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1. 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。

2. 发明申请

US20050075769A1 Aircraft accessory monitor 失效
标题翻译：飞机附件监视器
公开(公告)号：US20050075769A1
公开(公告)日：2005-04-07
申请号：US10677567
申请日：2003-10-01
申请人： David Eschborn , Paul Evans , Casey Hanlon , Calvin Potter , Glenn Lane , Gary Farnsworth , Louie Gaines , David Mathis
发明人： David Eschborn , Paul Evans , Casey Hanlon , Calvin Potter , Glenn Lane , Gary Farnsworth , Louie Gaines , David Mathis
IPC分类号： G05B23/02 , G07C5/00 , G07C5/08 , G06F7/00
CPC分类号： G05B23/0254 , G07C5/008 , G07C5/0825 , G07C5/0858
摘要： Methods and apparatus are provided for monitoring an aircraft accessory. The apparatus comprises a processor associated with said aircraft accessory, a transducer coupled to said processor and operable to produce parametric data relating to said aircraft accessory and a memory coupled to said processor having baseline parametric data residing therein, wherein said baseline parametric data comprises the parametric data obtained during an acceptance test procedure. The method comprises installing a transducer configured to produce parametric data relating to said aircraft accessory, coupling said transducer to a processor associated with said aircraft accessory, coupling said processor to a memory associated with said aircraft accessory, recording baseline parametric data relating to said aircraft accessory in said memory during an acceptance test procedure for said aircraft accessory.
摘要翻译：提供了用于监视飞行器附件的方法和装置。所述设备包括与所述飞行器附件相关联的处理器，耦合到所述处理器并可操作以产生与所述飞行器附件相关的参数数据的传感器和耦合到所述处理器的存储器，其中驻留有驻留参考数据的基准参数数据，其中所述基准参数数据包括参数在验收测试程序中获得的数据。该方法包括安装一个被配置成产生与所述飞行器附件相关的参数数据的换能器，将所述换能器耦合到与所述飞机附件相关联的处理器，将所述处理器耦合到与所述飞行器附件相关联的存储器，记录与所述飞机附件相关的基准参数数据在所述飞机附件的验收测试程序期间在所述存储器中。

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