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    • 2. 发明申请
    • GAS TURBINE FUEL METERING UNIT
    • 燃气涡轮机燃油计量单位
    • US20110289931A1
    • 2011-12-01
    • US13204117
    • 2011-08-05
    • Charles H. FalkeLeo J. VeilleuxDouglas A. Parsons
    • Charles H. FalkeLeo J. VeilleuxDouglas A. Parsons
    • F02C1/00
    • F02C9/263F02C7/232F02C9/30F02C9/36F05D2260/602
    • A fuel system for a turbine engine is provided. The fuel system includes a positive displacement pump driven by an electric motor. The pump is rotated in a first direction to deliver fuel to the turbine engine, and a second direction for evacuating fuel from the turbine engine. A shut-off check valve is open in a first direction in response to a first differential pressure created by the pump in the first direction. The shut-off check valve is biased to a closed position when the pump is rotating in the second direction. An ecology check valve is biased to a closed position in the first direction and open in the second direction in response to a second differential pressure created by the pump. The check valves open and close automatically in response to the pressures generated by the positive displacement pump in each of the first and second rotational directions. In this manner, simple, reliable valves are utilized to regulate the flow of fuel in the fuel system.
    • 提供了一种用于涡轮发动机的燃料系统。 燃料系统包括由电动机驱动的正排量泵。 泵沿第一方向旋转以将燃料输送到涡轮发动机,以及用于从涡轮发动机排出燃料的第二方向。 关闭止回阀响应于泵沿第一方向产生的第一差压在第一方向打开。 当泵沿第二方向旋转时,关闭止回阀被偏压到关闭位置。 响应于由泵产生的第二差压,生态止回阀被偏压到第一方向上的关闭位置并沿第二方向打开。 响应于正排量泵在第一和第二旋转方向中的每一个中产生的压力,止回阀自动打开和关闭。 以这种方式,使用简单可靠的阀来调节燃料系统中的燃料流。
    • 3. 发明授权
    • Gas turbine fuel metering unit
    • 燃气轮机燃油计量单元
    • US08234875B2
    • 2012-08-07
    • US13204117
    • 2011-08-05
    • Charles H. FalkeLeo J. VeilleuxDouglas A. Parsons
    • Charles H. FalkeLeo J. VeilleuxDouglas A. Parsons
    • F02C7/22F02C7/26
    • F02C9/263F02C7/232F02C9/30F02C9/36F05D2260/602
    • A fuel system for a turbine engine is provided. The fuel system includes a positive displacement pump driven by an electric motor. The pump is rotated in a first direction to deliver fuel to the turbine engine, and a second direction for evacuating fuel from the turbine engine. A shut-off check valve is open in a first direction in response to a first differential pressure created by the pump in the first direction. The shut-off check valve is biased to a closed position when the pump is rotating in the second direction. An ecology check valve is biased to a closed position in the first direction and open in the second direction in response to a second differential pressure created by the pump. The check valves open and close automatically in response to the pressures generated by the positive displacement pump in each of the first and second rotational directions. In this manner, simple, reliable valves are utilized to regulate the flow of fuel in the fuel system.
    • 提供了一种用于涡轮发动机的燃料系统。 燃料系统包括由电动机驱动的正排量泵。 泵沿第一方向旋转以将燃料输送到涡轮发动机,以及用于从涡轮发动机排出燃料的第二方向。 关闭止回阀响应于泵沿第一方向产生的第一差压在第一方向打开。 当泵沿第二方向旋转时,关闭止回阀被偏压到关闭位置。 响应于由泵产生的第二差压,生态止回阀被偏压到第一方向上的关闭位置并沿第二方向打开。 响应于正排量泵在第一和第二旋转方向中的每一个中产生的压力,止回阀自动打开和关闭。 以这种方式,使用简单可靠的阀来调节燃料系统中的燃料流。
    • 4. 发明申请
    • GAS TURBINE FUEL METERING UNIT
    • 燃气涡轮机燃油计量单位
    • US20100031658A1
    • 2010-02-11
    • US11621685
    • 2007-01-10
    • Charles H. FalkeLeo J. VeilleuxDouglas A. Parsons
    • Charles H. FalkeLeo J. VeilleuxDouglas A. Parsons
    • F02C7/22F04B49/00
    • F02C9/263F02C7/232F02C9/30F02C9/36F05D2260/602
    • A fuel system for a turbine engine is provided. The fuel system includes a positive displacement pump driven by an electric motor. The pump is rotated in a first direction to deliver fuel to the turbine engine, and a second direction for evacuating fuel from the turbine engine. A shut-off check valve is open in a first direction in response to a first differential pressure created by the pump in the first direction. The shut-off check valve is biased to a closed position when the pump is rotating in the second direction. An ecology check valve is biased to a closed position in the first direction and open in the second direction in response to a second differential pressure created by the pump. The check valves open and close automatically in response to the pressures generated by the positive displacement pump in each of the first and second rotational directions. In this manner, simple, reliable valves are utilized to regulate the flow of fuel in the fuel system.
    • 提供了一种用于涡轮发动机的燃料系统。 燃料系统包括由电动机驱动的正排量泵。 泵沿第一方向旋转以将燃料输送到涡轮发动机,以及用于从涡轮发动机排出燃料的第二方向。 关闭止回阀响应于泵沿第一方向产生的第一差压在第一方向打开。 当泵沿第二方向旋转时,关闭止回阀被偏压到关闭位置。 响应于由泵产生的第二差压,生态止回阀被偏压到第一方向上的关闭位置并沿第二方向打开。 响应于正排量泵在第一和第二旋转方向中的每一个中产生的压力,止回阀自动打开和关闭。 以这种方式,使用简单可靠的阀来调节燃料系统中的燃料流。
    • 6. 发明申请
    • VACUUM SYSTEM FOR MEMBRANE FUEL STABILIZATION UNIT
    • 用于膜燃料稳定装置的真空系统
    • US20090266229A1
    • 2009-10-29
    • US12495897
    • 2009-07-01
    • Douglas A. Parsons
    • Douglas A. Parsons
    • B01D19/00F02C7/22
    • F01D25/20B01D19/0036F02C7/16F02C7/22F02C7/32F05D2220/722Y02E20/18Y02T50/671Y02T50/675
    • Oil system components for a turbine engine are used to provide a vacuum system for a fuel stabilization unit (FSU). A vacuum system pulls oxygen and other contaminants from fuel into a vacuum chamber within the FSU. The vacuum system pumps the discharge through a vacuum outlet in the FSU toward a vacuum pump. Due to the quality of vacuum required, a two-stage vacuum pump is used. A first stage vacuum pump is an oil system scavenge pump for the turbine engine and the second stage vacuum is provided by a second stage vacuum pump. The discharge flows from the vacuum chamber through to the second stage vacuum pump and is then added to the oil supply. The oil and discharge mixture is sent through an oil system de-oiler and a de-aerator to clean the oil supply prior to pumping the oil back through the oil system.
    • 用于涡轮发动机的油系统部件用于为燃料稳定单元(FSU)提供真空系统。 真空系统将燃料中的氧气和其他污染物吸入FSU内的真空室。 真空系统通过FSU中的真空出口将排气泵送到真空泵。 由于需要真空的质量,所以使用两级真空泵。 第一级真空泵是用于涡轮发动机的油系清扫泵,第二级真空由第二级真空泵提供。 排放物从真空室通过到第二级真空泵,然后加到油源中。 油和排出混合物通过油系除油器和除气器送出,以在将油泵送回油系统之前清洁供油装置。
    • 8. 发明授权
    • Lubrication system valve
    • 润滑系统阀
    • US06886665B2
    • 2005-05-03
    • US10313859
    • 2002-12-06
    • Douglas A. ParsonsKenneth Marks
    • Douglas A. ParsonsKenneth Marks
    • F16K11/076F01M1/00
    • F16K11/076Y10T137/86863
    • A fluid scavenging system is provided for a lubrication system including a gas turbine engine having bearing compartments. A valve includes a housing with an outlet and a plurality of fluid inlets respectively in fluid communication with the bearing compartments. The valve includes a rotationally driven member arranged within the housing with the member having a plurality of ports arranged thereon each defining an arcuate slot. Each of the ports are selectively in fluid communication with one of the fluid inlets through the arcuate slot during rotation of the member for selectively permitting fluid flow between the opening of one of the fluid inlets through one of the corresponding ports in the member. A fluid pump is fluidly connected to the outlet for drawing fluid from each of the plurality of fluid compartments during fluid rotation of the member. The driven member rotates about an axis 360°, and preferably, the ports are respectively aligned with the fluid inlets for approximately at least 360° such that the pump does not run dry. The arcuate slots may overlap during a range of degrees such that more than one compartment is scavenged. The size of the arcuate slot and degrees through which the arcuate slot is in communication with its respective inlet determines the duration that a particular bearing compartment is scavenged and the volume of bearing fluid that may be removed from the compartment.
    • 提供了一种用于包括具有轴承隔室的燃气涡轮发动机的润滑系统的流体清除系统。 阀包括具有出口的壳体和分别与轴承隔室流体连通的多个流体入口。 阀包括布置在壳体内的旋转驱动构件,其中构件具有布置在其上的多个端口,每个端口限定弓形狭槽。 每个端口在构件的旋转期间选择性地通过弓形槽与一个流体入口流体连通,用于选择性地允许流体在通过构件中的相应端口之一的流体入口之间流动。 流体泵流体地连接到出口,用于在构件的流体旋转期间从多个流体隔室中的每一个抽出流体。 被驱动构件围绕360°旋转,优选地,端口分别与流体入口对准大约至少360°,使得泵不会干燥。 弧形槽可以在一定范围内重叠,使得多于一个隔室被清除。 弓形槽的尺寸和弧形槽与其相应的入口连通的程度确定特定的轴承隔室被清扫的持续时间和可以从隔间移除的轴承流体的体积。
    • 10. 发明授权
    • Vacuum system for membrane fuel stabilization unit
    • 膜燃料稳定装置真空系统
    • US08679226B2
    • 2014-03-25
    • US12495897
    • 2009-07-01
    • Douglas A. Parsons
    • Douglas A. Parsons
    • B01D19/00
    • F01D25/20B01D19/0036F02C7/16F02C7/22F02C7/32F05D2220/722Y02E20/18Y02T50/671Y02T50/675
    • Oil system components for a turbine engine are used to provide a vacuum system for a fuel stabilization unit (FSU). A vacuum system pulls oxygen and other contaminants from fuel into a vacuum chamber within the FSU. The vacuum system pumps the discharge through a vacuum outlet in the FSU toward a vacuum pump. Due to the quality of vacuum required, a two-stage vacuum pump is used. A first stage vacuum pump is an oil system scavenge pump for the turbine engine and the second stage vacuum is provided by a second stage vacuum pump. The discharge flows from the vacuum chamber through to the second stage vacuum pump and is then added to the oil supply. The oil and discharge mixture is sent through an oil system de-oiler and a de-aerator to clean the oil supply prior to pumping the oil back through the oil system.
    • 用于涡轮发动机的油系统部件用于为燃料稳定单元(FSU)提供真空系统。 真空系统将燃料中的氧气和其他污染物吸入FSU内的真空室。 真空系统通过FSU中的真空出口将排气泵送到真空泵。 由于需要真空的质量,所以使用两级真空泵。 第一级真空泵是用于涡轮发动机的油系清扫泵,第二级真空由第二级真空泵提供。 排放物从真空室通过到第二级真空泵,然后加到油源中。 油和排放混合物通过油系除油器和除气器送出,以在将油泵送回油系统之前清洁供油。