Turbomachine inlet heating system
    1.
    发明授权
    Turbomachine inlet heating system 有权
    涡轮机进气加热系统

    公开(公告)号:US08083466B2

    公开(公告)日:2011-12-27

    申请号:US12403444

    申请日:2009-03-13

    IPC分类号: F01D21/12

    摘要: A turbomachine system includes a compressor having a compressor intake and a compressor extraction outlet, and an inlet system fluidly connected to the compressor intake and the compressor extraction outlet. The inlet system includes a plenum having a first end portion that extends to a second end portion through an intermediate portion. The inlet system also includes a heating system having a plurality of conduits extending horizontally through the intermediate portion of the plenum and arranged in a vertical relationship. Heated air from the compressor extraction outlet passes through the plurality of conduits and raises a temperature of ambient air passing through the plenum and into the compressor intake.

    摘要翻译: 涡轮机系统包括具有压缩机进气口和压缩机排出口的压缩机,以及与压缩机进气口和压缩机排出口流体连接的入口系统。 入口系统包括具有通过中间部分延伸到第二端部的第一端部的增压室。 入口系统还包括加热系统,其具有水平延伸通过气室的中间部分并以垂直关系布置的多个管道。 来自压缩机排出口的加热空气通过多个管道,并且使经过集气室的环境空气的温度升高并进入压缩机进气口。

    TURBOMACHINE INLET HEATING SYSTEM
    2.
    发明申请
    TURBOMACHINE INLET HEATING SYSTEM 有权
    涡轮进气加热系统

    公开(公告)号:US20100232945A1

    公开(公告)日:2010-09-16

    申请号:US12403444

    申请日:2009-03-13

    IPC分类号: F01D25/08

    摘要: A turbomachine system includes a compressor having a compressor intake and a compressor extraction outlet, and an inlet system fluidly connected to the compressor intake and the compressor extraction outlet. The inlet system includes a plenum having a first end portion that extends to a second end portion through an intermediate portion. The inlet system also includes a heating system having a plurality of conduits extending horizontally through the intermediate portion of the plenum and arranged in a vertical relationship. Heated air from the compressor extraction outlet passes through the plurality of conduits and raises a temperature of ambient air passing through the plenum and into the compressor intake.

    摘要翻译: 涡轮机系统包括具有压缩机进气口和压缩机排出口的压缩机,以及与压缩机进气口和压缩机排出口流体连接的入口系统。 入口系统包括具有通过中间部分延伸到第二端部的第一端部的增压室。 入口系统还包括加热系统,其具有水平延伸通过气室的中间部分并以垂直关系布置的多个管道。 来自压缩机排出口的加热空气通过多个管道,并且使经过集气室的环境空气的温度升高并进入压缩机进气口。

    GAS TURBINE INLET AIR CONDITIONING COIL SYSTEM
    3.
    发明申请
    GAS TURBINE INLET AIR CONDITIONING COIL SYSTEM 审中-公开
    气体涡轮进口空调线圈系统

    公开(公告)号:US20160237902A1

    公开(公告)日:2016-08-18

    申请号:US14768428

    申请日:2013-11-05

    IPC分类号: F02C7/143 F02C7/057

    摘要: A system includes a gas turbine system, including an air intake system that includes a housing, a first plurality of air conditioning coils, a second plurality of air conditioning coils that is downstream relative to the first plurality, and a baffle extending between each of the first and second pluralities of air conditioning coils, wherein the baffle is configured to direct an air flow through the first or second pluralities of air conditioning coils in a closed position, and the baffle is configured to enable air flow to bypass the first and second pluralities of coils in an opened position.

    摘要翻译: 一种系统包括燃气轮机系统,其包括进气系统,其包括壳体,第一多个空调线圈,相对于第一多个下游的第二多个空调线圈,以及在每个 第一和第二多个空调线圈,其中所述挡板构造成在关闭位置引导空气流通过所述第一或第二多个空调线圈,并且所述挡板被配置为使空气流能够绕过所述第一和第二多个空调 的线圈处于打开位置。

    SYSTEM FOR TURBINE COMBUSTOR FUEL MIXING
    5.
    发明申请
    SYSTEM FOR TURBINE COMBUSTOR FUEL MIXING 有权
    涡轮机燃油混合系统

    公开(公告)号:US20130097991A1

    公开(公告)日:2013-04-25

    申请号:US13280216

    申请日:2011-10-24

    IPC分类号: F02C7/22

    摘要: A system includes a mixing assembly configured to mix a liquid fuel and a water to generate a fuel mixture. The fuel mixture is configured to combust in a combustor of a gas turbine. The mixing assembly includes a liquid fuel passage disposed in an integrated housing. The liquid fuel passage is configured to flow the liquid fuel and to exclude liquid traps. The mixing assembly also includes a water passage disposed in the integrated housing. The water passage is configured to flow the water and to exclude liquid traps. The mixing assembly also includes a mixer disposed in the integrated housing and coupled to the liquid fuel passage and the water passage. The mixer is configured to mix the liquid fuel and the water to form the fuel mixture.

    摘要翻译: 一种系统包括配置成混合液体燃料和水以产生燃料混合物的混合组件。 燃料混合物构造成在燃气轮机的燃烧器中燃烧。 混合组件包括设置在一体化壳体中的液体燃料通道。 液体燃料通道构造成流动液体燃料并排除液体捕集阱。 混合组件还包括设置在一体式壳体中的水通道。 水通道构造成流过水并排除液体捕集阱。 混合组件还包括设置在一体式壳体中并耦合到液体燃料通道和水通道的混合器。 混合器配置成混合液体燃料和水以形成燃料混合物。

    SYSTEM AND METHOD FOR DETERMINING A FLAME CONDITION IN A COMBUSTOR
    8.
    发明申请
    SYSTEM AND METHOD FOR DETERMINING A FLAME CONDITION IN A COMBUSTOR 审中-公开
    用于确定燃烧器中火焰条件的系统和方法

    公开(公告)号:US20120088197A1

    公开(公告)日:2012-04-12

    申请号:US12900668

    申请日:2010-10-08

    IPC分类号: F23C99/00

    摘要: A system for determining a flame condition in a combustor includes a pressure sensor that generates a pressure signal reflective of a pressure in the combustor. A controller receives the pressure signal and generates a flame signal reflective of the flame condition in the combustor. A method for determining a flame condition in a combustor includes measuring a pressure in the combustor, comparing the measured pressure in the combustor to a predetermined limit, and generating a flame signal based on the comparison of the measured pressure in the combustor to the predetermined limit, wherein the flame signal reflects the flame condition in the combustor.

    摘要翻译: 用于确定燃烧器中的火焰状态的系统包括产生反映燃烧器中的压力的​​压力信号的压力传感器。 控制器接收压力信号并产生反映燃烧器中的火焰状态的火焰信号。 一种用于确定燃烧器中的火焰状态的方法,包括测量燃烧器中的压力,将燃烧器中的测量压力与预定极限进行比较,并且基于将燃烧器中的测量压力与预定极限的比较来产生火焰信号 其中火焰信号反映燃烧器中的火焰状态。

    Turbomachine passage cleaning system
    10.
    发明授权
    Turbomachine passage cleaning system 有权
    涡轮机通道清洗系统

    公开(公告)号:US09376931B2

    公开(公告)日:2016-06-28

    申请号:US13359962

    申请日:2012-01-27

    IPC分类号: F04D29/58 F01D25/00

    摘要: A turbomachine passage cleaning system includes a first airflow passage having a first inlet configured and disposed to fluidly connect to a compressor portion, a first outlet configured and disposed to fluidly connect to a turbine portion, and a first intermediate portion including a first strainer. A second airflow passage is fluidly coupled to the first airflow passage. The second airflow passage has a second intermediate portion having second strainer. A first valve is arranged in the first intermediate portion upstream from the first strainer, and a second valve is arranged in the second intermediate portion upstream from the second strainer. The first and second valves are selectively operated to control fluid flow into respective ones of the first and second airflow passages to filter air passing from a turbomachine compressor portion to a turbomachine turbine portion.

    摘要翻译: 涡轮机通道清洁系统包括第一气流通道,其具有构造和设置成流体连接到压缩机部分的第一入口,被配置和设置成流体连接到涡轮机部分的第一出口和包括第一过滤器的第一中间部分。 第二气流通道流体地联接到第一气流通道。 第二气流通道具有具有第二过滤器的第二中间部分。 第一阀布置在第一过滤器上游的第一中间部分中,并且第二阀布置在第二过滤器上游的第二中间部分中。 选择性地操作第一阀和第二阀以控制流入第一和第二气流通道中的相应流体的流体,以过滤从涡轮机压缩机部分流到涡轮机涡轮机部分的空气。