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。

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。

公开(公告)号：US09194295B2

公开(公告)日：2015-11-24

申请号：US13684765

申请日：2012-11-26

Applicant: Hamilton Sundstrand Corporation

Inventor： Matthew Slayter ,  James Vandung Nguyen ,  Jeffrey A. Stadler ,  Timothy A. Johnson

IPC: F01D25/18 ,  F02C7/06 ,  F02C7/32 ,  B60R17/02

CPC classification number: F02C7/06 ,  B60R17/02 ,  F01D25/18 ,  F02C7/32 ,  F05D2260/98

Abstract: A mechanical system has a component to be lubricated that requires greater lubrication at lower speed conditions than would be required at higher speed conditions. A lubricant tower is biased to a position allowing a greater flow of lubrication to the component at lower speed conditions, then moved to a position at higher speed conditions where there is a lesser flow of lubrication.

Abstract translation: 机械系统具有要润滑的部件，在较低速度条件下需要比在较高速度条件下要求更高的润滑。 润滑塔被偏置到允许在较低速度条件下对组件进行更大润滑流动的位置，然后移动到较低流动润滑条件下的位置。

公开(公告)号：US20140144120A1

公开(公告)日：2014-05-29

申请号：US13684765

申请日：2012-11-26

Applicant: HAMILTON SUNDSTRAND CORPORATION

Inventor： Matthew Slayter ,  James Vandung Nguyen ,  Jeffrey A. Stadler ,  Timothy A. Johnson

IPC: F02C7/06

CPC classification number: F02C7/06 ,  B60R17/02 ,  F01D25/18 ,  F02C7/32 ,  F05D2260/98

Abstract: A mechanical system has a component to be lubricated that requires greater lubrication at lower speed conditions than would be required at higher speed conditions. A lubricant tower is biased to a position allowing a greater flow of lubrication to the component at lower speed conditions, then moved to a position at higher speed conditions where there is a lesser flow of lubrication.

Abstract translation: 机械系统具有要润滑的部件，在较低速度条件下需要比在较高速度条件下要求更高的润滑。 润滑塔被偏置到允许在较低速度条件下对组件进行更大润滑流动的位置，然后移动到较低流动润滑条件下的位置。

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。