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    Starter Motor Shared Lubrication System
    1.
    发明申请
    Starter Motor Shared Lubrication System 审中-公开
    起动马达共享润滑系统

    公开(公告)号：US20140250914A1

    公开(公告)日：2014-09-11

    申请号：US13792567

    申请日：2013-03-11

    Applicant: HAMILTON SUNDSTRAND CORPORATION

    Inventor： Matthew Slayter ,  Jeffrey M. Makulec ,  Jeffrey A. Stadler

    IPC: F02C7/26

    CPC classification number: F02C7/277 ,  F05D2260/6022 ,  F05D2260/98

    Abstract: A starter motor has a housing. The housing receives the starter motor and a plurality of locations to receive lubricant. The lubricant supply system shares a lubricant source with a main gas turbine engine to be started by the starter motor. The lubricant supply system has a shutoff valve. The shutoff valve is opened when starter motor is being driven to start a main gas turbine engine. The shutoff valve is generally closed once the main gas turbine engine is started.

    Abstract translation: 起动马达具有外壳。 壳体接收起动电动机和多个位置以接收润滑剂。 润滑剂供应系统与主燃气涡轮发动机共享润滑源，由起动马达启动。 润滑剂供应系统具有截止阀。 当启动电机被驱动以启动主燃气轮机时，截止阀打开。 一旦主燃气涡轮发动机启动，截止阀通常是关闭的。

    AIR TURBINE STARTER
    2.
    发明申请
    AIR TURBINE STARTER 有权
    空气涡轮起动器

    公开(公告)号：US20130022454A1

    公开(公告)日：2013-01-24

    申请号：US13628418

    申请日：2012-09-27

    Applicant: HAMILTON SUNDSTRAND CORPORATION

    Inventor： David J. Zawilinski ,  Jeffrey M. Makulec ,  Bradley Thomas Ryan ,  Matthew Slayter

    IPC: F01D1/02 ,  F01D5/14

    CPC classification number: F01D5/141 ,  F01D5/143 ,  F02C7/277 ,  F05D2250/74 ,  Y02T50/671 ,  Y02T50/673

    Abstract: 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 Z-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, and the Z-coordinate is a radial direction between an airfoil root and an airfoil tip.

    Abstract translation: 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Z坐标限定。 X坐标是切线方向，Z坐标是翼型根和翼型端之间的径向方向。

    Air turbine starter
    4.
    发明授权
    Air turbine starter 有权
    空气涡轮起动器

    公开(公告)号：US08672638B2

    公开(公告)日：2014-03-18

    申请号：US13628418

    申请日：2012-09-27

    Applicant: Hamilton Sundstrand Corporation

    Inventor： David J. Zawilinski ,  Jeffrey M. Makulec ,  Bradley Thomas Ryan ,  Matthew Slayter

    IPC: F01D5/14

    CPC classification number: F01D5/141 ,  F01D5/143 ,  F02C7/277 ,  F05D2250/74 ,  Y02T50/671 ,  Y02T50/673

    Abstract: 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 Z-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, and the Z-coordinate is a axial direction between the leading edge and the trailing edge.

    Abstract translation: 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Z坐标限定。 X坐标是切线方向，Z坐标是前缘和后缘之间的轴向方向。

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