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    Air turbine starter with unitary inlet and stator
    1.
    发明申请
    Air turbine starter with unitary inlet and stator 有权
    具有整体入口和定子的空气涡轮起动器

    公开(公告)号：US20050058542A1

    公开(公告)日：2005-03-17

    申请号：US10661312

    申请日：2003-09-12

    申请人： Roy Kruegel ,  Cynthia Byers ,  Gary Armstrong ,  Todd Langston ,  Marvin Collins

    发明人： Roy Kruegel ,  Cynthia Byers ,  Gary Armstrong ,  Todd Langston ,  Marvin Collins

    IPC分类号： F01D1/02

    CPC分类号： F02C7/277 ,  Y02T50/671 ,  Y10T29/4932

    摘要： An air turbine starter for use in aircraft or other gas turbine engine applications. In a particular embodiment, the air turbine starter has a titanium unitary inlet structure. The unitary inlet structure has a housing having a longitudinal centerline. The housing defines an air inlet, a mounting surface, and a flow path therebetween. Integrally formed inside the housing and transverse to the longitudinal centerline is a stator for directing the flow of air in to the turbine blades of the turbine starter. The stator has a central circular body with a plurality of angularly spaced circumferentially mounted stator fins. An improved unitary inlet structure and method for making such a unitary inlet and stator are also provided.

    摘要翻译： 用于飞机或其他燃气涡轮发动机应用的空气涡轮起动器。 在特定实施例中，空气涡轮起动器具有钛单一入口结构。 整体入口结构具有纵向中心线的壳体。 壳体限定空气入口，安装表面和它们之间的流动路径。 整体地形成在壳体内部并且横向于纵向中心线的是用于将空气流引导到涡轮启动器的涡轮机叶片的定子。 定子具有中心圆形体，其具有多个角度间隔开的周向安装的定子翅片。 还提供了改进的单一入口结构和制造这种单一入口和定子的方法。

    Aircraft engine accessory drive air film riding bulkhead seal
    3.
    发明申请
    Aircraft engine accessory drive air film riding bulkhead seal 审中-公开
    飞机发动机附件驱动空气膜乘坐舱壁密封

    公开(公告)号：US20060207834A1

    公开(公告)日：2006-09-21

    申请号：US11072840

    申请日：2005-03-03

    申请人： William Giesler ,  Todd Langston ,  Jennifer Zonneveld ,  David Mathis ,  Cynthia Byers

    发明人： William Giesler ,  Todd Langston ,  Jennifer Zonneveld ,  David Mathis ,  Cynthia Byers

    IPC分类号： F16N7/02

    CPC分类号： F02C7/32 ,  F01D11/04 ,  F01D25/183

    摘要： The present invention provides a lubrication system for supplying lubricant between a first housing and a second housing, where the first and second housings each comprising air and lubricant. In one exemplary embodiment, the system includes a lubricant supply tube, an output shaft, and a seal assembly. The lubricant supply tube extends at least partially through the second housing and is configured to receive a supply of lubricant from the first housing. The output shaft is rotationally mounted within the second housing. The seal assembly is mounted on the output shaft and disposed within the second housing. The seal assembly is configured to pump at least a portion of the air out of the second housing.

    摘要翻译： 本发明提供一种用于在第一壳体和第二壳体之间供应润滑剂的润滑系统，其中第一和第二壳体各自包括空气和润滑剂。 在一个示例性实施例中，系统包括润滑剂供应管，输出轴和密封组件。 润滑剂供应管至少部分地延伸穿过第二壳体并且构造成从第一壳体接收润滑剂供应。 输出轴旋转地安装在第二壳体内。 密封组件安装在输出轴上并且设置在第二壳体内。 密封组件构造成将至少一部分空气泵出第二壳体。

    Seal assembly for hydraulic pump output shaft
    4.
    发明申请
    Seal assembly for hydraulic pump output shaft 审中-公开
    液压泵输出轴密封组件

    公开(公告)号：US20060188381A1

    公开(公告)日：2006-08-24

    申请号：US11124468

    申请日：2005-05-06

    申请人： Mingfong Hwang ,  Cynthia Byers ,  William Ryan ,  Daniel Birchak

    发明人： Mingfong Hwang ,  Cynthia Byers ,  William Ryan ,  Daniel Birchak

    IPC分类号： F01C1/02

    CPC分类号： F04B1/0448 ,  F04C15/0038

    摘要： A seal assembly for a hydraulic pump is provided. The assembly includes a spacer ring, a rotor having a first side and a second side, the first side engaging the spacer ring, and a spring-loaded face seal having a face in contact with the rotor second side, where the face seal is configured to supply a force against the rotor sufficient to cause the face seal face to sealingly engage the rotor second side.

    摘要翻译： 提供了一种用于液压泵的密封组件。 所述组件包括间隔环，具有第一侧和第二侧的转子，所述第一侧与所述间隔环接合;以及弹簧加载的面密封件，其具有与所述转子第二侧接触的面，所述面密封件被配置 向转子提供足以使面密封面密封地接合转子第二侧的力。