is also provided. The method includes placing a belt matrix about a mandrel, placing a fabric about the external circumference of the belt matrix which wraps around the mandrel, placing the mandrel inside a shell having a plurality of grooves on the internal circumference, expanding the belt matrix and the fabric toward the internal circumference of the shell and thus pressing the fabric onto the internal circumference having the multi-ribbed structure, and curing the belt matrix with the fabric. The fabric is stretchable to accommodate itself to the multi-ribbed structure.

5. 发明申请

US20100167860A1 V-Ribbed Belt and Method for Manufacturing Same 有权
标题翻译： V型罗带及其制造方法
公开(公告)号：US20100167860A1
公开(公告)日：2010-07-01
申请号：US12722646
申请日：2010-03-12
申请人： Masahiro Mori , Min Gao , Lance C. Hall , Shawn Xiang Wu
发明人： Masahiro Mori , Min Gao , Lance C. Hall , Shawn Xiang Wu
IPC分类号： F16G5/20 , F16G1/28
CPC分类号： F16G5/08 , B29D29/08 , B29D29/103 , B29L2029/00 , D03D1/0094 , D03D3/02 , D03D15/0077 , D03D15/08 , D04B1/225 , D10B2201/02 , D10B2201/04 , D10B2201/06 , D10B2331/02 , D10B2331/10 , D10B2403/0312 , D10B2505/02 , F16G5/20 , Y10S264/57 , Y10S264/73 , Y10S264/77 , Y10T156/1041
摘要： A V-ribbed belt that includes a ribbed surface covered with fabric is provided. The fabric is stretchable in two predetermined directions. A method for manufacturing the V-ribbed belt is also provided. The method includes placing a belt matrix about a mandrel, placing a fabric about the external circumference of the belt matrix which wraps around the mandrel, placing the mandrel inside a shell having a plurality of grooves on the internal circumference, expanding the belt matrix and the fabric toward the internal circumference of the shell and thus pressing the fabric onto the internal circumference having the multi-ribbed structure, and curing the belt matrix with the fabric. The fabric is stretchable to accommodate itself to the multi-ribbed structure.
摘要翻译：提供了一种V形带状带，其包括被织物覆盖的肋状表面。织物在两个预定方向上是可拉伸的。还提供了一种用于制造V形肋带的方法。该方法包括将带状基体围绕心轴放置，将织物围绕围绕心轴的带矩阵的外圆周放置，将心轴放置在内圆周上具有多个凹槽的壳体中，使带状基体和织物朝向壳体的内周，从而将织物压到具有多肋结构的内圆周上，并使织物与带状基体固化。织物是可拉伸的以适应多肋结构。

6. 发明授权

US07008583B1 Process of inlaying a design in a fiberglass article 失效
标题翻译：在玻璃纤维制品中镶嵌设计的过程
公开(公告)号：US07008583B1
公开(公告)日：2006-03-07
申请号：US10424936
申请日：2003-04-29
申请人： Moises Edery , Saul Ariel Raschkovan
发明人： Moises Edery , Saul Ariel Raschkovan
IPC分类号： B29C39/12
CPC分类号： B29C37/0032 , B29C37/006 , B29C37/0067 , B29K2995/002 , B29L2009/00 , B29L2009/005 , Y10S264/57
摘要： A process of inlaying a design in a fiberglass article to provide a decorative article of manufacture. The process comprises applying a first lamina of releasing agent into a mold. Then forming a second lamina of clear gel coat on the first lamina and allowing it to dry. Then forming a third lamina of transparent polyester resin on the second lamina and submerging the design into the third lamina before the third lamina is dry. Then removing air bubbles from the design and the third lamina and allowing the third lamina to dry. Then applying a fourth lamina of curable resin on the third lamina, whereby the fourth lamina is formed substantially from fiberglass of a white pigmentation, and allowing it to dry. Lastly, removing the mold from the first, second, third, and fourth laminas.
摘要翻译：在玻璃纤维制品中嵌入设计以提供装饰制品的过程。该方法包括将第一层脱模剂施加到模具中。然后在第一层上形成透明凝胶涂层的第二层，并使其干燥。然后在第二层上形成透明聚酯树脂的第三层，并在第三层干燥之前将设计浸入第三层。然后从设计和第三层中除去气泡并允许第三层干燥。然后在第三层上施加可固化树脂的第四层，由此第四层基本上由白色色素沉淀的玻璃纤维形成，并使其干燥。最后，将模具从第一，第二，第三和第四层压板上取下。

7. 发明申请

US20030134944A1 Gypsum layered panels containing styrene butadiene latex additive 有权
标题翻译：含有苯乙烯丁二烯胶乳添加剂的石膏层板
公开(公告)号：US20030134944A1
公开(公告)日：2003-07-17
申请号：US10337447
申请日：2003-01-07
发明人： Gopalakrishnan Sethuraman , W. Roy Burke , Amba Ayambem , Richard J. Romanek
IPC分类号： C04B016/02
CPC分类号： C04B24/163 , C04B24/2676 , C04B24/2688 , C04B28/14 , C04B28/145 , C04B2103/0062 , C04B2111/0062 , C08F257/02 , C08F291/00 , C09K8/46 , E04C2/043 , Y02W30/97 , Y10S264/57 , Y10S425/241 , Y10T428/31855 , Y10T428/31938 , C04B24/2641 , C04B24/2652 , C08F212/08 , C08F236/10 , C08F236/06 , C04B18/241 , C04B38/10
摘要： Gypsum wallboard compositions are disclosed which contain functionalized styrene butadiene latex polymers. Methods for the use of the compositions in the manufacture of wallboard panels and sheets is presented.
摘要翻译：公开了含有官能化苯乙烯丁二烯胶乳聚合物的石膏墙板组合物。提出了在制造墙板和板材时使用组合物的方法。

8. 发明授权

US6014317A Chip package mounting structure for controlling warp of electronic assemblies due to thermal expansion effects 失效
标题翻译：用于控制由于热膨胀效应导致的电子组件翘曲的芯片封装安装结构
公开(公告)号：US6014317A
公开(公告)日：2000-01-11
申请号：US40847
申请日：1998-03-18
申请人： Mark F. Sylvester
发明人： Mark F. Sylvester
IPC分类号： H01L23/373 , H01L23/498 , H05K1/02 , H05K1/18 , H05K7/02
CPC分类号： H01L23/3735 , H01L23/49894 , H01L2924/15151 , H05K1/0271 , H05K1/181 , Y10S264/57 , Y10T29/49124 , Y10T29/49128
摘要： A chip package is provided for controlling warp of electronic assemblies. The chip package has a first component mounted on one side of a substrate. The substrate is a multi-layered laminate having a plurality of dielectric layers made of an organic material. The first component has a different coefficient of thermal expansion (CTE) than the substrate. The chip package includes a second component mounted on an opposite side of the substrate in a location substantially opposite the first component. The second component has a CTE that approximately matches the CTE of the first component. The second component tends to generate bending moments that offset distorting bending moments that may otherwise exist in the chip package without the second component.
摘要翻译：提供了用于控制电子组件翘曲的芯片封装。芯片封装具有安装在基板的一侧上的第一部件。基板是具有由有机材料制成的多个电介质层的多层层叠体。第一组分具有不同于底物的热膨胀系数（CTE）。芯片封装包括在基本上与第一部件相对的位置处安装在基板的相对侧上的第二部件。第二组件具有与第一组件的CTE近似匹配的CTE。第二部件倾向于产生弯曲力矩，该弯矩抵消可能存在于芯片封装中而不具有第二部件的扭曲弯矩。

9. 发明授权

US6012303A Eutectic bonding of single crystal components 失效
标题翻译：单晶组分的共晶键合
公开(公告)号：US6012303A
公开(公告)日：2000-01-11
申请号：US872946
申请日：1997-06-11
申请人： Scott R. Axelson , Herbert E. Bates , Joseph M. Collins , Jeremiah J. Fitzgibbon , John W. Locher , Brian J. McAndrews
发明人： Scott R. Axelson , Herbert E. Bates , Joseph M. Collins , Jeremiah J. Fitzgibbon , John W. Locher , Brian J. McAndrews
IPC分类号： B32B9/00 , C04B37/00 , C30B33/06 , H01K1/36
CPC分类号： C30B33/06 , B32B19/00 , C09J5/06 , C30B29/28 , C09J2400/123 , Y10S264/57 , Y10T156/1089 , Y10T156/1093
摘要： The present invention provides for a method and articles produced from this method for eutectically bonding together single crystal elements, such as sapphire, to form a strong bond therebetween which can withstand high temperatures and chemical attack. The eutectic bonding mixture of the present invention can include a Group IIIA compound, such as yttria.
摘要翻译：本发明提供了一种通过该方法制造的方法和制品，用于将诸如蓝宝石之类的单晶元件共晶地结合在一起，以在其间形成能够承受高温和化学侵蚀的强键。本发明的共晶粘合混合物可以包括IIIA族化合物，例如氧化钇。

10. 发明授权

US5900097A Method of fabricating a laminated composite material 失效
标题翻译：叠层复合材料的制造方法
公开(公告)号：US5900097A
公开(公告)日：1999-05-04
申请号：US739790
申请日：1996-10-30
申请人： Dennis P. Brown
发明人： Dennis P. Brown
IPC分类号： B32B7/02 , B32B18/00 , B32B37/14 , B32B31/18 , B32B31/20 , C03C27/00
CPC分类号： B32B37/144 , B32B18/00 , B32B7/02 , B32B2311/00 , B32B2315/02 , C04B2237/32 , C04B2237/40 , Y10S228/903 , Y10S264/36 , Y10S264/57 , Y10T156/1051 , Y10T156/1075
摘要： There is provided a method of fabricating a laminated composite material and laminated composite materials fabricated thereby wherein the method includes the initial step of forming a pre-laminate by overlaying a first layer characterized by a first thermal expansion coefficient and a first ductility parameter with a second layer characterized by a second thermal expansion coefficient and a second ductility parameter. The pre-laminate is heated to a temperature at which the first ductility parameter becomes substantially equivalent in value to the second ductility parameter. The first and second layers of the heated prelaminate are then pressed together, preferably by use of a rolling mill technique, with sufficient compression force to cause the layers to adhere one to the other, thus forming a core laminate. Preferably, the core laminate is divided, either by cutting or folding, into a plurality of divided laminate members. One of the divided laminate members is overlaid onto the other of the divided laminate members to form a laminate stack. The temperature of the laminate stack is then controlled to substantially equalize the first and second ductility parameters in each of the divided laminate members of the laminate stack. The divided laminate members of the laminate stack are then pressed together, preferably by use of a rolling mill technique.
摘要翻译：提供了一种制造层压复合材料和层压复合材料的方法，其中所述方法包括通过将第一热膨胀系数和第一延展性参数表征为特征的第一层与第二层其特征在于第二热膨胀系数和第二延性参数。将预层压体加热到第一延性参数变得与第二延性参数基本上相等的温度。然后将加热的预层压板的第一层和第二层优选地通过使用轧制技术以足够的压缩力压在一起，以使层彼此粘合，从而形成芯层叠体。优选地，将芯层叠体通过切割或折叠分割成多个分开的层叠构件。其中一个分开的层压件被覆在另一个分开的层叠件上，以形成层叠叠层。然后控制层压叠层的温度，以使叠层叠层的每个分层层压构件中的第一和第二延性参数基本相等。然后将叠层叠层叠的分层层压构件压在一起，优选采用轧机技术。

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