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21. 发明申请

US20050247529A1 Aircraft brake acuation system including an internally threaded ballscrew actuator assembly 审中-公开
标题翻译：飞机制动系统包括一个内螺纹滚珠丝杠执行器组件
公开(公告)号：US20050247529A1
公开(公告)日：2005-11-10
申请号：US10954822
申请日：2004-09-29
申请人： Louie Gaines , Kellan Geck , James Quitmeyer
发明人： Louie Gaines , Kellan Geck , James Quitmeyer
IPC分类号： F16D55/08 , F16D65/14
CPC分类号： F16D65/18 , F16D2121/24 , F16D2125/40 , F16D2125/48
摘要： An aircraft brake actuation system includes an actuator for selectively supplying a commanded brake force to one or more aircraft wheels. The actuator includes a ballscrew, a ballnut, and a plurality of balls. The ballscrew has a plurality of ball grooves formed on its inner surface, and is coupled to receive a rotational drive force. The ballnut is mounted against rotation, is disposed at least partially within the ballscrew, and includes a plurality of ball grooves formed on its outer surface. The plurality of balls are disposed within the ballnut ball grooves and at least selected ones of the ballscrew ball grooves.
摘要翻译：飞机制动器致动系统包括用于选择性地向一个或多个飞行器轮提供命令的制动力的致动器。致动器包括滚珠丝杠，滚珠丝杠和多个滚珠。滚珠丝杠具有形成在其内表面上的多个球槽，并且被联接以接收旋转驱动力。所述滚珠轴承被安装成防止旋转，至少部分地设置在所述滚珠丝杠内，并且包括在其外表面上形成的多个滚珠槽。所述多个球设置在所述滚珠球槽内和所述滚珠丝杠球槽中的至少一个中。

22. 发明申请

US20050191166A1 Passive improved air turbine starter lubrication system 有权
标题翻译：被动改进的空气涡轮起动器润滑系统
公开(公告)号：US20050191166A1
公开(公告)日：2005-09-01
申请号：US10788757
申请日：2004-02-27
申请人： Gary Farnsworth , Larry Ball , Kellan Geck , Todd Langston
发明人： Gary Farnsworth , Larry Ball , Kellan Geck , Todd Langston
IPC分类号： F01D11/00 , F01D25/18 , F02C7/277
CPC分类号： F01D25/183 , F02C7/277 , Y02T50/672 , Y10T137/7891
摘要： A passive ATS lubrication system is provided that includes a starter housing, a receptacle and two valves. The starter housing is adapted to couple to a gearbox assembly and includes a supply opening and an exhaust opening that are each configured to provide fluid communication between the gearbox assembly and the starter housing. The receptacle is coupled to the starter housing proximate the supply opening to thereby define a reservoir. The first valve is disposed within the reservoir and configured to open or close the supply opening in response to a pressure differential between the starter housing and the gearbox assembly. The second valve is coupled to the starter housing proximate to the exhaust opening and configured to open or close the exhaust opening in response to the pressure differential between the starter housing and the gearbox assembly.
摘要翻译：提供了一种被动ATS润滑系统，其包括起动器壳体，容器和两个阀。起动器壳体适于联接到齿轮箱组件，并且包括供给开口和排气开口，每个构造成用于在齿轮箱组件和起动器壳体之间提供流体连通。容器在靠近供应开口处联接到起动器壳体，从而限定储存器。第一阀设置在储存器内并且构造成响应于起动器壳体和齿轮箱组件之间的压差而打开或关闭供给开口。第二阀联接到起动器壳体，靠近排气开口并且构造成响应于起动器壳体和变速箱组件之间的压力差而打开或关闭排气口。

23. 发明授权

US06681579B2 Air turbine starter with fluid flow control 有权
标题翻译：具有流体流量控制的空气涡轮起动器
公开(公告)号：US06681579B2
公开(公告)日：2004-01-27
申请号：US10071175
申请日：2002-02-07
申请人： Glenn H. Lane , Gary A. Farnsworth , Gerhard Schroeder , Kellan Geck
发明人： Glenn H. Lane , Gary A. Farnsworth , Gerhard Schroeder , Kellan Geck
IPC分类号： F02C7277
CPC分类号： F01D25/18 , F02C7/277 , F05D2260/85 , F05D2300/2283 , Y02T50/671
摘要： An improved air turbine starter that includes fluid flow control devices. The devices may be check valves, for example normally open check valves. The check valves may be located in fluid flow paths between the starter and the gearbox to which it is mounted. The starter may also include a ring seal about the output shaft to restrict fluid flow over the shaft.
摘要翻译：一种改进的涡轮起动器，包括流体流量控制装置。这些装置可以是止回阀，例如常开止回阀。止回阀可以位于起动器和其所安装的齿轮箱之间的流体流动路径中。起动器还可以包括围绕输出轴的环形密封件，以限制流体在轴上的流动。

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