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    • 10. 发明申请
    • GAS TAKEOFF ISOLATION SYSTEM
    • 气体隔离系统
    • US20150308459A1
    • 2015-10-29
    • US14639221
    • 2015-03-05
    • Pascal LardyJose L. GilarranzWilliam C. Maier
    • Pascal LardyJose L. GilarranzWilliam C. Maier
    • F04D29/70F04D29/32F04D29/54F04D19/02F04D29/52
    • F04D29/701F04D17/122F04D25/0686F04D29/5806F04D29/5826
    • A fluid takeoff assembly for a motor-compressor is provided and includes an outer pipe having an inlet and an outlet, and an inner pipe defining a fluid passage extending from an open axial end toward a closed axial end thereof and a radial opening fluidly coupled with the fluid passage. The inner pipe may be disposed in the outer pipe such that the open axial end and the closed axial end are oriented toward the outlet and the inlet, respectively, and the inner and outer pipes define an annular space therebetween. A cross-flow member may be coupled with the inner pipe and may define a flowpath fluidly coupled with the fluid passage via the radial opening. A vane and the cross-flow member may be disposed in the annular space and configured to at least partially induce a swirling flow in a process fluid flowing through the annular space.
    • 提供了一种用于电动机 - 压缩机的流体起飞组件,并且包括具有入口和出口的外管,以及限定从开口轴向端部朝向其闭合轴向端延伸的流体通道的内管,以及径向开口, 流体通道。 内管可以设置在外管中,使得敞开的轴向端和闭合轴向端分别朝向出口和入口定向,并且内管和外管在它们之间限定环形空间。 横流构件可以与内管联接并且可以限定通过径向开口与流体通道流体连接的流路。 叶片和横流构件可以设置在环形空间中并且构造成在流过环形空间的过程流体中至少部分地引起旋流。