Fuel system for heat engine
    1.
    发明授权

    公开(公告)号:US11125169B2

    公开(公告)日:2021-09-21

    申请号:US16225457

    申请日:2018-12-19

    Abstract: A fuel metering system for a combustion section of a turbo machine is provided. The turbo machine includes a main fuel line configured to provide a flow of fuel and a zone fuel line split from the main fuel line through which at least a portion of the flow of fuel is provided. A fuel valve is disposed at the zone fuel line and is configured to obtain and receive a present fuel valve area value and a present valve position value. A first pressure sensor is disposed upstream of the fuel valve, in which the first pressure sensor is configured to obtain a first pressure value. A second pressure sensor is disposed downstream of the fuel valve, in which the second pressure sensor is configured to obtain a second pressure value. A flow meter is disposed downstream of the fuel valve. A controller is configured to perform operations, in which the operations include determining a demanded fuel valve actuator position based at least on an estimated fuel valve actuator position and a demanded fuel flow; comparing the demanded fuel flow and a present fuel flow; determining an actual fuel valve actuator position based at least on the demanded fuel valve actuator position and the compared demanded fuel flow and present fuel flow; and generating an valve effective area at the fuel valve based at least on the actual fuel valve actuator position.

    Pump Mixer Separator Unit
    2.
    发明申请

    公开(公告)号:US20200318539A1

    公开(公告)日:2020-10-08

    申请号:US16376184

    申请日:2019-04-05

    Abstract: A pump mixer separator unit is provided in communication with a stripping gas line that provides an inlet stripping gas flow and a fuel line that provides an inlet fuel flow. The pump mixer separator unit includes a first pump in fluid communication with the stripping gas line and the fuel line to form a fuel/gas mixture flow and generate a first pressure rise from the inlet fuel flow to the fuel/gas mixture flow; and a second pump in fluid communication with the first pump, wherein the second pump receives the fuel/gas mixture flow from the first pump, wherein the second pump separates the fuel/gas mixture flow into an outlet stripping gas flow and an outlet fuel flow and generates a second pressure rise from the fuel/gas mixture flow to the outlet fuel flow, wherein the first pump includes a supplemental pump feature for drawing an inlet fuel flow through the fuel line during operation.

    FUEL SYSTEMS FOR AIRCRAFT ENGINES

    公开(公告)号:US20250067217A1

    公开(公告)日:2025-02-27

    申请号:US18455316

    申请日:2023-08-24

    Abstract: A turbo engine for an aircraft includes a gas turbine engine having a fuel system to provide fuel to a combustion section. The fuel system includes a variable displacement pump driven by an accessory gearbox that is powered by a shaft of the gas turbine engine. The variable displacement pump has an inlet side and an outlet side. The variable displacement pump includes an actuator configured to adjust a discharge flow rate of the variable displacement pump. The fuel system also includes a fuel metering valve configured to receive pressurized fuel from the variable displacement pump and control a flow rate of the pressurized fuel to the combustion section. The fuel system further includes a bypass valve fluidly coupling the outlet side and the inlet side of the variable displacement pump to direct an excess portion of the pressurized fuel at the outlet side back to the inlet side.

    METHOD FOR FUEL DELIVERY
    4.
    发明申请

    公开(公告)号:US20210277836A1

    公开(公告)日:2021-09-09

    申请号:US16809711

    申请日:2020-03-05

    Abstract: A method of delivering fuel to an engine during operation of the engine, that includes, sensing the speed of sound in the fuel, determining a density or property of the fuel, and based on that density or fuel property adjusting the flow rate of the fuel. Further, an established fuel profile or determined energy density value can also be used to adjust the flow rate of the fuel.

    ROTARY ACTUATOR FOR VARIABLE GEOMETRY VANES
    9.
    发明申请
    ROTARY ACTUATOR FOR VARIABLE GEOMETRY VANES 有权
    旋转执行器可变几何空间

    公开(公告)号:US20160061117A1

    公开(公告)日:2016-03-03

    申请号:US14818813

    申请日:2015-08-05

    Abstract: A rotary actuator for control of variable geometry vanes is provided. The actuator is rotary so that operating components are internalized to protect fuel from contamination. The rotary actuator is a self-contained unit so that the device may be removed from the gas turbine engine without requiring removal of additional fuel system components. Finally, some embodiments of the rotary actuator may comprise multiple actuator loops to provide adjustment for two or more rows of vanes, independently.

    Abstract translation: 提供了用于控制可变几何叶片的旋转致动器。 致动器是旋转的,使得操作部件被内部化以保护燃料免受污染。 旋转致动器是独立的单元,使得该装置可以从燃气涡轮发动机移除,而不需要除去额外的燃料系统部件。 最后,旋转致动器的一些实施例可以包括多个致动器回路,以独立地为两行或多列叶片提供调节。

    Method for fuel delivery
    10.
    发明授权

    公开(公告)号:US11506133B2

    公开(公告)日:2022-11-22

    申请号:US16809711

    申请日:2020-03-05

    Abstract: A method of delivering fuel to an engine during operation of the engine, that includes, sensing the speed of sound in the fuel, determining a density or property of the fuel, and based on that density or fuel property adjusting the flow rate of the fuel. Further, an established fuel profile or determined energy density value can also be used to adjust the flow rate of the fuel.

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