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    • 3. 发明申请
    • PUMP AUTHORITY SWITCHING APPARATUS FOR A FLUID DISTRIBUTION SYSTEM
    • 用于流体分配系统的泵管理权限切换装置
    • US20160084272A1
    • 2016-03-24
    • US14494309
    • 2014-09-23
    • Austin Wade MuellerCarthel C. BakerMichael P. Garry
    • Austin Wade MuellerCarthel C. BakerMichael P. Garry
    • F15B11/02F15B13/044
    • F15B11/02B64D37/34F02C7/236F04B49/225F15B13/044
    • A fluid distribution system includes a boost supply providing a fluid flow, and a fluid metering system downstream of the boost supply. The fluid metering system supplies fluid to a downstream device. A main fluid pump supplies at least a portion of the fluid flow to the fluid metering system. A shut-off valve is positioned upstream of a main fluid pump inlet. An actuation system is positioned downstream of the boost supply. The actuation system supplies fluid to one or more hydraulically-operated devices. An actuation pump supplies at least a portion of the fluid flow to the fluid metering system and to the actuation system. A first valve is positioned between the actuation pump and the fluid metering system. The first valve and the shut-off valve are operable to switch between the main fluid pump and the actuation pump as a source of fluid supply to the fluid metering system.
    • 流体分配系统包括提供流体流的升压电源和在升压电源下游的流体计量系统。 流体计量系统向下游装置供应流体。 主流体泵将至少一部分流体流供应到流体计量系统。 截止阀位于主流体泵入口的上游。 驱动系统位于升压电源的下游。 致动系统将流体提供给一个或多个液压操作的装置。 致动泵将流体流的至少一部分供应到流体计量系统和致动系统。 第一阀位于致动泵和流体计量系统之间。 第一阀和截止阀可操作以在主流体泵和致动泵之间切换,作为流体计量系统的流体源。
    • 4. 发明申请
    • Fuel System With Liquid Ring Pump With Centrifugal Air/Fuel Separator
    • 带有离心空气/燃油分离器的液环泵的燃油系统
    • US20150044016A1
    • 2015-02-12
    • US13962043
    • 2013-08-08
    • Austin Wade MuellerDmitriy Baryshnikov
    • Austin Wade MuellerDmitriy Baryshnikov
    • F02M39/02F04D9/02
    • F04D9/02B01D19/0057F04C19/001F04C19/004F04C2210/1044F04D5/002F05B2210/132
    • A fuel system incorporating a boost pump unit, a boost pump unit and method of pumping fuel are provided. The fuel system and boost pump unit are preferably self-priming and do not utilize an airframe mounted pump for supplying fuel for an aircraft combustor. The boost pump unit includes a liquid ring pump and an air/fuel separator. The air/fuel separator has an inlet and first and second outlet ports. The inlet is operably fluidly coupled to an outlet of the liquid ring pump. The air/fuel separator has an arcuate flow path. The first outlet port is in fluid communication with a radially outer portion of the arcuate flow path and the second outlet port is in fluid communication with a radially inner portion of the arcuate flow path. A return line connected to the first outlet port is configured to return fuel to the liquid ring pump.
    • 提供了包括增压泵单元,增压泵单元和泵送燃料的方法的燃料系统。 燃料系统和增压泵单元优选是自吸式的,并且不使用机身安装的泵来为飞行器燃烧器供应燃料。 增压泵单元包括液环泵和空气/燃料分离器。 空气/燃料分离器具有入口和第一和第二出口。 入口可操作地流体耦合到液环泵的出口。 空气/燃料分离器具有弓形流动路径。 第一出口端口与弧形流动路径的径向外部部分流体连通,第二出口端口与弧形流动路径的径向内部部分流体连通。 连接到第一出口的回流管被配置成将燃料返回到液环泵。