Carbon Dioxide Refrigeration Cycle
    1.
    发明申请
    Carbon Dioxide Refrigeration Cycle 有权
    二氧化碳制冷循环

    公开(公告)号:US20140090405A1

    公开(公告)日:2014-04-03

    申请号:US13644177

    申请日:2012-10-03

    IPC分类号: F25B1/06

    摘要: A refrigeration cycle is operated in conjunction with various thermodynamic cycle working fluid circuits to cool a target fluid that may be used in a separate system or duty. In one embodiment, the refrigeration cycle includes an ejector that extracts a motive fluid from the working fluid cycles in order to entrain a suction fluid that is also extracted from the working fluid circuits. Expanding the suction fluid reduces the pressure and temperature of the suction fluid for cooling the target fluid in an evaporator, which evaporates the suction fluid before being entrained into the ejector by the motive fluid. A mixed fluid is discharged from the ejector and injected into the working fluid circuits upstream from a condenser that cools the mixed fluid and the working fluid circulating throughout the working fluid circuits.

    摘要翻译: 制冷循环与各种热力循环工作流体回路结合运行,以冷却可在单独的系统或任务中使用的目标流体。 在一个实施例中,制冷循环包括喷射器,其从工作流体循环中提取运动流体,以便夹带也从工作流体回路中提取的抽吸流体。 膨胀吸入流体减少了用于冷却蒸发器中的目标流体的抽吸流体的压力和温度,蒸发器在被运动流体夹带到喷射器之前蒸发吸入流体。 混合流体从喷射器排出并注入到冷凝器上游的工作流体回路中,该冷凝器冷却混合流体和在整个工作流体回路中循环的工作流体。

    PARALLEL CYCLE HEAT ENGINES
    3.
    发明申请
    PARALLEL CYCLE HEAT ENGINES 有权
    并联循环热发动机

    公开(公告)号:US20120131920A1

    公开(公告)日:2012-05-31

    申请号:US13212631

    申请日:2011-08-18

    IPC分类号: F01K27/02 F01K25/00 F01K25/08

    摘要: Waste heat energy conversion cycles, systems and devices use multiple waste heat exchangers arranged in series in a waste heat stream, and multiple thermodynamic cycles run in parallel with the waste heat exchangers in order to maximize thermal energy extraction from the waste heat stream by a working fluid. The parallel cycles operate in different temperature ranges with a lower temperature work output used to drive a working fluid pump. A working fluid mass management system is integrated into or connected to the cycles.

    摘要翻译: 废热转换循环,系统和装置使用多个排放在废热流中的废热交换器,并且多个热力循环与废热交换器并联运行,以便通过工作来最大限度地从废热流中提取热能 流体。 并联循环在不同的温度范围内工作,较低温度的工作输出用于驱动工作流体泵。 工作流体质量管理系统集成到或连接到循环。

    DRIVEN STARTER PUMP AND START SEQUENCE
    4.
    发明申请
    DRIVEN STARTER PUMP AND START SEQUENCE 有权
    驱动起动器泵和起动序列

    公开(公告)号:US20120131919A1

    公开(公告)日:2012-05-31

    申请号:US13205082

    申请日:2011-08-08

    IPC分类号: F01K13/02

    摘要: Various thermodynamic power-generating cycles are disclosed. A turbopump arranged in the cycles is started and ramped-up using a starter pump arranged in parallel with the main pump of the turbopump. Once the turbopump is able to self-sustain, a series of valves may be manipulated to deactivate the starter pump and direct additional working fluid to a power turbine for generating electrical power.

    摘要翻译: 公开了各种热力发电循环。 启动循环中布置的涡轮泵,并使用与涡轮泵的主泵平行布置的起动泵升高。 一旦涡轮泵能够自维持,可以操纵一系列阀来停用启动泵,并将额外的工作流体引导到动力涡轮机以产生电力。

    Carbon dioxide refrigeration cycle
    6.
    发明授权
    Carbon dioxide refrigeration cycle 有权
    二氧化碳制冷循环

    公开(公告)号:US09062898B2

    公开(公告)日:2015-06-23

    申请号:US13644177

    申请日:2012-10-03

    IPC分类号: F25B1/06

    摘要: A refrigeration cycle is operated in conjunction with various thermodynamic cycle working fluid circuits to cool a target fluid that may be used in a separate system or duty. In one embodiment, the refrigeration cycle includes an ejector that extracts a motive fluid from the working fluid cycles in order to entrain a suction fluid that is also extracted from the working fluid circuits. Expanding the suction fluid reduces the pressure and temperature of the suction fluid for cooling the target fluid in an evaporator, which evaporates the suction fluid before being entrained into the ejector by the motive fluid. A mixed fluid is discharged from the ejector and injected into the working fluid circuits upstream from a condenser that cools the mixed fluid and the working fluid circulating throughout the working fluid circuits.

    摘要翻译: 制冷循环与各种热力循环工作流体回路结合运行,以冷却可在单独的系统或任务中使用的目标流体。 在一个实施例中,制冷循环包括喷射器,其从工作流体循环中提取运动流体,以便夹带也从工作流体回路中提取的抽吸流体。 膨胀吸入流体减少了用于冷却蒸发器中的目标流体的抽吸流体的压力和温度,蒸发器在被运动流体夹带到喷射器之前蒸发吸入流体。 混合流体从喷射器排出并注入到冷凝器上游的工作流体回路中,该冷凝器冷却混合流体和在整个工作流体回路中循环的工作流体。

    METHODS AND APPARATUS TO FACILITATE DECREASING COMBUSTOR ACOUSTICS
    7.
    发明申请
    METHODS AND APPARATUS TO FACILITATE DECREASING COMBUSTOR ACOUSTICS 有权
    方法和装置,以减少化学反应器的声学

    公开(公告)号:US20080229753A1

    公开(公告)日:2008-09-25

    申请号:US11689759

    申请日:2007-03-22

    IPC分类号: F02C3/04

    CPC分类号: F23R3/343 F23R3/14 F23R3/26

    摘要: A method for operating a gas turbine engine including a compressor and a combustor is provided. The method comprises channeling between about 0% to about 8% of the total airflow discharged from a compressor towards a pilot swirler coupled within the burner, wherein the burner includes a main swirler and an annular centerbody extending between the pilot and main swirlers, injecting a portion of the total fuel flow supplied to the burner through a plurality of apertures defined in a hollow pilot centerbody coupled within the pilot swirler, channeling the remaining airflow discharged from the compressor towards the main swirler, and injecting the remaining fuel flow supplied to the burner through at least one main swirler vane coupled within the main swirler, such that the portion of fuel is pre-mixed with a portion of the total airflow.

    摘要翻译: 提供了一种用于操作包括压缩机和燃烧器的燃气涡轮发动机的方法。 该方法包括将从压缩机排出的总气流的约0%至约8%引导至连接在燃烧器内的先导式旋流器,其中燃烧器包括主旋流器和在飞行员和主旋流器之间延伸的环形中心体, 通过被连接在先导式旋流器内的中空先导中心体中限定的多个孔口供应到燃烧器的总燃料流量的一部分,将从压缩机排出的剩余气流引导到主旋流器,以及喷射供应到燃烧器的剩余燃料流 通过联接在主旋流器内的至少一个主旋流器叶片,使得燃料的一部分与总气流的一部分预混合。

    Apparatus to facilitate decreasing combustor acoustics
    9.
    发明授权
    Apparatus to facilitate decreasing combustor acoustics 有权
    便于降低燃烧器声学的装置

    公开(公告)号:US07905093B2

    公开(公告)日:2011-03-15

    申请号:US11689759

    申请日:2007-03-22

    IPC分类号: F02C1/00

    CPC分类号: F23R3/343 F23R3/14 F23R3/26

    摘要: A method for operating a gas turbine engine including a compressor and a combustor is provided. The method comprises channeling between about 0% to about 8% of the total airflow discharged from a compressor towards a pilot swirler coupled within the burner, wherein the burner includes a main swirler and an annular centerbody extending between the pilot and main swirlers, injecting a portion of the total fuel flow supplied to the burner through a plurality of apertures defined in a hollow pilot centerbody coupled within the pilot swirler, channeling the remaining airflow discharged from the compressor towards the main swirler, and injecting the remaining fuel flow supplied to the burner through at least one main swirler vane coupled within the main swirler, such that the portion of fuel is pre-mixed with a portion of the total airflow.

    摘要翻译: 提供了一种用于操作包括压缩机和燃烧器的燃气涡轮发动机的方法。 该方法包括将从压缩机排出的总气流的约0%至约8%引导至连接在燃烧器内的先导式旋流器,其中燃烧器包括主旋流器和在飞行员和主旋流器之间延伸的环形中心体, 通过被连接在先导式旋流器内的中空先导中心体中限定的多个孔口供应到燃烧器的总燃料流量的一部分,将从压缩机排出的剩余气流引导到主旋流器,以及喷射供应到燃烧器的剩余燃料流 通过联接在主旋流器内的至少一个主旋流器叶片,使得燃料的一部分与总气流的一部分预混合。

    Combustor mixer having plasma generating nozzle
    10.
    发明授权
    Combustor mixer having plasma generating nozzle 失效
    具有等离子体生成喷嘴的燃烧器混合器

    公开(公告)号:US06453660B1

    公开(公告)日:2002-09-24

    申请号:US09764638

    申请日:2001-01-18

    IPC分类号: F02C7266

    摘要: A mixer assembly for use in a combustion chamber of a gas turbine engine. The mixer assembly includes a mixer housing having a hollow interior, an inlet and an outlet. The housing delivers a mixture of fuel and air through the outlet to the combustion chamber for burning. The mixer assembly includes a fuel nozzle assembly mounted in the housing having a fuel passage adapted for connection to a fuel supply. The passage extends to an outlet port for delivering fuel from the passage to the hollow interior of the mixer housing. The nozzle assembly includes a plasma generator for generating at least one of a dissociated fuel and an ionized fuel from the fuel delivered through the nozzle outlet port to the hollow interior of the housing.

    摘要翻译: 一种用于燃气涡轮发动机的燃烧室的混合器组件。 混合器组件包括具有中空内部,入口和出口的混合器壳体。 壳体通过出口将燃料和空气的混合物输送到燃烧室用于燃烧。 混合器组件包括安装在壳体中的燃料喷嘴组件,其具有适于连接到燃料供应的燃料通道。 通道延伸到出口,用于将燃料从通道输送到混合器壳体的中空内部。 喷嘴组件包括等离子体发生器,其用于从通过喷嘴出口输送的燃料产生离解燃料和离子化燃料中的至少一种到壳体的中空内部。