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    • 2. 发明授权
    • Flare stack adapted to heat incoming fuel
    • 适用于加热进入燃料的火炬烟囱
    • US07857898B2
    • 2010-12-28
    • US11828006
    • 2007-07-25
    • E. Todd WigginsD. Jeffrey Hill
    • E. Todd WigginsD. Jeffrey Hill
    • B01D53/14
    • F23N1/002F23G7/085F23J2213/203F23N2025/19F23N2025/21Y02E20/12
    • A flare stack that preferably comprises a burner assembly, an exhaust stack, an housing, and a fuel line. The burner assembly burns a fuel to generate thermal energy and combustion byproducts. The exhaust stack is cooperatively associated with the burner assembly to direct the thermal energy and combustion byproducts away from the burner assembly. The housing at least partially defines a fluid-receiving chamber in thermal communication with the exhaust stack. The fluid-receiving chamber has a heat-transfer fluid disposed therein. The fuel line is in fluid communication with the burner assembly to deliver fuel to the burner assembly. At least a portion of the fuel line is in thermal communication with at least one of the exhaust stack, housing, or heat-transfer fluid to permit fuel in the fuel line to absorb thermal energy before reaching the burner assembly. In one embodiment, the burner assembly includes a pressure-variable burner to increase the rate of fuel consumption of the burner in relation to the pressure in the fuel line. In the preferred embodiment, the housing has an inlet and an outlet formed therethrough in fluid communication with the fluid-receiving chamber. The inlet permits heat-transfer fluid to flow into the fluid-receiving chamber to absorb thermal energy from the exhaust stack, and the outlet permits heat-transfer fluid to flow out of the fluid-receiving chamber.
    • 优选地包括燃烧器组件,排气叠层,壳体和燃料管线的火炬烟囱。 燃烧器组件燃烧燃料以产生热能和燃烧副产物。 废气堆叠与燃烧器组件协作地关联以将热能和燃烧副产物远离燃烧器组件。 壳体至少部分地限定与废气堆叠热连通的流体接收室。 流体接收室具有设置在其中的传热流体。 燃料管线与燃烧器组件流体连通以将燃料输送到燃烧器组件。 燃料管线的至少一部分与排气叠层,壳体或传热流体中的至少一个热连通,以允许燃料管线中的燃料在到达燃烧器组件之前吸收热能。 在一个实施例中,燃烧器组件包括压力可变燃烧器,以相对于燃料管线中的压力增加燃烧器的燃料消耗率。 在优选实施例中,壳体具有与流体接收室流体连通的通过其形成的入口和出口。 入口允许热传递流体流入流体接收室以吸收来自排气叠层的热能,并且出口允许热传递流体流出流体接收室。
    • 3. 发明申请
    • Limited modulation furnace and method for controlling the same
    • 有限调制炉及其控制方法
    • US20060199121A1
    • 2006-09-07
    • US11366084
    • 2006-03-02
    • Curtis Caskey
    • Curtis Caskey
    • F23N1/02
    • F23N1/082F23N2023/36F23N2025/19F23N2025/21
    • A limited modulation furnace and a method for controlling the limited modulation furnace using a floating control algorithm are disclosed. The method includes providing a furnace comprising a modulating furnace stage and at least one fixed heat output furnace stage, each fixed heat output furnace stage having an operational status of either on or off, passing a heating fluid through the furnace, measuring a temperature of the heating fluid exiting the furnace, determining an error based on a difference between the measured temperature and a set-point temperature, the set-point temperature being associated with a thermostat setting, determining whether the error is within a deadband range for the set-point temperature, and modifying at least one of the heat output of the modulating furnace stage or the operational status of at least one of the fixed heat output furnace stages in response to the error being outside the deadband range.
    • 公开了一种使用浮动控制算法来控制有限调制炉的有限调制炉和方法。 该方法包括提供包括调制炉台和至少一个固定热输出炉台的炉,每个固定的热输出炉台具有开启或关闭的操作状态,使加热流体通过炉,测量温度 加热排出炉的流体,基于测量温度和设定点温度之间的差异确定误差,设定点温度与恒温器设置相关联,确定误差是否在设定点的死区范围内 温度,并且响应于该误差在死区范围之外,修改调制炉台的热输出中的至少一个或至少一个固定热输出炉级的操作状态。
    • 5. 发明授权
    • Integrated fuel/air ratio control system
    • 一体化燃油/空气比率控制系统
    • US5634786A
    • 1997-06-03
    • US346787
    • 1994-11-30
    • Thomas Tillander
    • Thomas Tillander
    • F23N1/02F23N5/18
    • F23N1/022F23N5/184F23N2005/181F23N2021/10F23N2025/21F23N2035/06F23N2035/12Y02E20/348
    • An integrated fuel-to-air control system is disclosed in which fuel and air pressure differential sensors are provided for measuring the flow pressure differential of fuel and air across orifices in the respective flow paths. The pressure differential sensors generate signals which are characteristic of the pressure differentials across the orifices.A control system is provided which includes an electronic comparator for receiving the pressure differential signals and generating a difference signal corresponding to the difference between these signals. The difference signal in turn is transmitted to a valve actuator which respectively opens or closes a valve in the fuel flow path in order to vary the fuel flow pressure differential so as to achieve a desired fuel-to-air ratio with the oxidant flow pressure differential. The fuel flow pressure is varied up or down as necessary until the difference signal reaches zero at the desired ratio.The present invention may include a temperature sensor which communicates a temperature signal for pre-heated air to the control system. The control system responds to the temperature signal by compensating the fuel flow to correspond to temperature-related changes in air density which affect the fuel-to-air ratio. The present invention also includes means for decreasing the fuel flow automatically so as to create an excess of air for air pressures below the excess air breakpoint.
    • 公开了一种集成的燃料 - 空气控制系统,其中提供燃料和空气压力差动传感器,用于测量相应流动路径中的喷口之间的燃料和空气的流量压差。 压力差传感器产生了通过孔口的压差特征的信号。 提供一种控制系统,其包括用于接收压差信号的电子比较器,并产生与这些信号之间的差相对应的差分信号。 差分信号又被传递到阀致动器,其分别打开或关闭燃料流动路径中的阀,以便改变燃料流量压差,从而实现与氧化剂流量压差的期望的燃料 - 空气比 。 燃料流量压力根据需要上升或下降,直到差分信号以期望的比例达到零。 本发明可以包括将预热空气的温度信号传递到控制系统的温度传感器。 控制系统通过补偿燃料流量来响应温度信号,以对应于影响燃料与空气比的空气密度的温度相关变化。 本发明还包括用于自动降低燃料流量以便为低于过量空气断点的空气压力产生过量空气的装置。
    • 8. 发明授权
    • Method of detecting a partial flame failure in a gas turbine engine and a gas turbine engine
    • 一种检测燃气涡轮发动机和燃气涡轮发动机中部分火焰故障的方法
    • US08474269B2
    • 2013-07-02
    • US12524788
    • 2008-01-28
    • Vili Panov
    • Vili Panov
    • F02C9/28
    • F23N5/102F01D21/003F02C7/262F23N5/242F23N2025/16F23N2025/21F23N2031/06F23N2041/20Y02T50/677
    • A method of detecting a partial flame failure in a gas turbine is provided. The method includes a gas duct to guide a propulsion gas and several combustors, each combustor leads into the gas duct and includes a burner. The method includes measuring a first temperature over time at each of at least two probing points located downstream from the combustors in the gas duct, measuring a second temperature over time in each of at least two of the burners, and detecting a partial flame failure from the first temperature measurements and the second temperature measurements, wherein the detecting of a partial flame failure includes determining a first detection parameter, the first detection parameter is determined from a rate of change of a variation between the first temperature measurements at different probing points. A gas turbine including temperature sensors to detect a partial flame failure is also provided.
    • 提供了一种在燃气轮机中检测局部火焰故障的方法。 该方法包括用于引导推进气体和几个燃烧器的气体管道,每个燃烧器引入气体管道并且包括燃烧器。 该方法包括在位于气体管道中的燃烧器下游的至少两个探测点中的每一个处测量第一温度,测量至少两个燃烧器中的每一个中随时间推移的第二温度,并且检测部分火焰故障 第一温度测量和第二温度测量,其中部分火焰故障的检测包括确定第一检测参数,从不同探测点处的第一温度测量之间的变化的变化率确定第一检测参数。 还提供了包括用于检测局部火焰故障的温度传感器的燃气轮机。
    • 9. 发明授权
    • Flare stack adapted to heat incoming fuel
    • 适用于加热进入燃料的火炬烟囱
    • US07981200B2
    • 2011-07-19
    • US12907736
    • 2010-10-19
    • E. Todd WigginsD. Jeffrey Hill
    • E. Todd WigginsD. Jeffrey Hill
    • B01D53/14
    • F23N1/002F23G7/085F23J2213/203F23N2025/19F23N2025/21Y02E20/12
    • A flare stack that preferably comprises a burner assembly, an exhaust stack, an housing, and a fuel line. The burner assembly burns a fuel to generate thermal energy and combustion byproducts. The exhaust stack is cooperatively associated with the burner assembly to direct the thermal energy and combustion byproducts away from the burner assembly. The housing at least partially defines a fluid-receiving chamber in thermal communication with the exhaust stack. The fluid-receiving chamber has a heat-transfer fluid disposed therein. The fuel line is in fluid communication with the burner assembly to deliver fuel to the burner assembly. At least a portion of the fuel line is in thermal communication with at least one of the exhaust stack, housing, or heat-transfer fluid to permit fuel in the fuel line to absorb thermal energy before reaching the burner assembly. In one embodiment, the burner assembly includes a pressure-variable burner to increase the rate of fuel consumption of the burner in relation to the pressure in the fuel line. In the preferred embodiment, the housing has an inlet and an outlet formed therethrough in fluid communication with the fluid-receiving chamber. The inlet permits heat-transfer fluid to flow into the fluid-receiving chamber to absorb thermal energy from the exhaust stack, and the outlet permits heat-transfer fluid to flow out of the fluid-receiving chamber.
    • 优选地包括燃烧器组件,排气叠层,壳体和燃料管线的火炬烟囱。 燃烧器组件燃烧燃料以产生热能和燃烧副产物。 废气堆叠与燃烧器组件协作地关联以将热能和燃烧副产物远离燃烧器组件。 壳体至少部分地限定与废气堆叠热连通的流体接收室。 流体接收室具有设置在其中的传热流体。 燃料管线与燃烧器组件流体连通以将燃料输送到燃烧器组件。 燃料管线的至少一部分与排气叠层,壳体或传热流体中的至少一个热连通,以允许燃料管线中的燃料在到达燃烧器组件之前吸收热能。 在一个实施例中,燃烧器组件包括压力可变燃烧器,以相对于燃料管线中的压力增加燃烧器的燃料消耗率。 在优选实施例中,壳体具有与流体接收室流体连通的通过其形成的入口和出口。 入口允许热传递流体流入流体接收室以吸收来自排气叠层的热能,并且出口允许热传递流体流出流体接收室。