Discrete input circuit
    1.
    发明授权
    Discrete input circuit 有权
    离散输入电路

    公开(公告)号:US09355791B2

    公开(公告)日:2016-05-31

    申请号:US13680515

    申请日:2012-11-19

    IPC分类号: H01H1/60

    CPC分类号: H01H1/60 H01H1/605 Y10T307/74

    摘要: Embodiments are directed to a discrete input circuit comprising: a switch, a capacitor coupled to the switch, a first resistor connected in series with the capacitor and coupled to a power supply, and a second resistor coupled to the power supply and the switch, wherein a value of the capacitor, a value of the first resistor, and a value of the second resistor are selected to provide a wetting current from the power supply to the switch when the switch is closed in order to clean contacts associated with the switch.

    摘要翻译: 实施例涉及离散输入电路,包括:开关,耦合到开关的电容器,与电容器串联连接并耦合到电源的第一电阻器,以及耦合到电源和开关的第二电阻器,其中 选择电容器的值,第一电阻器的值和第二电阻器的值以在开关闭合时从电源向开关提供润湿电流,以便清洁与开关相关联的触点。

    Vehicle monitoring system
    2.
    发明授权
    Vehicle monitoring system 有权
    车辆监控系统

    公开(公告)号:US09092029B2

    公开(公告)日:2015-07-28

    申请号:US12427691

    申请日:2009-04-21

    IPC分类号: G05B23/02

    CPC分类号: G05B23/0213

    摘要: An example reconfigurable vehicle monitoring arrangement includes a housing securable relative to a vehicle, a communication base at least partially disposed within the housing, and a universal connector assembly configured to selectively operatively connect the communication base with a plurality of different modules. At least one of the modules is configured to communicate data gathered from a plurality of vehicle data sources to the communication base.

    摘要翻译: 示例性可重构车辆监视装置包括相对于车辆可固定的壳体,至少部分地设置在壳体内的通信基座以及被配置为选择性地将通信基座与多个不同模块连接的通用连接器组件。 至少一个模块被配置为将从多个车辆数据源收集的数据传送到通信基座。

    Dual-pump fuel system and method for starting a gas turbine engine
    4.
    发明授权
    Dual-pump fuel system and method for starting a gas turbine engine 有权
    双泵燃料系统及起动燃气轮机的方法

    公开(公告)号:US08276360B2

    公开(公告)日:2012-10-02

    申请号:US12471092

    申请日:2009-05-22

    IPC分类号: F02C9/00

    摘要: A dual-pump fuel system for use with a gas turbine engine comprises a fuel metering system, a mechanical fuel pump, an electric fuel pump and an engine controller. The fuel metering system is configured to dispense fuel flow to the engine based on operational needs of the gas turbine engine. The mechanical fuel pump is configured to deliver fuel to the metering system dependent on operational speeds of the engine. The electric fuel pump is configured to deliver fuel directly to the engine independent of operation of the engine. The engine controller is connected to the metering system and the electric fuel pump and is configured to cause the electric fuel pump to deliver fuel to the engine to start and operate the engine until the engine operates the mechanical fuel pump to deliver fuel to the metering system sufficient to sustain operation of the engine.

    摘要翻译: 用于燃气涡轮发动机的双泵燃料系统包括燃料计量系统,机械燃料泵,电动燃料泵和发动机控制器。 燃料计量系统被配置为基于燃气涡轮发动机的操作需要将燃料流分配到发动机。 机械燃油泵构造成根据发动机的运行速度将燃料输送到计量系统。 电动燃料泵被配置为直接将燃料直接输送到发动机,而与发动机的运转无关。 发动机控制器连接到计量系统和电动燃料泵,并且被配置为使电动燃料泵将燃料输送到发动机以启动和操作发动机,直到发动机操作机械燃料泵以将燃料输送到计量系统 足以维持发动机的运转。

    Bypass Monitor for Fuel Supply System
    5.
    发明申请
    Bypass Monitor for Fuel Supply System 审中-公开
    燃油供应系统旁路监视器

    公开(公告)号:US20120167594A1

    公开(公告)日:2012-07-05

    申请号:US12984779

    申请日:2011-01-05

    IPC分类号: F02C6/00 G01M3/28

    CPC分类号: F02C9/36

    摘要: A method for monitoring a fuel supply system for a turbine engine, the fuel supply system comprising a fuel pump and a pressure regulation valve configured to receive fuel from an outlet of the fuel pump includes determining by a bypass monitor an amount of bypass flow in a bypass path located between the pressure regulation valve and an inlet of the fuel pump; determining an amount of leakage flow in the fuel supply system by the bypass monitor based on the bypass flow; and determining whether the leakage flow exceeds a predetermined threshold by the bypass monitor, and in the event the leakage flow exceeds the predetermined threshold, indicating a need for maintenance of the fuel supply system.

    摘要翻译: 一种用于监测用于涡轮发动机的燃料供应系统的方法,所述燃料供应系统包括燃料泵和被配置为从所述燃料泵的出口接收燃料的压力调节阀,包括通过旁路监视器确定一个旁路流量 旁路路径位于压力调节阀和燃油泵的入口之间; 基于所述旁路流量,通过所述旁路监视器确定所述燃料供给系统中的泄漏量; 并且通过旁路监视器确定泄漏流量是否超过预定阈值,并且在泄漏流量超过预定阈值的情况下,指示维护燃料供应系统的需要。

    Fan embedded power generator
    6.
    发明授权
    Fan embedded power generator 有权
    风机嵌入式发电机

    公开(公告)号:US08522522B2

    公开(公告)日:2013-09-03

    申请号:US12847299

    申请日:2010-07-30

    IPC分类号: F02G3/00

    摘要: A power generator, such as a permanent magnet alternator (“PMA”) or a permanent magnet generator (“PMG”), may be used to provide electric power to a deicing system, for example. The power generator is embedded within a spinner, and may be in communication with a locally mounted electronic control unit (“ECU”).

    摘要翻译: 诸如永磁式交流发电机(“PMA”)或永磁发电机(“PMG”)之类的发电机例如可用于向除冰系统提供电力。 发电机嵌入在旋转器内,并且可以与本地安装的电子控制单元(“ECU”)通信。

    VARIABLE VANE ANGULAR POSITION SENSOR
    7.
    发明申请
    VARIABLE VANE ANGULAR POSITION SENSOR 审中-公开
    可变的角度角位置传感器

    公开(公告)号:US20130084179A1

    公开(公告)日:2013-04-04

    申请号:US13250396

    申请日:2011-09-30

    IPC分类号: F02C9/22 F02C7/00

    摘要: A variable vane control system for use with a gas turbine engine includes an actuator, a mechanical linkage assembly, and a vane position sensor. The gas turbine engine has a plurality of variable vanes each having an airfoil disposed in a gas flow path of the gas turbine engine. The plurality of variable vanes includes a first variable vane. The mechanical linkage assembly operably connects the actuator to at least the first variable vane. The vane position sensor is connected to one of the first variable vane or a portion of the mechanical linkage assembly proximate the first variable vane for sensing angular position of the first variable vane.

    摘要翻译: 与燃气涡轮发动机一起使用的可变叶片控制系统包括致动器,机械连杆组件和叶片位置传感器。 燃气涡轮发动机具有多个可变叶片,每个叶片具有设置在燃气涡轮发动机的气体流路中的翼型件。 多个可变叶片包括第一可变叶片。 机械联动装置将致动器可操作地连接到至少第一可变叶片。 叶片位置传感器连接到靠近第一可变叶片的第一可变叶片或机械连杆机构的一部分,用于检测第一可变叶片的角位置。

    CONTROLLABLE CONSTANT SPEED GEARBOX
    8.
    发明申请
    CONTROLLABLE CONSTANT SPEED GEARBOX 审中-公开
    可控恒速齿轮箱

    公开(公告)号:US20110314963A1

    公开(公告)日:2011-12-29

    申请号:US12824732

    申请日:2010-06-28

    IPC分类号: F16H37/06

    摘要: An engine mountable gearbox is provided and includes a body formed to define a plurality of connection points at which a main engine generator and one or more accessories are mounted, a first transmission disposed within the body at the connection point of the main engine generator to run the main engine generator at a controlled constant speed at varying speeds of the engine rotation and a second transmission disposed within the body at least at one of the connection points of the one or more accessories to run the one of the one or more of the accessories at a controlled constant speed at varying speeds of the engine rotation.

    摘要翻译: 本发明提供一种发动机安装式变速箱,它包括主体,其形成为限定主机发电机和一个或多个附件安装在其上的多个连接点;第一变速器,其设置在主发动机发电机连接点处的主体内运行 所述主发动机发电机在所述发动机旋转的变化速度下以受控的恒定速度和在所述主体内至少在所述一个或多个附件的所述连接点中的一个连接点处设置的第二变速器来运行所述一个或多个附件中的一个 在发动机转速的变化速度下以受控的恒定速度。

    Distributed approach to electronic engine control for gas turbine engines
    9.
    发明授权
    Distributed approach to electronic engine control for gas turbine engines 有权
    燃气轮机发动机电子发动机控制分布式方法

    公开(公告)号:US08295995B2

    公开(公告)日:2012-10-23

    申请号:US12427814

    申请日:2009-04-22

    IPC分类号: G01C23/00

    摘要: A distributed electronic engine control system includes an airframe module, an electronic engine control module, and an engine I/O module. The modules are arranged in locations remote from one another. A serial communications bus interconnects the modules with one another. A first engine controls device is connected to the engine I/O module and is configured to interact with an engine component and provide a first data. The engine I/O module includes inner loop control logic that uses the first data and produces a second data in response thereto. The electronic engine control module includes an outer loop control logic using the second data and produces a third data in response thereto. The airframe module receives power and distributes the power to the electronic engine control and engine I/O modules. The first, second and third data are provided on the serial communications bus.

    摘要翻译: 分布式电子发动机控制系统包括机身模块,电子发动机控制模块和发动机I / O模块。 模块布置在彼此远离的位置。 串行通信总线将模块互相互连。 第一发动机控制装置连接到发动机I / O模块,并被配置为与发动机部件交互并提供第一数据。 发动机I / O模块包括内循环控制逻辑,其使用第一数据并响应于此产生第二数据。 电子引擎控制模块包括使用第二数据的外环控制逻辑并响应于此产生第三数据。 机身模块接收电力并将电力分配给电子发动机控制和发动机I / O模块。 第一,第二和第三数据在串行通信总线上提供。

    TIME DELAY CONTACTOR FOR AIRCRAFT APU STARTER
    10.
    发明申请
    TIME DELAY CONTACTOR FOR AIRCRAFT APU STARTER 有权
    飞机APU起动机延时接触器

    公开(公告)号:US20110304158A1

    公开(公告)日:2011-12-15

    申请号:US12959471

    申请日:2010-12-03

    IPC分类号: F02N11/00

    摘要: A starter for an auxiliary power unit includes a direct current motor operably connectable to an auxiliary power unit. A clutch is arranged in an electrically parallel relationship and configured to operably connect the motor to the auxiliary power unit when engaged, the motor and the clutch powered by a common input line. A time delay switching element is located and configured to delay power delivery to the direct current motor thus providing for full engagement of the clutch prior to initiation of rotation of the motor.

    摘要翻译: 用于辅助动力单元的起动器包括可操作地连接到辅助动力单元的直流马达。 离合器以电并联的方式布置,并且构造成当接合时电动机与辅助动力单元可操作地连接,马达和离合器由公共输入线供电。 时间延迟开关元件被定位和配置成延迟向直流马达的动力输送,从而在马达的旋转开始之前提供离合器的完全接合。