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    Bevel gear for gearbox
    1.
    发明授权
    Bevel gear for gearbox 有权
    齿轮减速齿轮

    公开(公告)号：US08950284B2

    公开(公告)日：2015-02-10

    申请号：US13408215

    申请日：2012-02-29

    申请人： Matthew Slayter

    发明人： Matthew Slayter

    IPC分类号： F16H1/14 ,  F16H55/08

    CPC分类号： F16H55/0846 ,  F16H55/17 ,  Y10T29/49464 ,  Y10T74/19665 ,  Y10T74/19958

    摘要： A gear set is provided for use in a gearbox. The gear set includes a first bevel gear having a first rotational axis and a second bevel gear having a second rotational axis. The second gear is driven by the first gear. The first gear has an outside diameter of about 3.1956 inches, an outer cone distance of about 2.1044 inches, a face width of about 0.62 inches, and a ratio of the outside diameter to a length parallel to the axis of rotation between the crown and the pitch apex of about 1.83. The second gear has an outside diameter of about 2.8337 inches, an outer cone distance of about 2.1044 inches, a face width of about 0.62 inches, and a ratio of the outside diameter to a length parallel to the axis of rotation between the crown and the pitch apex of about 2.33.

    摘要翻译： 齿轮组提供用于齿轮箱。 齿轮组包括具有第一旋转轴线的第一锥齿轮和具有第二旋转轴线的第二锥齿轮。 第二档由第一档驱动。 第一档具有大约3.1956英寸的外径，大约2.1044英寸的外锥距离，大约0.62英寸的面宽度，以及外径与平行于表冠之间的旋转轴线的长度的比率 顶点约1.83。 第二齿轮具有大约2.8337英寸的外径，大约2.1044英寸的外锥体距离，约0.62英寸的面宽度，以及外径与平行于表冠和表面之间的旋转轴线的长度的比率 节距为2.33左右。

    Air turbine starter turbine blade airfoil
    2.
    发明授权
    Air turbine starter turbine blade airfoil 有权
    涡轮起动器涡轮机叶片翼型

    公开(公告)号：US08672637B2

    公开(公告)日：2014-03-18

    申请号：US12858399

    申请日：2010-08-17

    申请人： David J. Zawilinski ,  Jeffrey M. Makulec ,  Matthew Slayter

    发明人： David J. Zawilinski ,  Jeffrey M. Makulec ,  Matthew Slayter

    IPC分类号： F01D5/14

    CPC分类号： F01D5/141 ,  F02C7/277 ,  F05D2250/74 ,  Y02T50/671 ,  Y02T50/673

    摘要： A blade profile section for an Air Turbine Starter includes an airfoil which defines an airfoil profile section through a leading edge and a trailing edge. The airfoil profile section is defined by a set of X-coordinates and Y-coordinates defined in any of Table I, Table II, Table III or Table IV scaled by a desired factor. The X-coordinate is the tangential direction, the Y-coordinate is the axial direction, and the Z-coordinate is a radial direction between an airfoil root and an airfoil tip.

    摘要翻译： 用于空气涡轮起动器的叶片轮廓部分包括翼型件，其限定通过前缘和后缘的翼型轮廓部分。 机翼轮廓部分由按照期望因子缩放的表I，表II，表III或表IV中任一个中定义的一组X坐标和Y坐标限定。 X坐标是切线方向，Y坐标是轴向，Z坐标是翼型根和翼型端之间的径向方向。

    AIR TURBINE STARTER TURBINE BLADE AIRFOIL
    4.
    发明申请
    AIR TURBINE STARTER TURBINE BLADE AIRFOIL 有权
    空气涡轮起动器涡轮叶片飞行器

    公开(公告)号：US20120045342A1

    公开(公告)日：2012-02-23

    申请号：US12858399

    申请日：2010-08-17

    申请人： David J. Zawilinski ,  Jeffrey M. Makulec ,  Matthew Slayter

    发明人： David J. Zawilinski ,  Jeffrey M. Makulec ,  Matthew Slayter

    IPC分类号： F01D5/14 ,  B23P15/04

    CPC分类号： F01D5/141 ,  F02C7/277 ,  F05D2250/74 ,  Y02T50/671 ,  Y02T50/673

    摘要： A blade profile section for an Air Turbine Starter includes an airfoil which defines an airfoil profile section through a leading edge and a trailing edge. The airfoil profile section is defined by a set of X-coordinates and Y-coordinates defined in any of Table I, Table II, Table III or Table IV scaled by a desired factor. The X-coordinate is the tangential direction, the Y-coordinate is the axial direction, and the Z-coordinate is a radial direction between an airfoil root and an airfoil tip.

    摘要翻译： 用于空气涡轮起动器的叶片轮廓部分包括翼型件，其限定通过前缘和后缘的翼型轮廓部分。 机翼轮廓部分由按照期望因子缩放的表I，表II，表III或表IV中任一个中定义的一组X坐标和Y坐标限定。 X坐标是切线方向，Y坐标是轴向，Z坐标是翼型根和翼型端之间的径向方向。

    SYSTEM AND METHOD FOR CLEARING CHIPS FROM A MAGNETIC CHIP COLLECTOR
    7.
    发明申请
    SYSTEM AND METHOD FOR CLEARING CHIPS FROM A MAGNETIC CHIP COLLECTOR 审中-公开
    用于从磁性芯片收集器中清除晶片的系统和方法

    公开(公告)号：US20140124449A1

    公开(公告)日：2014-05-08

    申请号：US13668983

    申请日：2012-11-05

    申请人： Matthew Slayter ,  Jeffrey M. Makulec

    发明人： Matthew Slayter ,  Jeffrey M. Makulec

    IPC分类号： B03C1/02

    CPC分类号： B03C1/0332 ,  B03C1/284 ,  B03C1/286 ,  B03C2201/18 ,  B03C2201/28

    摘要： A chip collector body is provided including a coupled base and elongate member. The base and elongate member have a substantially hollow interior extending from a first end to a second end, so as to form a shell. A collector element is positioned within the hollow interior. The collector element has a magnetic element positioned adjacent the second end and a flange positioned near the first end. The collector element is configured to move between a first position and a second position to selectively demagnetize the chip collector body. An axial biasing member is positioned between the flange of the collector element and a rigid surface. The axial biasing member is configured to bias the collector element into the first position.

    摘要翻译： 提供了一种芯片收集器本体，其包括联接的底座和细长构件。 基部和细长构件具有从第一端延伸到第二端的基本上中空的内部，从而形成外壳。 收集器元件位于中空内部。 集电器元件具有邻近第二端定位的磁性元件和位于第一端附近的凸缘。 集电体元件构造成在第一位置和第二位置之间移动，以选择性地使集电体本体去磁。 轴向偏置构件位于收集器元件的凸缘和刚性表面之间。 轴向偏置构件构造成将收集器元件偏置到第一位置。

    Methods for cluster gear timing and manufacturing
    8.
    发明授权
    Methods for cluster gear timing and manufacturing 有权
    集群齿轮定时和制造方法

    公开(公告)号：US08613142B2

    公开(公告)日：2013-12-24

    申请号：US12847448

    申请日：2010-07-30

    申请人： Matthew Slayter ,  Charles E. Long

    发明人： Matthew Slayter ,  Charles E. Long

    IPC分类号： B21D53/28

    CPC分类号： B23F17/00 ,  F02C7/275 ,  F02C7/36 ,  F16H1/46 ,  F16H1/48

    摘要： A method of manufacturing a gear cluster from a first gear body and a second gear body comprises producing a first set of gear teeth on the first gear body such that each tooth on the first set of gear teeth has a first pitch point. The second gear body is axially aligned with the first gear body. A timing position for a second set of gear teeth on the second gear body is determined by dimensioning from the first set of gear teeth. A second set of gear teeth on the second gear body is produced based on the timing position and each tooth on the second set of gear teeth has a second pitch point. The gear cluster is inspected for timing position by measuring a reference dimension between the first pitch point and the second pitch point.

    摘要翻译： 一种从第一齿轮体和第二齿轮体制造齿轮组的方法包括在第一齿轮体上产生第一组齿轮齿，使得第一组齿轮齿上的每个齿具有第一节距点。 第二齿轮体与第一齿轮体轴向对准。 通过从第一组齿轮齿的尺寸确定第二齿轮体上的第二组齿轮齿的定时位置。 基于定时位置产生第二齿轮体上的第二组齿轮齿，并且第二组齿轮齿上的每个齿具有第二节距点。 通过测量第一节距点和第二节距点之间的参考尺寸来检查齿轮组的定时位置。

    LUBRICATION MANAGEMENT SYSTEM FOR A ROTATING SHAFT ASSEMBLY AND METHOD OF FORMING
    9.
    发明申请
    LUBRICATION MANAGEMENT SYSTEM FOR A ROTATING SHAFT ASSEMBLY AND METHOD OF FORMING 审中-公开
    旋转轴组件的润滑管理系统及其形成方法

    公开(公告)号：US20130267331A1

    公开(公告)日：2013-10-10

    申请号：US13441174

    申请日：2012-04-06

    申请人： William C. Trommer ,  Michael R. Blewett ,  Matthew Slayter

    发明人： William C. Trommer ,  Michael R. Blewett ,  Matthew Slayter

    IPC分类号： F01M11/00 ,  F16N1/00 ,  B23P11/00 ,  F16C3/02

    CPC分类号： F16H57/0427 ,  Y10T29/49881

    摘要： A lubrication management system for a rotating shaft assembly includes a shaft rotatable about a central axis and in operable connection with at least one component, wherein lubrication is supplied proximate an outer diameter of the shaft. Also included is a lubrication manipulation device for directing the lubrication radially away from the outer diameter of the shaft, wherein the lubrication manipulation device comprises a threaded portion for fixedly securing the lubrication manipulation device to the outer diameter of the shaft.

    摘要翻译： 用于旋转轴组件的润滑管理系统包括可围绕中心轴线旋转并且与至少一个部件可操作地连接的轴，其中在轴的外径附近提供润滑。 还包括一种润滑操纵装置，用于将润滑剂从径向远离轴的外径引导，其中润滑操纵装置包括用于将润滑操纵装置固定地固定到轴的外径的螺纹部分。