Combined air turbine starter, air-oil cooler, and fan
    1.
    发明授权
    Combined air turbine starter, air-oil cooler, and fan 有权
    组合式空气涡轮起动器,空气 - 油冷却器和风扇

    公开(公告)号:US08522521B2

    公开(公告)日:2013-09-03

    申请号:US12942520

    申请日:2010-11-09

    申请人: Gerald P. Dyer

    发明人: Gerald P. Dyer

    摘要: An air turbine starter assembly includes a starter turbine housing having a turbine gas flow path and a fan gas flow path, and a shaft rotatable with respect to the starter turbine housing. A plurality of turbine blades are connected to the shaft. A plurality of fan blades are also connected to the shaft.

    摘要翻译: 一种空气涡轮起动器组件包括具有涡轮机气体流动路径和风扇气体流动路径的起动涡轮机壳体以及相对于起动涡轮机壳体可旋转的轴。 多个涡轮机叶片连接到轴。 多个风扇叶片也连接到轴。

    COMBINED AIR TURBINE STARTER, AIR-OIL COOLER, AND FAN
    3.
    发明申请
    COMBINED AIR TURBINE STARTER, AIR-OIL COOLER, AND FAN 有权
    组合式空气涡轮起动器,空气冷却器和风扇

    公开(公告)号:US20120111022A1

    公开(公告)日:2012-05-10

    申请号:US12942520

    申请日:2010-11-09

    申请人: Gerald P. Dyer

    发明人: Gerald P. Dyer

    IPC分类号: F02C7/277

    摘要: An air turbine starter assembly includes a starter turbine housing having a turbine gas flow path and a fan gas flow path, and a shaft rotatable with respect to the starter turbine housing. A plurality of turbine blades are connected to the shaft. A plurality of fan blades are also connected to the shaft.

    摘要翻译: 一种空气涡轮起动器组件包括具有涡轮机气体流动路径和风扇气体流动路径的起动涡轮机壳体以及相对于起动涡轮机壳体可旋转的轴。 多个涡轮机叶片连接到轴。 多个风扇叶片也连接到轴。

    Viscosity regulating valve
    4.
    发明授权
    Viscosity regulating valve 有权
    粘度调节阀

    公开(公告)号:US06789562B2

    公开(公告)日:2004-09-14

    申请号:US10379063

    申请日:2003-03-04

    IPC分类号: G05D703

    摘要: The subject invention is a valve for regulating the viscosity of fluid. The valve includes a housing defining a bore having a first inlet supplying “cold” hydraulic fluid at a first viscosity and a second inlet supplying “hot” hydraulic fluid at a second viscosity. A spool valve disposed within the bore has at least one land to proportionally control the flow of hydraulic fluid through the inlets. Hydraulic fluid from the first and second inlets mixes within the valve and exits the valve through an outlet at an optimum viscosity. A flow restrictor creates a pressure force on the spool valve that is proportional to the viscosity of the hydraulic fluid flowing through the outlet. The pressure force acts to move the spool valve such that the spool valve partially blocks the flow of hydraulic fluid through the first and second inlets, thereby controlling the proportion of “cold” and “hot” fluid to maintain the viscosity of the hydraulic fluid flowing through the outlet.

    摘要翻译: 本发明是用于调节流体粘度的阀。 所述阀包括限定孔的壳体,所述孔具有以第一粘度供应“冷”液压流体的第一入口和以第二粘度供应“热”液压流体的第二入口。 设置在孔内的滑阀具有至少一个平台以成比例地控制通过入口的液压流体的流动。 来自第一和第二入口的液压流体在阀内混合并通过出口以最佳粘度离开阀。 限流器在滑阀上产生与流过出口的液压流体的粘度成比例的压力。 压力用于移动滑阀,使得滑阀部分地阻塞通过第一和第二入口的液压流体的流动,从而控制“冷”和“热”流体的比例,以保持液压流体的粘度流动 通过插座。

    Integrated permanent magnet alternator and cooling fan
    5.
    发明授权
    Integrated permanent magnet alternator and cooling fan 有权
    集成永磁发电机和冷却风扇

    公开(公告)号:US08395275B2

    公开(公告)日:2013-03-12

    申请号:US12942527

    申请日:2010-11-09

    IPC分类号: F01D15/10

    摘要: A permanent magnet alternator includes a permanent magnet alternator stator attached to a housing. A shaft is rotatable with respect to the housing with a permanent magnet alternator rotor attached to the shaft. The permanent magnet alternator rotor is positioned with respect to the permanent magnet alternator stator so as to generate electricity when the shaft rotates. A cooling fan is also attached to the shaft and is positioned in a gas flow path for flowing air through the gas flow path.

    摘要翻译: 永磁式交流发电机包括固定在外壳上的永磁式交流发电机定子。 轴可相对于壳体旋转,永磁式交流发电机转子附接到轴上。 永磁式交流发电机转子相对于永磁式交流发电机定子定位,以便当轴旋转时发电。 冷却风扇也安装在轴上,并且位于用于使空气流过气体流路的气体流路中。

    FUEL PUMPING SYSTEM FOR A GAS TURBINE ENGINE
    6.
    发明申请
    FUEL PUMPING SYSTEM FOR A GAS TURBINE ENGINE 有权
    燃气涡轮发动机燃油泵系统

    公开(公告)号:US20110289925A1

    公开(公告)日:2011-12-01

    申请号:US12786844

    申请日:2010-05-25

    IPC分类号: F02C7/22

    摘要: A fuel supply system for a gas turbine engine has a first pump for delivering fuel to a first use on a gas turbine engine, and a second pump for delivering fuel to a second use on the gas turbine engine. A valve allows flow from the first pump to be delivered to the first use, but also routes some flow from the first pump to supplement fuel flow from the second pump until a pressure downstream of the second pump increases. The valve then allows flow from the second pump to flow to the first use to supplement the flow from the first pump.

    摘要翻译: 用于燃气涡轮发动机的燃料供应系统具有用于将燃料输送到燃气涡轮发动机上的第一次使用的第一泵和用于将燃料输送到燃气涡轮发动机上的第二次使用的第二泵。 阀允许来自第一泵的流量被输送到第一次使用,而且还将来自第一泵的一些流动路线补充来自第二泵的燃料流,直到第二泵下游的压力增加。 然后,阀允许来自第二泵的流动流动到第一次使用以补充来自第一泵的流量。

    Fuel metering system
    7.
    发明授权
    Fuel metering system 失效
    燃油计量系统

    公开(公告)号:US5448882A

    公开(公告)日:1995-09-12

    申请号:US166685

    申请日:1993-12-14

    IPC分类号: F02C7/228 F02C9/26

    CPC分类号: F02C7/228 F02C9/263

    摘要: A fuel control system independently meters fuel flow to a first and a second set of pilot fuel nozzles, and to a set of main fuel nozzles. A pilot coaxial metering and pressure regulating valve is coupled between a primary fuel inlet line and the first and second sets of pilot nozzles, and a main coaxial metering and pressure regulating valve is coupled between the primary fuel inlet line and the set of main fuel nozzles. Each coaxial metering and pressure regulating valve maintains a substantially constant pressure drop across the respective valve, and includes a metering window. The size of each metering window is controlled by an engine electronic control unit based on the signals transmitted by a respective LVDT, in order to precisely meter the fuel flow through the valve and to the respective sets of fuel nozzles. A control pressure regulating valve maintains a minimum pressure differential between the fuel inlet line and the downstream sides of the coaxial metering and pressure regulating valves, in order to provide sufficient pressure to operate the valves, and directs excess fuel from the fuel pump into a return line. A minimum pressure and shut-off valve is coupled between each coaxial metering and pressure regulating valve and the respective fuel nozzles, in order to maintain a minimum fuel pressure level, and to terminate fuel flow to the nozzles. A sequence valve is coupled to the minimum pressure and shut-off valves to control actuation of the valves.

    摘要翻译: 燃料控制系统独立地计量到第一和第二组先导燃料喷嘴的燃料流量以及一组主燃料喷嘴。 一个先导同轴计量和压力调节阀连接在主燃料入口管线和第一和第二组先导喷嘴之间,并且主同轴计量和压力调节阀联接在主要燃料入口管线和主燃料喷嘴组之间 。 每个同轴计量和压力调节阀在相应的阀上保持基本恒定的压降,并且包括计量窗口。 每个计量窗口的尺寸由发动机电子控制单元基于由相应的LVDT传输的信号来控制,以便精确地计量通过阀门和各组燃料喷嘴的燃料流量。 控制压力调节阀保持燃料入口管线和同轴计量和压力调节阀的下游侧之间的最小压力差,以便提供足够的压力来操作阀门,并且将多余的燃料从燃料泵引导到回流 线。 最小压力和截止阀联接在每个同轴计量和压力调节阀与相应的燃料喷嘴之间,以便保持最小燃料压力水平,并终止燃料流向喷嘴。 顺序阀联接到最小压力和截止阀以控制阀的致动。

    PASSIVE EQUILIZATION FLOW DIVIDER VALVE
    9.
    发明申请
    PASSIVE EQUILIZATION FLOW DIVIDER VALVE 有权
    被动均衡流量分流阀

    公开(公告)号:US20130255270A1

    公开(公告)日:2013-10-03

    申请号:US13431187

    申请日:2012-03-27

    IPC分类号: F02C7/228 F02C7/232

    CPC分类号: F02C7/232 F02C9/263

    摘要: A method and system for providing fuel to primary and secondary fuel nozzles in a gas turbine engine fuel system comprises generating a fuel flow and routing primary fuel from the fuel flow to a primary fuel nozzle. Backpressure on the fuel flow is maintained using a valve. The valve is opened at increased fuel flow to route secondary fuel from the fuel flow to a secondary fuel nozzle. The valve is progressively opened under increasing fuel flows to reduce a pressure drop across the valve produced by the secondary fuel.

    摘要翻译: 一种用于向燃气涡轮发动机燃料系统中的主要和次要燃料喷嘴提供燃料的方法和系统包括产生燃料流并且将一次燃料从燃料流引导到主燃料喷嘴。 使用阀门保持燃油流量的背压。 阀门以增加的燃料流量打开以将二次燃料从燃料流引导到二次燃料喷嘴。 在增加的燃料流量下逐渐打开阀门,以减少由二次燃料产生的阀门上的压降。

    Fuel splitter valve assembly for gas turbine
    10.
    发明授权
    Fuel splitter valve assembly for gas turbine 失效
    用于燃气轮机的燃油分配阀组件

    公开(公告)号:US5339636A

    公开(公告)日:1994-08-23

    申请号:US985769

    申请日:1992-12-04

    IPC分类号: F02C7/228 F02C1/00 F02G3/00

    CPC分类号: F02C7/228 Y10T137/2521

    摘要: A fuel delivery system (10) incorporates a fuel splitter valve assembly (30) including a first valve (40) having a selectively positionable spool (42) disposed therein for controllably metering fuel flow therethrough for delivery to a first combustion chamber (22) and a second valve (50) operative to pass a second portion of the fuel flow to a second combustion chamber (24) while maintaining at least a desired minimum pressure upstream of the first valve (40) whenever the second combustion chamber is in operation, and to shut-off fuel flow to the second combustion chamber whenever the second combustion chamber is not in operation.

    摘要翻译: 燃料输送系统(10)包括燃料分配阀组件(30),其包括第一阀(40),第一阀(40)具有设置在其中的可选择性定位的阀芯(42),用于可控地计量通过其中的燃料流以输送到第一燃烧室(22)和 第二阀(50),其操作以将燃料流的第二部分传递到第二燃烧室(24),同时在第二燃烧室运行时保持至少所述第一阀(40)上游的所需最小压力,以及 每当第二燃烧室不工作时,切断到第二燃烧室的燃料流。