SYSTEM AND METHOD FOR OPERATING A POWER PLANT
    3.
    发明申请
    SYSTEM AND METHOD FOR OPERATING A POWER PLANT 有权
    用于操作发电厂的系统和方法

    公开(公告)号:US20140238039A1

    公开(公告)日:2014-08-28

    申请号:US14037268

    申请日:2013-09-25

    CPC classification number: F02C7/236 F02C3/04 F02C3/045 F02C7/22 F02C9/40

    Abstract: A system including a fuel-supply system including, an auxiliary-fuel-gas compressor configured to compress a fuel for use by a gas-turbine system, an expander configured to generate power by expanding an oxidant from the gas-turbine system, and a motor/generator configured to function in a motor mode and in a generator mode, wherein the motor/generator drives fuel compression with the auxiliary fuel-gas compressor in the motor mode, and the motor/generator generates power in the generator mode as the expander uses oxidant from the gas-turbine system to drive the motor/generator

    Abstract translation: 一种包括燃料供给系统的系统,包括:构造成压缩由燃气轮机系统使用的燃料的辅助燃料气体压缩机;膨胀机,其构造成通过从所述燃气轮机系统膨胀氧化剂而发电;以及 电动机/发电机被配置为在电动机模式和发电机模式下起作用,其中电动机/发电机在电动机模式下利用辅助燃料气体压缩机驱动燃料压缩,并且电动发电机以发电机模式发电,作为膨胀机 使用来自燃气轮机系统的氧化剂来驱动电动机/发电机

    Inlet Bleed Heat System with Integrated Air Knife/Silencer Panels
    5.
    发明申请
    Inlet Bleed Heat System with Integrated Air Knife/Silencer Panels 有权
    入口排气热系统与集成气刀/消音器面板

    公开(公告)号:US20140123674A1

    公开(公告)日:2014-05-08

    申请号:US13669478

    申请日:2012-11-06

    Abstract: The present application provides an inlet bleed heat system for supplying a flow of bleed air to a flow of incoming air into a compressor of a gas turbine engine. The inlet bleed heat system may include an air knife and a silencer panel. The air knife may include a compressor bleed air port in communication with the flow of bleed air and a discharge gap to discharge the flow of bleed air into the flow of incoming air. The air knife may and the silencer panel may form an integrated air knife/silencer panel.

    Abstract translation: 本申请提供了一种入口放气加热系统,用于将进气流输送到燃气涡轮发动机的压缩机中。 入口放气加热系统可以包括气刀和消声器面板。 气刀可以包括与排放气流连通的压缩机排气口和排放间隙,以将排出的空气流进入进入的空气流中。 气刀可以和消音器面板可以形成一体的气刀/消声器面板。

    SYSTEM AND METHOD FOR OPERATING A POWER PLANT
    6.
    发明申请
    SYSTEM AND METHOD FOR OPERATING A POWER PLANT 审中-公开
    用于操作发电厂的系统和方法

    公开(公告)号:US20170022902A1

    公开(公告)日:2017-01-26

    申请号:US15282635

    申请日:2016-09-30

    CPC classification number: F02C7/236 F02C3/04 F02C3/045 F02C7/22 F02C9/40

    Abstract: A system including a fuel-supply system including, an auxiliary-fuel-gas compressor configured to compress a fuel for use by a gas-turbine system, an expander configured to generate power by expanding an oxidant from the gas-turbine system, and a motor/generator configured to function in a motor mode and in a generator mode, wherein the motor/generator drives fuel compression with the auxiliary fuel-gas compressor in the motor mode, and the motor/generator generates power in the generator mode as the expander uses oxidant from the gas-turbine system to drive the motor/generator

    Abstract translation: 一种包括燃料供给系统的系统,包括:构造成压缩由燃气轮机系统使用的燃料的辅助燃料气体压缩机;膨胀机,其构造成通过从所述燃气轮机系统膨胀氧化剂而发电;以及 电动机/发电机被配置为在电动机模式和发电机模式下起作用,其中电动机/发电机在电动机模式下利用辅助燃料气体压缩机驱动燃料压缩,并且电动发电机以发电机模式发电,作为膨胀机 使用来自燃气轮机系统的氧化剂来驱动电动机/发电机

    System and method for operating a power plant
    7.
    发明授权
    System and method for operating a power plant 有权
    运行发电厂的系统和方法

    公开(公告)号:US09464576B2

    公开(公告)日:2016-10-11

    申请号:US14037268

    申请日:2013-09-25

    CPC classification number: F02C7/236 F02C3/04 F02C3/045 F02C7/22 F02C9/40

    Abstract: A system including a fuel-supply system including, an auxiliary-fuel-gas compressor configured to compress a fuel for use by a gas-turbine system, an expander configured to generate power by expanding an oxidant from the gas-turbine system, and a motor/generator configured to function in a motor mode and in a generator mode, wherein the motor/generator drives fuel compression with the auxiliary fuel-gas compressor in the motor mode, and the motor/generator generates power in the generator mode as the expander uses oxidant from the gas-turbine system to drive the motor/generator.

    Abstract translation: 一种包括燃料供给系统的系统,包括:构造成压缩由燃气轮机系统使用的燃料的辅助燃料气体压缩机;膨胀机,其构造成通过从所述燃气轮机系统膨胀氧化剂而发电;以及 电动机/发电机被配置为在电动机模式和发电机模式下起作用,其中电动机/发电机在电动机模式下利用辅助燃料气体压缩机驱动燃料压缩,并且电动发电机以发电机模式发电,作为膨胀机 使用来自燃气轮机系统的氧化剂来驱动电动机/发电机。

    GAS TURBINE INLET AIR CONDITIONING COIL SYSTEM
    8.
    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

    Abstract: 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.

    Abstract translation: 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。

    GAS TURBINE SYSTEM AND METHOD
    9.
    发明申请
    GAS TURBINE SYSTEM AND METHOD 审中-公开
    气体涡轮机系统和方法

    公开(公告)号:US20160273456A1

    公开(公告)日:2016-09-22

    申请号:US14768431

    申请日:2013-10-16

    Abstract: A fuel supply system includes a first fuel gas compressor coupled to a fuel gas compressor shaft and configured to pressurize a fuel for a gas turbine system. A clutch is coupled to the fuel gas compressor shaft and is configured to selectively engage the fuel gas compressor shaft with a turbine shaft of the gas turbine system. An electromechanical machine is configured to operator as a motor to drive the fuel gas compressor shaft or to operate as a generator driven by the turbine shaft to generator power, based on an operating condition of the gas turbine system.

    Abstract translation: 燃料供应系统包括耦合到燃料气体压缩机轴并被配置为对燃气轮机系统的燃料加压的第一燃料气体压缩机。 离合器联接到燃料气体压缩机轴并且构造成选择性地将燃料气体压缩机轴与燃气轮机系统的涡轮轴接合。 机电机构被配置为基于燃气轮机系统的操作条件,作为电动机操作以驱动燃料气体压缩机轴或作为由涡轮机轴驱动的发电机运行以发电机功率。

    GAS TURBINE INLET HAVING INTEGRATED COILS AND MIST REDUCING VANES
    10.
    发明申请
    GAS TURBINE INLET HAVING INTEGRATED COILS AND MIST REDUCING VANES 审中-公开
    具有集成线圈和减雾器的气体涡轮机入口

    公开(公告)号:US20150308338A1

    公开(公告)日:2015-10-29

    申请号:US14117661

    申请日:2013-01-11

    CPC classification number: F02C7/12 F01D25/32 F28F1/32 F28F17/00

    Abstract: An integrated coil and fin system in a gas turbine inlet. The integrated system includes at least one wavy, non-planar, fin integrated with at least one heating/cooling coil, wherein the at least one coil is configured to heat or cool air moving through the gas turbine inlet, and wherein the at least one non-planar fin is configured to remove moisture in the air moving through the gas turbine inlet. In one embodiment, at least one hook can be included at an end or along a length of at least one non-planar fin.

    Abstract translation: 燃气轮机入口中的集成线圈和翅片系统。 集成系统包括与至少一个加热/冷却盘管集成的至少一个波浪形非平面翅片,其中至少一个线圈构造成加热或冷却通过燃气轮机入口移动的空气,并且其中至少一个 非平面翅片构造成去除移动通过燃气轮机入口的空气中的水分。 在一个实施例中,至少一个钩可以包括在至少一个非平面翅片的一端或一段长度上。

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