Microwave vibration sensors
    32.
    发明授权
    Microwave vibration sensors 有权
    微波振动传感器

    公开(公告)号:US09316622B2

    公开(公告)日:2016-04-19

    申请号:US13889763

    申请日:2013-05-08

    CPC classification number: G01N29/36 G01H9/00 G10K11/002

    Abstract: A vibration sensor includes a probe body with a vibration isolator operatively connected to the probe body for isolation of the probe body from vibrations of a structure to be monitored for vibration. A waveguide is operatively connected to the probe body to convey microwaves to and from a surface for sensing vibration of the structure to be monitored for vibration.

    Abstract translation: 振动传感器包括具有可操作地连接到探针主体的隔振器的探针主体,用于将探针体与用于振动监测的结构的振动隔离。 波导管可操作地连接到探针体,以将微波传送到表面和从表面传送用于感测待监测的结构的振动以进行振动。

    FLUX BYPASS FOR SOLENOID ACTUATOR
    33.
    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
    34.
    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
    35.
    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

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