Device for supplying fuel to a gas turbine engine with regulated fuel flow rate
    1.
    发明授权
    Device for supplying fuel to a gas turbine engine with regulated fuel flow rate 有权
    用于向具有调节的燃料流量的燃气涡轮发动机供应燃料的装置

    公开(公告)号:US08549863B2

    公开(公告)日:2013-10-08

    申请号:US11816535

    申请日:2006-02-17

    IPC分类号: F02C9/28

    摘要: A fuel supply device includes a fuel supply pipe receiving fuel at a non-regulated pressure delivered by a pump, a device for measuring the flow rate of fuel in the pipe, a first controlled variable-restriction valve mounted in the supply pipe, a control system connected to the flow rate measurement device and to the first valve to control the valve to deliver fuel to the engine at a desired flow rate under normal operating conditions of the engine, a second controlled variable-restriction valve mounted in the supply pipe in series with the first valve, and a control for controlling the second valve to enable the engine to be supplied with fuel at an adjustable, reduced flow rate in response to detecting over-speed or over-thrust of the engine.

    摘要翻译: 燃料供给装置包括燃料供给管,其接收由泵输送的非调节压力的燃料,用于测量管道内的燃料的流量的装置,安装在供给管中的第一受控可变截止阀,控制装置 连接到流量测量装置和第一阀的控制阀,以在发动机的正常运行条件下以期望的流量将燃料输送到发动机,第二受控可变节流阀串联安装在供应管中 具有第一阀,以及用于控制第二阀的控制器,以响应于检测到发动机的超速或超推力而使发动机以可调节的减小的流量供应燃料。

    Aircraft Engine Fuel Supply
    3.
    发明申请
    Aircraft Engine Fuel Supply 有权
    飞机发动机燃油供应

    公开(公告)号:US20110139123A1

    公开(公告)日:2011-06-16

    申请号:US11816586

    申请日:2006-02-17

    IPC分类号: F02M59/36 F02M37/04 F02M37/00

    摘要: A centrifugal pump driven by mechanical coupling with an engine has a low pressure inlet receiving fuel from a fuel circuit of an aircraft, a high pressure outlet connected to a regulator circuit for regulating the flow rate of fuel supplied to the engine, and an assistance pump unit that is electrically controlled, having an inlet connected to the aircraft fuel circuit and an outlet connected to the flow rate regulator circuit so as to deliver, via its outlet, fuel that is at a predetermined minimum pressure, the pressure of the fuel supplied to the regulator circuit being the higher of the pressures delivered by the centrifugal pump and the assistance pump unit.

    摘要翻译: 由发动机机械联接驱动的离心泵具有从飞行器的燃料回路接收燃料的低压入口,连接到用于调节供应到发动机的燃料的流量的调节器电路的高压出口以及辅助泵 具有电控制的单元,具有连接到飞行器燃料回路的入口和连接到流量调节器电路的出口,以便经由其出口将处于预定最小压力的燃料输送到供应到 调节器电路是离心泵和辅助泵单元输送的压力越高。

    Device For Supplying Fuel To A Gas Turbine Engine With Regulated Fuel Flow Rate
    4.
    发明申请
    Device For Supplying Fuel To A Gas Turbine Engine With Regulated Fuel Flow Rate 有权
    向具有调节燃油流量的燃气轮机发动机供油的装置

    公开(公告)号:US20080163931A1

    公开(公告)日:2008-07-10

    申请号:US11816535

    申请日:2006-02-17

    IPC分类号: F16K31/02

    摘要: A fuel supply device includes a fuel supply pipe receiving fuel at a non-regulated pressure delivered by a pump, a device for measuring the flow rate of fuel in the pipe, a first controlled variable-restriction valve mounted in the supply pipe, a control system connected to the flow rate measurement device and to the first valve to control the valve to deliver fuel to the engine at a desired flow rate under normal operating conditions of the engine, a second controlled variable-restriction valve mounted in the supply pipe in series with the first valve, and a control for controlling the second valve to enable the engine to be supplied with fuel at an adjustable, reduced flow rate in response to detecting over-speed or over-thrust of the engine.

    摘要翻译: 燃料供给装置包括燃料供给管,其接收由泵输送的非调节压力的燃料,用于测量管道内的燃料的流量的装置,安装在供给管中的第一受控可变截止阀,控制装置 连接到流量测量装置和第一阀的控制阀,以在发动机的正常运行条件下以期望的流量将燃料输送到发动机,第二受控可变节流阀串联安装在供应管中 具有第一阀,以及用于控制第二阀的控制器,以响应于检测到发动机的超速或超推力而使发动机以可调节的减小的流量供应燃料。