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    • 7. 发明授权
    • Turning vane
    • 转动叶片
    • US09399199B2
    • 2016-07-26
    • US14772461
    • 2014-02-09
    • ILLINOIS TOOL WORKS INC.
    • Joseph C. DilleRobert W. AltonjiGuoging Wang
    • G01F1/37B01F5/06G01F1/684G01F1/84G01F5/00G05D7/06G01F1/82F15D1/00
    • B01F5/0602F15D1/001G01F1/684G01F1/6842G01F1/82G01F1/84G01F5/00G05D7/0635
    • The disclosed embodiments include a mass flow controller for controlling a flow of a fluid. In one embodiment, the mass flow controller comprises an inlet for receiving the fluid; a flow path in which the fluid passes through the mass flow controller; a mass flow meter for providing a signal corresponding to mass flow of the fluid through the flow path, the mass flow meter having a bypass through which a majority of fluid flows; a turning vane positioned upstream of the bypass for generating a more uniform fluid flow; an adjustable valve for regulating the flow of the fluid out of an outlet of the mass flow controller; and a controller configured to apply a valve control signal to adjust the adjustable valve to a desired valve position to control the flow of the fluid out of an outlet of the mass flow controller.
    • 所公开的实施例包括用于控制流体流动的质量流量控制器。 在一个实施例中,质量流量控制器包括用于接收流体的入口; 流体通过质量流量控制器的流动路径; 质量流量计,用于提供对应于通过流路的流体的质量流量的信号,质量流量计具有大部分流体流经的旁路; 位于旁路上游的转动叶片,用于产生更均匀的流体流动; 用于调节流体流出质量流量控制器的出口的可调节阀; 以及控制器,被配置为施加阀控制信号以将可调节阀调节到期望的阀位置,以控制流体流出质量流量控制器的出口。
    • 9. 发明申请
    • Ventilated Drainage System
    • 通风排水系统
    • US20150361999A1
    • 2015-12-17
    • US14302676
    • 2014-06-12
    • The Boeing Company
    • Robert Henry WillieDavid F. Cerra
    • F15D1/00B64D29/00B64D37/00
    • F15D1/001B64C1/1453B64D29/00B64D37/005B64D37/26F01D25/32F02K1/82F05D2260/602F15D1/008Y02T50/672Y10T137/0391Y10T137/2082
    • A method and apparatus for draining fluid from a structure on an aircraft. The apparatus comprises a drainage tube, a housing, a number of inlet holes in the housing, and a number of outlet holes in the housing. The drainage tube has first end that connects to a structure on an aircraft and a second end opposite the first end. The housing connects to the structure. The drainage tube is located within the housing. Air flows into the housing during flight of the aircraft through the number of inlet holes in the housing. The air flows out of the housing during flight of the aircraft through the number of outlet holes. The air flowing into the housing through the number of inlet holes and out the housing through the number of outlet holes directs fluid out of the drainage tube and away from the structure during flight of the aircraft.
    • 一种用于从飞机上的结构排出流体的方法和装置。 该装置包括排水管,壳体,壳体中的多个入口孔以及壳体中的多个出口孔。 排水管具有连接到飞机上的结构的第一端和与第一端相对的第二端。 外壳连接到结构。 引流管位于外壳内。 在飞行器飞行期间,空气通过壳体中的入口孔数进入壳体。 在飞行器飞行期间,空气通过出口孔流出外壳。 通过多个入口孔流入壳体的空气通过出口孔排出壳体,在飞行器飞行期间将流体引导出排水管并远离结构。
    • 10. 发明授权
    • Conditioner, apparatus and method
    • 护发素,装置和方法
    • US09003895B2
    • 2015-04-14
    • US13734705
    • 2013-01-04
    • Christopher B. LairdGregor Brown
    • Christopher B. LairdGregor Brown
    • G01F1/66G01F15/00
    • F15D1/025F15D1/001F15D1/06G01F1/662G01F1/667G01F15/00
    • The present invention pertains to a flow conditioner for displacing and mixing fluid flow to minimize the effects of thermal gradients on the accuracy of a transit time ultrasonic flowmeter and defines an envelope in a cross sectional direction in a pipe having a first ramp adapted to be disposed in the pipe and extending from the outside of the envelope inward toward the center of the pipe in a downstream direction with respect to the fluid flow and forming an angle between 0° and 90° relative to the pipe's inner surface. The conditioner has a second ramp adapted to be disposed in the pipe and in juxtaposition with the first ramp, the second ramp extending from the outside of the envelope inward toward the center of the pipe in an upstream direction with respect to the fluid flow and forming an angle between 0° and 90° relative to the pipe's inner surface. An apparatus for determining fluid flow in a pipe having ultrasonic transducer sites. A method for determining fluid flow in a pipe. A method for affecting fluid flow in a pipe.
    • 本发明涉及一种用于移动和混合流体流动的流量调节器,以最小化热梯度对渡越时间超声波流量计的精度的影响,并且在具有适于被布置的第一斜坡的管中限定横截面方向上的包络 并且在相对于流体流动的下游方向从管状体的外侧向内侧向管的中心延伸,并相对于管的内表面形成0°〜90°的角度。 调节器具有适于设置在管道中并与第一斜坡并置的第二斜坡,第二斜面从壳体的外侧向内朝向管的中心沿相对于流体流动的上游方向延伸并形成 相对管道内表面为0°至90°的角度。 一种用于确定具有超声换能器位置的管道中的流体流动的装置。 一种用于确定管道中的流体流动的方法。 一种影响管道中流体流动的方法。