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    Wing Foil Bearings and Methods of Manufacturing Same
    2.
    发明申请
    Wing Foil Bearings and Methods of Manufacturing Same 审中-公开
    翼箔轴承及其制造方法相同

    公开(公告)号：US20160208848A1

    公开(公告)日：2016-07-21

    申请号：US14914981

    申请日：2014-09-10

    申请人： XDOT ENGINEERING AND ANALYSIS, PLLC

    发明人： Erik Swanson ,  Patrick O'Meara

    IPC分类号： F16C17/02 ,  F16C43/02

    CPC分类号： F16C17/024 ,  F16C17/042 ,  F16C27/02 ,  F16C27/04 ,  F16C43/02 ,  F16C2202/08 ,  F16C2220/68 ,  F16C2220/82 ,  F16F1/028 ,  Y10T29/49705

    摘要： A wing foil bearing may include one or more wing or tab foil layers. A tab foil layer may comprise a thin material with a two-dimensional array of tab shapes. A tab shape may be defined by a boundary of material separated from the thin material and having an integral edge and a free edge. Tab shapes may include one or more free-state bends relative to the thin material, forming a two-dimensional array of cantilever wings or tabs. Tab arrays may be one or more of various types or two-dimensional arrays, and a tab foil layer may include additional tab arrays and tabs. One or more tab foil layers may be engaged with a mounting surface layer and a counter-surface layer to form a wing foil bearing. Tab foil layers may be stacked and or nested, including partial nesting and complete nesting.

    摘要翻译： 翼箔轴承可以包括一个或多个翼片或翼片箔层。 凸片箔层可以包括具有凸片形状的二维阵列的薄材料。 突片形状可以由与薄材料分离并且具有整体边缘和自由边缘的材料的边界限定。 突片形状可以包括相对于薄材料的一个或多个自由状态弯曲，形成悬臂翼或翼片的二​​维阵列。 标签阵列可以是各种类型或二维阵列中的一种或多种，​​并且突片箔层可以包括附加的标签阵列和突片。 一个或多个凸片箔层可以与安装表面层和相对表面层接合以形成翼片轴承。 标签箔层可以堆叠或嵌套，包括部分嵌套和完全嵌套。

    SHAFT CLAMP ASSEMBLY AND A METHOD OF USING THE SAME
    3.
    发明申请
    SHAFT CLAMP ASSEMBLY AND A METHOD OF USING THE SAME 有权
    轴夹组件及其使用方法

    公开(公告)号：US20150275978A1

    公开(公告)日：2015-10-01

    申请号：US14633660

    申请日：2015-02-27

    申请人： ROLLS-ROYCE PLC

    发明人： Christopher John DURLING

    IPC分类号： F16D1/06 ,  F02C7/06

    CPC分类号： F16D1/06 ,  F01D5/025 ,  F02C7/06 ,  F04D29/266 ,  F16C19/06 ,  F16C35/063 ,  F16C2202/06 ,  F16C2202/08 ,  F16C2202/22 ,  F16C2240/06 ,  F16C2360/23 ,  Y10T29/49959 ,  Y10T403/7069

    摘要： A shaft clamp assembly has first, second and third members. Each member has respective first and opposite second ends, and an annular body extending between the ends. The second member has a radially outwardly extending flange at its first end, and a radially inwardly extending flange at its second end. The third member also has a radially inwardly extending flange at its second end. The first, second and third members are disposed concentrically in sequence, with a threaded portion of the first member being threadingly engaged with a corresponding threaded surface on the shaft, the second end of the first member presses against the second end flange of the second member, the first end flange of the second member presses against the first end of the third member and the second end flange of the third member presses against the object to thereby secure the object to the shaft.

    摘要翻译： 轴夹组件具有第一，第二和第三构件。 每个构件具有相应的第一和相对的第二端，以及在端部之间延伸的环形体。 第二构件在其第一端处具有径向向外延伸的凸缘，在其第二端具有径向向内延伸的凸缘。 第三构件在其第二端还具有径向向内延伸的凸缘。 第一，第二和第三构件按顺序同心设置，第一构件的螺纹部分与轴上的对应的螺纹表面螺纹接合，第一构件的第二端压靠第二构件的第二端部凸缘 第二构件的第一端部凸缘压靠第三构件的第一端并且第三构件的第二端部凸缘压靠在物体上，从而将物体固定到轴上。

    Roller bearing apparatuses including compliant rolling elements, and related methods of manufacture
    7.
    发明授权
    Roller bearing apparatuses including compliant rolling elements, and related methods of manufacture 有权
    包括柔性滚动元件的滚子轴承装置和相关的制造方法

    公开(公告)号：US08939652B2

    公开(公告)日：2015-01-27

    申请号：US13713096

    申请日：2012-12-13

    申请人： US Synthetic Corporation

    发明人： S. Barrett Peterson ,  Craig H Cooley ,  David P Miess

    IPC分类号： F16C33/62 ,  F16C19/22 ,  F16C43/06 ,  F16C33/32 ,  F16C33/34 ,  F16C33/58

    CPC分类号： F16C33/34 ,  F16C17/028 ,  F16C17/047 ,  F16C19/22 ,  F16C21/00 ,  F16C33/32 ,  F16C33/585 ,  F16C33/62 ,  F16C43/06 ,  F16C2202/04 ,  F16C2202/08 ,  F16C2206/04 ,  Y10T29/49684 ,  Y10T29/49689

    摘要： In an embodiment, a roller bearing apparatus may include a rotor having first superhard raceway elements distributed circumferentially about an axis. Each first superhard raceway element includes a raceway surface positioned/configured to form a first portion of a raceway. The apparatus includes a stator including second superhard raceway elements generally opposed to the first superhard raceway elements. Each second superhard raceway element includes a raceway surface positioned/configured to form a second portion of the raceway. The apparatus includes rolling elements interposed between the rotor and stator and positioned and configured to roll on the raceway. One or more of the rolling elements may be configured to elastically deform on the raceway during use. At least a portion of the raceway exhibits a first modulus of elasticity greater than a second modulus of elasticity of at least a portion of the one or more of the rolling elements.

    摘要翻译： 在一个实施例中，滚子轴承装置可以包括具有围绕轴线周向分布的第一超硬轨道元件的转子。 每个第一超硬体滚道元件包括定位/构造成形成滚道的第一部分的滚道表面。 该装置包括定子，其包括通常与第一超硬轨道元件相对的第二超硬轨道元件。 每个第二超硬轨道元件包括定位/配置成形成滚道的第二部分的滚道表面。 该装置包括插入在转子和定子之间的滚动元件，并定位和构造成在滚道上滚动。 一个或多个滚动元件可以被配置为在使用期间在滚道上弹性变形。 滚道的至少一部分呈现出比一个或多个滚动元件的至少一部分的第二弹性模量大的第一弹性模量。

    Wing Foil Bearings and Methods of Manufacturing Same
    8.
    发明申请
    Wing Foil Bearings and Methods of Manufacturing Same 有权
    翼箔轴承及其制造方法相同

    公开(公告)号：US20140376844A1

    公开(公告)日：2014-12-25

    申请号：US14482435

    申请日：2014-09-10

    申请人： Xdot Engineering and Analysis, PLLC

    发明人： Erik E. Swanson ,  Patrick Shawn O'Meara

    IPC分类号： F16C27/02 ,  F16C43/02 ,  F16C23/02

    CPC分类号： F16C17/024 ,  F16C17/042 ,  F16C27/02 ,  F16C27/04 ,  F16C43/02 ,  F16C2202/08 ,  F16C2220/68 ,  F16C2220/82 ,  F16F1/028 ,  Y10T29/49705

    摘要： A wing foil bearing may include one or more wing or tab foil layers. A tab foil layer may comprise a thin material with a two-dimensional array of tab shapes. A tab shape may be defined by a boundary of material separated from the thin material and having an integral edge and a free edge. Tab shapes may include one or more free-state bends relative to the thin material, forming a two-dimensional array of cantilever wings or tabs. Tab arrays may be one or more of various types or two-dimensional arrays, and a tab foil layer may include additional tab arrays and tabs. One or more tab foil layers may be engaged with a mounting surface layer and a counter-surface layer to form a wing foil bearing. Tab foil layers may be stacked and or nested, including partial nesting and complete nesting.

    摘要翻译： 翼箔轴承可以包括一个或多个翼片或翼片箔层。 凸片箔层可以包括具有凸片形状的二维阵列的薄材料。 突片形状可以由与薄材料分离并且具有整体边缘和自由边缘的材料的边界限定。 突片形状可以包括相对于薄材料的一个或多个自由状态弯曲，形成悬臂翼或翼片的二​​维阵列。 标签阵列可以是各种类型或二维阵列中的一种或多种，​​并且突片箔层可以包括附加的标签阵列和突片。 一个或多个凸片箔层可以与安装表面层和相对表面层接合以形成翼片轴承。 标签箔层可以堆叠或嵌套，包括部分嵌套和完全嵌套。