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    Device and method for adjusting post-spacer height in production of liquid crystal displays
    5.
    发明授权
    Device and method for adjusting post-spacer height in production of liquid crystal displays 有权
    用于调节液晶显示​​器生产中后隔垫高度的装置和方法

    公开(公告)号：US09381682B2

    公开(公告)日：2016-07-05

    申请号：US14117208

    申请日：2012-12-18

    申请人： BEIJING BOE OPTOELECTRONICS TECHNOLOGY CO., LTD.

    发明人： Chengtan Zhao ,  Tae Yup Min ,  Xu Chen ,  Hui Li ,  Weixin Meng ,  Lang Zhang

    IPC分类号： B29C37/00 ,  H01L21/02 ,  G02F1/1339 ,  B29L7/00

    CPC分类号： B29C37/005 ,  B29L2007/00 ,  G02F1/13394 ,  G02F2201/503 ,  H01L21/02656

    摘要： A device and a method for adjusting post-spacer height in production of liquid crystal displays (LCDs), and the device comprises a controller (11) and an extrusion panel (12), the controller (1) is configured to control the extrusion panel (12) to perform plastic deformation treatment; and the extrusion panel (12) is configured to perform plastic deformation treatment on post spacers on a substrate, of which a height is more than a predetermined height value, under the control of the controller (11) after a rubbing process and before a cell assembly process, so that the standard deviation of the post-spacer height on the substrate can fall in a range of the predetermined standard deviation required to be achieved by products. The device and the method can effectively improve the uniformity of the post-spacer height on the substrates.

    摘要翻译： 一种用于调节液晶显示​​器（LCD）生产中的后隔间高度的装置和方法，并且该装置包括控制器（11）和挤出板（12），该控制器（1）构造成控制挤压板 （12）进行塑性变形处理; 并且所述挤出面板（12）被配置为在摩擦处理之后和在电池单元之前在控制器（11）的控制下对基板上的高度大于预定高度值的支柱间隔件进行塑性变形处理 组装过程，使得衬底上的后隔垫高度的标准偏差可以落在产品所需的预定标准偏差的范围内。 该装置和方法可以有效地提高基片上后隔垫高度的均匀性。

    Shape-distorting tooling system and method for curing composite parts
    6.
    发明授权
    Shape-distorting tooling system and method for curing composite parts 有权
    形状变形工具系统和固化复合零件的方法

    公开(公告)号：US08986484B2

    公开(公告)日：2015-03-24

    申请号：US13649013

    申请日：2012-10-10

    申请人： The Boeing Company

    发明人： Robert T. Loftus, Jr. ,  Jason M. Robinson ,  Mitchell J. Lee

    IPC分类号： B29C35/02 ,  B29C35/00 ,  B29C37/00 ,  B29C70/44 ,  B29C33/38 ,  B29L31/08

    CPC分类号： B29C33/3828 ,  B29C33/38 ,  B29C35/002 ,  B29C35/02 ,  B29C37/005 ,  B29C70/446 ,  B29K2995/0012 ,  B29K2995/0013 ,  B29L2031/082 ,  Y10T156/1002

    摘要： A tooling system may include a cure tool and a biasing element. The cure tool may have a cure tool coefficient of thermal expansion (CTE) and may be configured for curing a composite article formed of two or more components having dissimilar component CTEs. The biasing element may be fixedly attached to the cure tool and has a biasing element CTE that may be different than the cure tool CTE. The biasing element may be configured such that a combination of the cure tool CTE and the biasing element CTE causes a heat-up displacement in the cure tool when heated and the composite article is cured in a distorted shape. When the cured composite article is cooled, the cured composite article may substantially assume an as-designed shape.

    摘要翻译： 工具系统可以包括固化工具和偏置元件。 固化工具可以具有固化工具的热膨胀系数（CTE），并且可以被配置用于固化由具有不同组分CTE的两个或更多个组分形成的复合制品。 偏置元件可以固定地附接到固化工具，并且具有可以与固化工具CTE不同的偏置元件CTE。 偏置元件可以被构造成使得固化工具CTE和偏置元件CTE的组合在加热时在固化工具中引起加热位移，并且复合制品以变形的形状固化。 当固化的复合制品被冷却时，固化的复合制品可以基本上呈现为设计形状。

    Systems and Methods for Fabricating Hybrid Rocket Fuel Motor Fuel Grains
    7.
    发明申请
    Systems and Methods for Fabricating Hybrid Rocket Fuel Motor Fuel Grains 审中-公开
    混合火箭燃料电机燃料颗粒的制造和方法

    公开(公告)号：US20130042596A1

    公开(公告)日：2013-02-21

    申请号：US13564445

    申请日：2012-08-01

    申请人： Jerome Keith Fuller

    发明人： Jerome Keith Fuller

    IPC分类号： F02K9/18 ,  B05C5/02 ,  B05D7/24

    CPC分类号： F02K9/18 ,  B29C37/005 ,  B29C64/106 ,  B29L2031/3097 ,  B33Y30/00 ,  B33Y80/00 ,  C06B21/005 ,  C06B21/0083 ,  C06B45/00

    摘要： Embodiments of the invention relate to systems and methods for fabricating hybrid rocket motor fuel grains. In one embodiment, a method for fabricating a rocket motor fuel grain can be provided. The method can include providing a platform operable to support a rocket motor fuel grain during fabrication. The method can also include disposing at least one fuel material onto the platform to form a material layer. Further, the method can include successively disposing additional fuel material onto the material layer in small amounts, wherein the rocket motor fuel grain is formed on the platform.

    摘要翻译： 本发明的实施例涉及用于制造混合火箭发动机燃料颗粒的系统和方法。 在一个实施例中，可以提供一种用于制造火箭发动机燃料颗粒的方法。 该方法可以包括在制造期间提供可操作以支撑火箭发动机燃料颗粒的平台。 该方法还可以包括将至少一种燃料材料设置在平台上以形成材料层。 此外，该方法可以包括以少量连续地将附加燃料材料布置在材料层上，其中在平台上形成火箭发动机燃料颗粒。

    Method of manufacturing a carbon-carbon brake disc
    9.
    发明授权
    Method of manufacturing a carbon-carbon brake disc 有权
    制造碳碳制动盘的方法

    公开(公告)号：US08105511B2

    公开(公告)日：2012-01-31

    申请号：US12213235

    申请日：2008-06-17

    申请人： Allen H. Simpson ,  Mark L. La Forest ,  Slawomir T. Fryska ,  Barry P. Soos

    发明人： Allen H. Simpson ,  Mark L. La Forest ,  Slawomir T. Fryska ,  Barry P. Soos

    IPC分类号： C01B31/00

    CPC分类号： B29C33/0011 ,  B29C31/008 ,  B29C37/005 ,  B29C71/02 ,  B29L2031/7482

    摘要： A method of manufacturing a carbon-carbon brake disc uses a restraint fixture (12) that includes a preform retention region configured to limit contracting forces applied against a preform (10) in the preform retention region when the restraint fixture (12) thermally contracts. In one embodiment, the restraint fixture (12) comprises a band (12) having a first surface defining the preform retention region and a first expansion portion (26, 28, 29) adapted to deform upon application of a force to the band (12).

    摘要翻译： 制造碳碳制动盘的方法使用约束固定装置（12），所述约束装置包括预制件保持区域，所述预制件保持区域被构造成当所述约束装置（12）热收缩时限制在所述预成型件保持区域中施加的预成型件（10）的收缩力。 在一个实施例中，约束固定件（12）包括具有限定预成型件保持区域的第一表面的带（12）和适于在对带（12）施加力时变形的第一膨胀部分（26,28,29） ）。

    Method for forming composite components and tool for use therein
    10.
    发明授权
    Method for forming composite components and tool for use therein 有权

    公开(公告)号：US07922957B2

    公开(公告)日：2011-04-12

    申请号：US12213931

    申请日：2008-06-26

    申请人： Simon Astwood ,  Steven Evans

    发明人： Simon Astwood ,  Steven Evans

    IPC分类号： B29C70/44

    CPC分类号： B29C37/005 ,  B29C70/446

    摘要： A method of making an aircraft component is provided, wherein the method comprises the steps of:providing a mould (1) for the receipt of a material (3) from which the aircraft component is to be made providing the mould with said material providing an intensification tool (14) in spaced relationship to the mould and heating the material, tool and mould so that the tool expands and applies pressure to the material and so as to form the component andwherein the linear coefficient of thermal expansion of the tool in a first direction is matched to the coefficient of thermal expansion of the component in the first direction, and the coefficient of thermal expansion of the tool in a second direction is greater than the coefficient of thermal expansion of the component in the second direction, the tool being provided with at least one contacting surface for contacting the material and through which pressure is applied to the material, the expansion of the tool in the second direction causing the at least one contacting surface to contact, and exert pressure on, the material.