Gas turbine under frequency response improvement system and method
    1.
    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。

    Method and apparatus for refurbishing turbine components
    2.
    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。

    Method And System For Determining Power Plant Machine Reliability
    5.
    发明申请
    Method And System For Determining Power Plant Machine Reliability 审中-公开
    确定电厂机器可靠性的方法和系统

    公开(公告)号:US20150106059A1

    公开(公告)日:2015-04-16

    申请号:US14052363

    申请日:2013-10-11

    CPC classification number: G01M15/14 G05B23/0283 G21D3/00 G21D2010/00 Y02E30/39

    Abstract: Disclosed are methods and systems to determine a power plant machine reliability forecast. In an embodiment, a method may comprise obtaining an environmental factor of a power plant machine based on geospatial data of a first area and location data of a second area, obtaining an operating factor of the power plant machine, and determining a reliability forecast based on the obtained environmental factor and the obtained operating factor.

    Abstract translation: 公开了确定发电厂机器可靠性预报的方法和系统。 在一个实施例中,一种方法可以包括基于第一区域的地理空间数据和第二区域的位置数据获得发电厂机器的环境因子,获得发电厂机器的运行因子,以及基于 获得的环境因素和获得的操作系数。

    Method And System For Determining Wind Turbine Reliability
    6.
    发明申请
    Method And System For Determining Wind Turbine Reliability 审中-公开
    确定风力发电机组可靠性的方法与系统

    公开(公告)号:US20150101401A1

    公开(公告)日:2015-04-16

    申请号:US14052405

    申请日:2013-10-11

    CPC classification number: G01W1/02 F03D17/00 F05B2260/821

    Abstract: Disclosed are methods and systems to determine a reliability forecast for a wind turbine. In an embodiment, a method may comprise obtaining an environmental factor of a wind turbine based on geospatial data of a first area and location data of a second area, obtaining an operating factor of the wind turbine, and determining a reliability forecast based on the environmental factor and the operating factor.

    Abstract translation: 公开了确定风力涡轮机的可靠性预报的方法和系统。 在一个实施例中,方法可以包括基于第一区域的地理空间数据和第二区域的位置数据获得风力涡轮机的环境因子,获得风力涡轮机的运行系数,以及基于环境来确定可靠性预测 因素和经营因素。

    Systems and Methods For Measuring Fouling in a Turbine System
    7.
    发明申请
    Systems and Methods For Measuring Fouling in a Turbine System 审中-公开
    用于测量涡轮机系统结垢的系统和方法

    公开(公告)号:US20140174163A1

    公开(公告)日:2014-06-26

    申请号:US13721718

    申请日:2012-12-20

    CPC classification number: G01M15/02 G01N17/008 G01N27/041

    Abstract: Systems and methods for measuring fouling in a gas turbine compressor include a conductivity resistance sensor disposed in a compressor inlet mouth. The degree of compressor fouling is correlated to changes in resistance measured by the conductivity resistance sensor. Measurements of resistance changes are converted to an indicia of fouling and used to trigger cleaning of the compressor.

    Abstract translation: 用于测量燃气轮机压缩机中的结垢的系统和方法包括设置在压缩机入口中的电导率传感器。 压缩机污染程度与由电阻率传感器测量的电阻变化相关。 电阻变化的测量被转换为污垢的标记,并用于触发压缩机的清洁。

    Systems and Methods for De-Icing a Gas Turbine Engine Inlet Screen and Dehumidifying Inlet Air Filters
    8.
    发明申请
    Systems and Methods for De-Icing a Gas Turbine Engine Inlet Screen and Dehumidifying Inlet Air Filters 有权
    燃气轮机发动机入口屏幕和除湿进气空气过滤器的系统和方法

    公开(公告)号:US20130340439A1

    公开(公告)日:2013-12-26

    申请号:US14011318

    申请日:2013-08-27

    CPC classification number: F02C7/047 F02C6/08 F02C6/18 F02C7/055

    Abstract: A system for de-icing a gas turbine engine is provided. A manifold is coupled to an inlet screen. A first conduit is coupled to a stage of the compressor and a first input of a mixing component. A second conduit is coupled to the exhaust and a second input of the mixing component. The second conduit being adapted to extract exhaust gases without increasing the pressure at the exhaust. A third conduit is coupled to the output of the mixing component and the manifold. A method for de-icing a gas turbine engine inlet screen includes determining a current temperature at the inlet screen, and determining a desired temperature at the inlet screen. If the current temperature at the inlet screen is less than the desired temperature at the inlet screen first flow rate of an air-exhaust mixture necessary to achieve the desired inlet screen temperature is calculated. The method also includes extracting an amount of exhaust gas from a turbine exhaust subsystem without increasing a pressure at the turbine exhaust subsystem, extracting an amount of air from a compressor stage, and mixing the amount of exhaust gas with the amount of air to generate an air-exhaust mixture that is conveyed to the inlet screen.

    Abstract translation: 提供了一种用于除燃气涡轮发动机的系统。 歧管联接到入口屏幕。 第一导管连接到压缩机的级和混合部件的第一输入端。 第二导管连接到排气口和混合部件的第二输入端。 第二导管适于在不增加排气压力的情况下提取废气。 第三导管连接到混合部件和歧管的输出端。 一种用于除燃燃气涡轮发动机入口屏幕的方法包括确定入口屏幕处的当前温度,以及确定入口屏幕处的期望温度。 如果入口筛网处的当前温度低于进口筛网所需的温度,则计算达到所需入口筛网温度所需的排气混合物的第一流量。 该方法还包括从涡轮机排气子系统中抽取一定量的废气而不增加涡轮排气子系统的压力,从压缩机级提取一定量的空气,并将废气量与空气量混合以产生 输送到入口屏幕的排气混合物。

    SYSTEMS AND METHODS FOR PASSIVELY PROVIDING ONE OR MORE FLOWS OF COOLING FLUID TO A HOT CAVITY WITHIN A COOLING CIRCUIT OF A GAS TURBINE ENGINE
    10.
    发明申请
    SYSTEMS AND METHODS FOR PASSIVELY PROVIDING ONE OR MORE FLOWS OF COOLING FLUID TO A HOT CAVITY WITHIN A COOLING CIRCUIT OF A GAS TURBINE ENGINE 审中-公开
    一种或多种冷却流体到燃气涡轮发动机冷却回路中的热空气的系统和方法

    公开(公告)号:US20160356221A1

    公开(公告)日:2016-12-08

    申请号:US14733251

    申请日:2015-06-08

    Abstract: A thermal valve is disclosed. The thermal valve may provide one or more flows of cooling fluid to a hot cavity within a cooling circuit of a gas turbine engine. The thermal valve may include a temperature sensitive element and a valve assembly in communication with the temperature sensitive element. The valve assembly may include at least one inlet in fluid communication with at least one cooling fluid source, at least one outlet in fluid communication with the hot cavity, and at least one valve in communication with the temperature sensitive element. The at least one valve may be disposed between the at least one inlet and the at least one outlet. The temperature sensitive element may be configured to move the at least one valve between a closed position and an open position.

    Abstract translation: 公开了一种热阀。 热阀可以向燃气涡轮发动机的冷却回路内的热腔提供一个或多个冷却流体流。 热阀可以包括温度敏感元件和与温度敏感元件连通的阀组件。 阀组件可以包括与至少一个冷却流体源流体连通的至少一个入口,与热腔流体连通的至少一个出口以及与温度敏感元件连通的至少一个阀。 所述至少一个阀可以设置在所述至少一个入口和所述至少一个出口之间。 温度敏感元件可以被配置为在关闭位置和打开位置之间移动至少一个阀。

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