TURBOMACHINE SYSTEM INCLUDING AN INLET BLEED HEAT SYSTEM AND METHOD OF OPERATING A TURBOMACHINE AT PART LOAD
    81.
    发明申请
    TURBOMACHINE SYSTEM INCLUDING AN INLET BLEED HEAT SYSTEM AND METHOD OF OPERATING A TURBOMACHINE AT PART LOAD 审中-公开
    涡轮发动机系统,包括入口加热系统和部分负载运行涡轮机的方法

    公开(公告)号:US20160040596A1

    公开(公告)日:2016-02-11

    申请号:US14455112

    申请日:2014-08-08

    Abstract: A turbomachine system includes a compressor portion having at least one compressor extraction, a turbine portion operatively connected to the compressor portion, and a combustor assembly including at least one combustor fluidically connected to the compressor portion and the turbine portion. A heat recovery steam generator (HRSG) is fluidically connected to the turbine portion, and an air inlet system is fluidically connected to the compressor portion. An inlet bleed heat (IBH) system is fluidically connected to each of the compressor portion, the air inlet system and the HRSG. An inlet bleed heat (IBH) system includes a first conduit having a first valve fluidically connecting the compressor extraction and the air inlet system, and a second conduit including a second valve connecting one of the HRSG and a secondary stream source with the first conduit.

    Abstract translation: 涡轮机系统包括具有至少一个压缩机抽出的压缩机部分,可操作地连接到压缩机部分的涡轮部分,以及包括流体连接到压缩机部分和涡轮机部分的至少一个燃烧器的燃烧器组件。 热回收蒸汽发生器(HRSG)流体地连接到涡轮部分,并且空气入口系统流体地连接到压缩机部分。 入口放热(IBH)系统流体连接到压缩机部分,进气系统和HRSG中的每一个。 入口放热(IBH)系统包括具有流体连接压缩机抽出和空气入口系统的第一阀的第一管道和包括连接HRSG和次流源之一与第一管道的第二阀的第二管道。

    Gas turbine under frequency response improvement system and method
    82.
    发明授权
    Gas turbine under frequency response improvement system and method 有权
    燃气轮机在频率响应改进系统和方法下

    公开(公告)号:US09209730B2

    公开(公告)日:2015-12-08

    申请号:US13751689

    申请日:2013-01-28

    Abstract: A system and method is provided that improves the under frequency response of gas turbines by providing a fast-response power augmentation system. The system includes a tank storing a blended mixture of motive fuel such as ethanol or methanol and demineralized water in a predetermined ratio that is provided as a diluent to be injected into the compressor bellmouth, the Compressor Discharge Chamber (CDC), and/or the combustion system via one to three dedicated circuits. To achieve the instantaneous injection of the diluent at the correct pressure and for the appropriate duration to meet the needs of the gas turbine Grid compliance mandate, an accumulator is used as the motive force to drive the augmentation fluid in the dedicated circuits. The injected diluent is microprocessor controlled to either be simultaneous into all three circuits or is sequenced based on a determination of the best turbine control and performance.

    Abstract translation: 提供了一种通过提供快速响应功率增加系统来改善燃气轮机的低频响应的系统和方法。 该系统包括储存燃料如乙醇或甲醇的混合混合物和预定比例的软化水的罐,其作为要注入压缩机喇叭口的稀释剂,压缩机排放室(CDC)和/或 燃烧系统通过一到三个专用电路。 为了实现在正确压力下的适当持续时间的稀释剂的瞬时注入,以满足燃气轮机电网顺应性要求的需要,使用蓄能器作为驱动专用电路中的增压流体的动力。 喷射的稀释剂是微处理器控制的,以便同时进入所有三个电路,或者基于确定最佳涡轮机控制和性能进行排序。

    SYSTEMS AND METHODS FOR PREHEATING FUEL FOR GAS TURBINE ENGINES
    83.
    发明申请
    SYSTEMS AND METHODS FOR PREHEATING FUEL FOR GAS TURBINE ENGINES 审中-公开
    用于燃气涡轮发动机燃料预热的系统和方法

    公开(公告)号:US20150345401A1

    公开(公告)日:2015-12-03

    申请号:US14290608

    申请日:2014-05-29

    Abstract: Systems and methods for preheating fuel in a gas turbine engine are provided. In one embodiment, a system may include a gas turbine engine, a fuel line in fluid communication with the gas turbine engine, a gas turbine compartment disposed about the gas turbine engine, and a first conduit in fluid communication with the gas turbine compartment. The first conduit may include ventilation discharge air from the gas turbine compartment. The system also may include a first heat exchanger in communication with the fuel line and the first conduit. The first heat exchanger may be configured to exchange heat between the fuel and the ventilation discharge air from the gas turbine compartment.

    Abstract translation: 提供了一种用于在燃气涡轮发动机中预热燃料的系统和方法。 在一个实施例中,系统可以包括燃气涡轮发动机,与燃气涡轮发动机流体连通的燃料管路,围绕燃气涡轮发动机设置的燃气涡轮机室,以及与燃气涡轮机室流体连通的第一导管。 第一导管可以包括来自燃气轮机室的通风排放空气。 该系统还可以包括与燃料管线和第一管道连通的第一热交换器。 第一热交换器可以被配置为在燃料和来自燃气轮机室的通风排放空气之间交换热量。

    SYSTEMS AND METHODS FOR UTILIZING GAS TURBINE COMPARTMENT VENTILATION DISCHARGE AIR
    84.
    发明申请
    SYSTEMS AND METHODS FOR UTILIZING GAS TURBINE COMPARTMENT VENTILATION DISCHARGE AIR 审中-公开
    采用气体涡轮机组通风排放空气的系统和方法

    公开(公告)号:US20150345393A1

    公开(公告)日:2015-12-03

    申请号:US14290580

    申请日:2014-05-29

    CPC classification number: F02C7/08 F01D25/145 F02C1/08 F02C7/047 F02C9/18

    Abstract: Systems and methods for utilizing gas turbine compartment ventilation discharge air. In one embodiment, a system may include a gas turbine engine having a compressor. The system also may include a gas turbine compartment disposed about the gas turbine engine. Moreover, the system may include an inlet bleed heat (IBH) manifold in fluid communication with the compressor. The gas turbine compartment may be in fluid communication with the IBH manifold for providing the IBH manifold with ventilation discharge air from the gas turbine compartment.

    Abstract translation: 利用燃气轮机室通风排气的系统和方法。 在一个实施例中,系统可以包括具有压缩机的燃气涡轮发动机。 该系统还可以包括围绕燃气涡轮发动机设置的燃气轮机室。 此外,系统可以包括与压缩机流体连通的入口放热(IBH)歧管。 燃气轮机室可以与IBH歧管流体连通,以向IBH歧管提供来自燃气轮机室的通风排放空气。

    Method and apparatus for refurbishing turbine components
    85.
    发明授权
    Method and apparatus for refurbishing turbine components 有权
    涡轮机组件翻新的方法和装置

    公开(公告)号:US09163322B2

    公开(公告)日:2015-10-20

    申请号:US13932341

    申请日:2013-07-01

    CPC classification number: C25F3/16 B23H9/10 C25F7/00

    Abstract: A refurbishing method, refurbishing apparatus and refurbished article are provided. The refurbishing method includes accessing a plurality of rotatable components attached to a turbine assembly, the turbine assembly being a portion of a turbomachine, providing a predetermined volume of a buffered electrolytic solution in an electro-polishing tank, coupling the plurality of rotatable components to a power supply, immersing an immersion portion of at least one of the plurality of rotatable components in the buffered electrolytic solution, passing an electrical energy through the immersion portion of at least one of the plurality of rotatable components while the immersion portion is immersed in the buffered electrolytic solution, wherein an electrical flux to the immersion portion electro-polishes the immersion portion, separating the immersion portion from the buffered electrolytic solution, and applying a corrosion inhibitor to the plurality of rotatable components.

    Abstract translation: 提供翻新方法,翻新设备和翻新的物品。 翻新方法包括访问附接到涡轮机组件的多个可旋转部件,涡轮组件是涡轮机的一部分,在电抛光槽中提供预定体积的缓冲电解液,将多个可旋转部件连接到 电源,将所述多个可旋转部件中的至少一个的浸没部分浸入所述缓冲电解液中,使得所述浸没部分浸入所述缓冲电解液中的电能通过所述多个可旋转部件中的至少一个的所述浸没部分; 电解液,其中向浸渍部分的电流电浸渍浸渍部分,将浸没部分与缓冲电解液分离,并将腐蚀抑制剂施加到多个可旋转部件。

    SYSTEM ENCLOSURE VENTILATION MONITORING SYSTEM
    88.
    发明申请
    SYSTEM ENCLOSURE VENTILATION MONITORING SYSTEM 审中-公开
    系统外壳通风监测系统

    公开(公告)号:US20150056912A1

    公开(公告)日:2015-02-26

    申请号:US13971047

    申请日:2013-08-20

    CPC classification number: F24F11/76 F24F11/30 F24F2110/50 F24F2140/40

    Abstract: A system enclosure ventilation monitoring system includes a controller having an enclosure temperature input configured to receive signals indicating internal temperatures of the system enclosure, an air circulating device speed input configured to receive signals indicating operating speed of at least one air circulating device, and a damper position input configured to receive a damper position signal and an output. The controller is configured and disposed to set damper position through the output based on at least one of the air circulating device speed input and the enclosure temperature input.

    Abstract translation: 一种系统外壳通风监测系统,包括具有壳体温度输入的控制器,其被配置为接收指示系统外壳内部温度的信号;空气循环装置速度输入器,被配置为接收指示至少一个空气循环装置的操作速度的信号,以及阻尼器 位置输入被配置为接收阻尼器位置信号和输出。 控制器被配置和布置成基于空气循环装置速度输入和机壳温度输入中的至少一个来设置通过输出的阻尼器位置。

    SYSTEMS AND METHODS FOR WASHING A GAS TURBINE COMPRESSOR
    89.
    发明申请
    SYSTEMS AND METHODS FOR WASHING A GAS TURBINE COMPRESSOR 审中-公开
    用于洗涤气体涡轮压缩机的系统和方法

    公开(公告)号:US20140174474A1

    公开(公告)日:2014-06-26

    申请号:US13947319

    申请日:2013-07-22

    CPC classification number: F01D25/002 G01N17/008 G01N27/041

    Abstract: A method is provided for washing a compressor in a gas turbine. The method includes establishing a compressor fouling set point and sensing a fouling level in the compressor with a sensor. The fouling level is communicated to a control subsystem that determines a wash initiation instruction based on the fouling level and the compressor fouling set point. The wash initiation instruction is executed by initiating a wash with a fluid. A system is also disclosed including a compressor, an on-line wash system coupled to the compressor, and a compressor fouling sensor that senses a compressor fouling level. A source of washing fluid is provided, and a control subsystem that initiates a wash with washing fluid from the source of washing fluid based on a compressor fouling level.

    Abstract translation: 提供一种用于清洗燃气轮机中的压缩机的方法。 该方法包括建立压缩机污垢设定点并用传感器感测压缩机中的结垢水平。 污染水平被传送到控制子系统,该控制子系统基于污垢水平和压缩机污垢设定点来确定洗涤开始指令。 洗涤开始指令通过开始用流体洗涤来执行。 还公开了一种系统,其包括压缩机,耦合到压缩机的在线洗涤系统以及感测压缩机结垢水平的压缩机污垢传感器。 提供洗涤液的源,以及控制子系统,其基于压缩机结垢水平从洗涤液源引发洗涤液的洗涤。

    System to Improve Gas Turbine Output and Hot Gas Path Component Life Utilizing Humid Air for Nozzle Over Cooling
    90.
    发明申请
    System to Improve Gas Turbine Output and Hot Gas Path Component Life Utilizing Humid Air for Nozzle Over Cooling 审中-公开
    改善燃气轮机输出和热气路径的系统组件使用湿度空气进行冷却喷嘴

    公开(公告)号:US20140123666A1

    公开(公告)日:2014-05-08

    申请号:US13751675

    申请日:2013-01-28

    Abstract: A system to improve gas turbine output and extend the life of hot gas path components includes a subsystem for estimating an amount of water or steam to be added to the flow of air to achieve the desired hot gas path temperature. The system includes a water or steam injection component adapted to inject the amount of water or steam to the flow of air to generate a flow of humid air and an injection subsystem adapted to inject the flow of humid air into a nozzle at the turbine stage are also included. The system includes a temperature sensor disposed at a turbine stage, and a subsystem for determining a desired hot gas path temperature at the turbine stage. An extraction conduit is coupled to a compressor stage and is adapted to extract a flow of air.

    Abstract translation: 改进燃气轮机输出并延长热气路径部件寿命的系统包括用于估计要添加到空气流中以获得期望的热气路径温度的水或蒸汽的量的子系统。 该系统包括适于将水或蒸汽的量注入到空气流中以产生潮湿空气流的水或蒸汽注入组件,以及适于将潮湿空气流喷射到涡轮级的喷嘴中的喷射子系统 也包括在内。 该系统包括设置在涡轮级的温度传感器和用于确定涡轮机级期望的热气体路径温度的子系统。 提取管道耦合到压缩机级并且适于提取空气流。

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