AIRCRAFT FUEL SYSTEM
    41.
    发明申请
    AIRCRAFT FUEL SYSTEM 有权
    飞机燃油系统

    公开(公告)号:US20160138473A1

    公开(公告)日:2016-05-19

    申请号:US14541929

    申请日:2014-11-14

    Abstract: A fuel supplying system includes a primary circuit for delivering fuel from a fuel tank to a primary circuit outlet. The system also includes a first supply circuit connected to the primary circuit outlet, the first supply circuit comprising a first supply circuit pump configured to pump fuel from the primary circuit outlet to engine fuel nozzles. The system further includes a second supply circuit also connected to the primary circuit outlet. The second supply circuit includes at least one actuating device configured to receive power from hydraulic pressure of the fuel. The second supply circuit also includes a second supply circuit pump configured to pump fuel from the primary circuit outlet to an actuating device, wherein the second supply circuit pump is independent from the first supply circuit pump. The second supply circuit further includes a return circuit configured to return fuel from the actuating device to the second supply circuit between the primary circuit outlet and the second supply circuit pump.

    Abstract translation: 燃料供给系统包括用于将燃料从燃料箱输送到主回路出口的主回路。 该系统还包括连接到主电路出口的第一供电电路,第一供电电路包括第一供电电路泵,其构造成将燃料从主电路出口泵送到发动机燃料喷嘴。 该系统还包括也连接到主电路出口的第二电源电路。 第二供应回路包括配置成从燃料的液压接收功率的至少一个致动装置。 第二供应回路还包括第二供应回路泵,其构造成将燃料从主要回路出口泵送到致动装置,其中第二供应回路泵独立于第一供应回路泵。 第二供应回路还包括一个回流回路,其配置成将燃料从致动装置返回到主回路出口和第二供应回路泵之间的第二供应回路。

    HEAT EXCHANGER
    42.
    发明申请
    HEAT EXCHANGER 审中-公开
    热交换器

    公开(公告)号:US20160122024A1

    公开(公告)日:2016-05-05

    申请号:US14531376

    申请日:2014-11-03

    Abstract: An air to air heat exchanger is provided including a core having a plurality of alternately stacked first layers and second layers. Each first layer includes a plurality of first modules having corrugated fins that define a plurality of first fluid flow paths. The first modules are aligned to fluidly couple the first fluid flow paths. Each second layer includes at least one second module having corrugated fins that define a plurality of second fluid flow paths. At least one second layer includes a third module having a plurality of corrugated fins that define a plurality of third fluid flow paths. The third module is arranged such that the third fluid flow paths are parallel to the second fluid flow paths. A number of corrugated fins formed in the third module is less than a number of corrugated fins formed in the second module.

    Abstract translation: 提供一种空气 - 空气热交换器,包括具有多个交替层叠的第一层和第二层的芯。 每个第一层包括具有限定多个第一流体流动路径的波纹状翅片的多个第一模块。 第一模块对准以流体地联接第一流体流动路径。 每个第二层包括具有限定多个第二流体流动路径的波纹状翅片的至少一个第二模块。 至少一个第二层包括具有限定多个第三流体流动路径的多个波纹状翅片的第三模块。 第三模块被布置成使得第三流体流动路径平行于第二流体流动路径。 形成在第三模块中的多个波纹状散热片小于形成在第二模块中的多个波纹状散热片。

    FUEL INTELLIGENT CROSSFEED VALVE FOR DETECTING LEAKAGE IN AIRCRAFT FUEL TANKS
    43.
    发明申请
    FUEL INTELLIGENT CROSSFEED VALVE FOR DETECTING LEAKAGE IN AIRCRAFT FUEL TANKS 有权
    用于检测飞机燃油箱泄漏的燃油智能交叉阀

    公开(公告)号:US20160122004A1

    公开(公告)日:2016-05-05

    申请号:US14531599

    申请日:2014-11-03

    Abstract: A fuel management system may include a first fuel tank and a second fuel tank. The fuel management system may also include an intelligent crossfeed valve positioned between the first fuel tank and the second fuel tank and configured to allow fuel to flow between the first fuel tank and the second fuel tank. The fuel management system may also include a sensor configured to detect an amount to which the intelligent crossfeed valve is open. The fuel management system may also include an engine controller connected to the sensor and configured to cause the intelligent crossfeed valve to close in response to the intelligent crossfeed valve being open a third predetermined amount.

    Abstract translation: 燃料管理系统可以包括第一燃料箱和第二燃料箱。 燃料管理系统还可以包括位于第一燃料箱和第二燃料箱之间并被配置为允许燃料在第一燃料箱和第二燃料箱之间流动的智能交叉进料阀。 燃料管理系统还可以包括被配置为检测智能交叉进料阀打开的量的传感器。 燃料管理系统还可以包括连接到传感器的发动机控制器,并且被配置为响应于智能交叉进料阀打开第三预定量而导致智能交叉进给阀关闭。

    ENERGY EFFICIENT PUMP SYSTEM
    45.
    发明申请
    ENERGY EFFICIENT PUMP SYSTEM 有权
    能源效率泵系统

    公开(公告)号:US20150101339A1

    公开(公告)日:2015-04-16

    申请号:US14183966

    申请日:2014-02-19

    CPC classification number: F02C7/236

    Abstract: A fuel system for a gas turbine engine, which includes a combustor section and an actuator, includes a fuel source, a combustor system, and an actuation system. The combustor system includes a combustor pump that is fluidly connected to the fuel source and to the combustor section, with the combustor pump being mechanically connected to and powered by an electric motor. The actuation system includes an actuator pump that is fluidly connected to the fuel source and to the actuator, with the actuator pump being mechanically connected to and powered by a gearbox or an electric motor.

    Abstract translation: 一种用于燃气涡轮发动机的燃料系统,其包括燃烧器部分和致动器,其包括燃料源,燃烧器系统和致动系统。 燃烧器系统包括燃烧器泵,该燃烧器泵流体连接到燃料源和燃烧器部分,燃烧器泵机械地连接到电动机并由电动机驱动。 致动系统包括致动器泵,该致动器泵流体地连接到燃料源和致动器,致动器泵机械地连接到齿轮箱或电动马达并由其驱动。

    FLUX BYPASS FOR SOLENOID ACTUATOR
    46.
    发明申请
    FLUX BYPASS FOR SOLENOID ACTUATOR 有权
    电磁阀执行器的通风旁路

    公开(公告)号:US20150097130A1

    公开(公告)日:2015-04-09

    申请号:US14169793

    申请日:2014-01-31

    Abstract: An electromagnetic solenoid actuator comprises a ferromagnetic core and a ferromagnetic plunger. The ferromagnetic core supports a plurality of windings, and is oriented along an axis. The ferromagnetic plunger is aligned axially with the ferromagnetic core, and is translatable along the axis to vary a width of an air gap separating the ferromagnetic plunger from the ferromagnetic core. The ferromagnetic plunger and the ferromagnetic core overlap axially at a flux bypass that provides an alternative flux path that diverts increasing flux away from the air gap as the width of air gap decreases.

    Abstract translation: 电磁螺线管致动器包括铁磁芯和铁磁柱塞。 铁磁芯支撑多个绕组,并且沿着轴线定向。 铁磁柱塞与铁磁芯轴向对准,并且可沿轴线平移以改变将铁磁柱塞与铁磁芯分离的气隙的宽度。 铁磁柱塞和铁磁芯在通量旁路处轴向重叠,提供了随着气隙宽度减小而将增加的磁通从气隙转移的替代磁通路径。

    SELF POWERED FLUID METERING UNITS
    47.
    发明申请
    SELF POWERED FLUID METERING UNITS 有权
    自供电流量计单位

    公开(公告)号:US20140324238A1

    公开(公告)日:2014-10-30

    申请号:US13872614

    申请日:2013-04-29

    Abstract: A system includes a metering module that receives fluid through a fluid inlet. The metering module includes a rotating component driven by the fluid, an electric machine, and a controller. The fluid is received from the fluid inlet at an inlet flow rate, and the rotating component provides the fluid to an outlet of the rotating component at an outlet pressure. The electric machine is configured to generate electrical power in response to rotation of the rotating component. The controller is powered by the electrical power generated by the electric machine, and controls a rotational speed of the rotating component to control the outlet pressure.

    Abstract translation: 一种系统包括一个通过流体入口接收流体的计量模块。 计量模块包括由流体驱动的旋转部件,电机和控制器。 流体以入口流速从流体入口接收,并且旋转部件在出口压力下将流体提供给旋转部件的出口。 电机被配置为响应于旋转部件的旋转产生电力。 控制器由电机产生的电力供电,并控制旋转部件的旋转速度以控制出口压力。

    FUEL AND ACTUATION SYSTEM FOR GAS TURBINE ENGINE
    48.
    发明申请
    FUEL AND ACTUATION SYSTEM FOR GAS TURBINE ENGINE 有权
    燃气发动机燃油和执行系统

    公开(公告)号:US20140290266A1

    公开(公告)日:2014-10-02

    申请号:US13851580

    申请日:2013-03-27

    CPC classification number: F02C9/263 F01D17/10 F02C7/236

    Abstract: A fuel system for an aircraft comprises a boost pump, a main fuel pump and a motive pump. The boost pump receives fuel from a storage unit. The main fuel pump receives fuel from the boost pump and delivers fuel to a distribution system. The motive fuel pump receives fuel from the boost pump, routes fuel through the storage unit, and delivers fuel to an actuator. A method for delivering fuel in an aircraft comprises pumping fuel from a fuel tank to a distribution system using a main pump, pumping fuel from a fuel tank to an actuator using a motive pump, and routing fuel from the actuator to the main pump

    Abstract translation: 用于飞行器的燃料系统包括增压泵,主燃料泵和动力泵。 增压泵从存储单元接收燃料。 主燃料泵从增压泵接收燃料并将燃料输送到分配系统。 动力燃料泵从增压泵接收燃料,将燃料通过存储单元引导,并将燃料输送到致动器。 用于在飞行器中输送燃料的方法包括:使用主泵将燃料从燃料箱泵送到配电系统,使用动力泵将燃料从燃料箱泵送到致动器,以及将燃料从致动器路由到主泵

    HIGH GAIN SERVO VALVE
    49.
    发明申请
    HIGH GAIN SERVO VALVE 有权
    高增压伺服阀

    公开(公告)号:US20140216245A1

    公开(公告)日:2014-08-07

    申请号:US13760815

    申请日:2013-02-06

    Abstract: A servo valve includes a movable throttling member positioned between a first opening and an opposing second opening, and a first inlet port and a second inlet port to convey a fluid flow toward the first and opening, respectively. A first inlet orifice, defined between the first inlet port and a first pressure reaction member, is located between and in fluid communication with the first inlet port and the first opening. A second inlet orifice, is located between and in fluid communication with the second inlet port and the second opening. The second pressure reaction member is secured to the first pressure reaction member at a substantially fixed distance. Each of the first inlet orifice and the second inlet orifice is variable via a change a pressure of the fluid flow downstream of the first inlet orifice and the second inlet orifice.

    Abstract translation: 伺服阀包括位于第一开口和相对的第二开口之间的可动节流件,以及分别向第一和开口输送流体流的第一入口端口和第二入口端口。 限定在第一入口和第一压力反应构件之间的第一入口孔位于第一入口和第一开口之间并与第一入口和第一开口流体连通。 第二入口孔位于第二入口和第二开口之间并与第二入口和第二开口流体连通。 第二压力反应构件以基本固定的距离固定到第一压力反应构件。 第一入口孔口和第二入口孔口中的每一个可以通过改变第一入口孔口和第二入口孔口下游的流体流动的压力而变化。

    VALVE SYSTEMS
    50.
    发明申请

    公开(公告)号:US20250109755A1

    公开(公告)日:2025-04-03

    申请号:US18376103

    申请日:2023-10-03

    Abstract: A system can include a first controllable valve configured to output a control pressure on one or more first pressure control lines, a second controllable valve configured to output a control pressure on one or more second pressure control lines, a transfer valve in fluid communication with the first controllable valve and the second controllable valve, and a hydraulic centering system operatively associated with and/or forming part of the transfer valve. The transfer valve can be configured to move between a first position, a second position, and a third position. The hydraulic centering system can be configured to maintain the transfer valve in the first position.

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