Turbine exhaust plume mitigation system
    161.
    发明授权
    Turbine exhaust plume mitigation system 有权
    涡轮排气羽流缓解系统

    公开(公告)号:US09003762B2

    公开(公告)日:2015-04-14

    申请号:US13633559

    申请日:2012-10-02

    Abstract: Various embodiments include an exhaust plume mitigation system for a turbine and systems incorporating the exhaust plume mitigation system. In some embodiments, the exhaust plume mitigation system includes: a first conduit fluidly connecting a compressor to an exhaust chamber of the turbine; a first control valve operably connected with the first conduit for regulating flow of compressor air through the first conduit; and a fluid inductor including: a first inlet fluidly connected with the first conduit; a second inlet fluidly connected with ambient; and an outlet fluidly connected with the exhaust chamber.

    Abstract translation: 各种实施例包括用于涡轮机的排气羽流减轻系统和结合排气羽流缓解系统的系统。 在一些实施例中,排气羽流减轻系统包括:将压缩机流体连接到涡轮机的排气室的第一管道; 与第一管道可操作地连接的第一控制阀,用于调节压缩机空气通过第一管道的流动; 以及流体感应器,包括:与所述第一导管流体连接的第一入口; 与环境流体连接的第二入口; 以及与排气室流体连接的出口。

    METHOD AND SYSTEM FOR AUGMENTING THE DETECTION RELIABILITY OF SECONDARY FLAME DETECTORS IN A GAS TURBINE
    163.
    发明申请
    METHOD AND SYSTEM FOR AUGMENTING THE DETECTION RELIABILITY OF SECONDARY FLAME DETECTORS IN A GAS TURBINE 审中-公开
    用于增强二次火焰探测器在气体涡轮机中的可靠性的方法和系统

    公开(公告)号:US20150075170A1

    公开(公告)日:2015-03-19

    申请号:US14029280

    申请日:2013-09-17

    Abstract: Systems and methods for operating a gas turbine combustion system by generating a flame detection signal are provided. A set of modeled parameters expected when there is a flame in a secondary combustion zone is calculated. A set of measured gas turbine parameters is measured. A flame validation signal based on the set of measured parameters and the set of modeled parameters is generated. The systems include a subsystem that calculates a set of modeled parameters expected when there is a flame in the secondary combustion zone and a subsystem that measures a set of measured parameters. A subsystem generates a flame validation signal based on the set of measured parameters and the set of modeled parameters.

    Abstract translation: 提供了通过产生火焰检测信号来操作燃气轮机燃烧系统的系统和方法。 计算在二次燃烧区域中存在火焰时预期的一组建模参数。 测量一组测量的燃气轮机参数。 产生基于测量参数集合和建模参数集的火焰确认信号。 该系统包括一个子系统,该子系统计算在二次燃烧区域中有火焰时所预期的一组建模参数,以及一个测量一组测量参数的子系统。 子系统基于测量参数集合和建模参数集合生成火焰验证信号。

    Gas Turbine Under Frequency Response Improvement System and Method
    164.
    发明申请
    Gas Turbine Under Frequency Response Improvement System and Method 有权
    燃气轮机频率响应改进系统与方法

    公开(公告)号:US20140210217A1

    公开(公告)日:2014-07-31

    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。

    Compressor Bellmouth with a Wash Door
    166.
    发明申请
    Compressor Bellmouth with a Wash Door 有权
    压缩机Bellmouth与洗手间门

    公开(公告)号:US20140126998A1

    公开(公告)日:2014-05-08

    申请号:US13670520

    申请日:2012-11-07

    CPC classification number: F01D25/002 B05B7/0892 B08B3/02

    Abstract: The present application thus provides a compressor wash system for use about a bellmouth of a compressor of a gas turbine engine. The compressor wash system may include a bellmouth wash nozzle positioned about the bellmouth of the compressor and a wash door assembly positioned about a lower half of the bellmouth such that the wash door assembly may be closed when the bellmouth wash nozzle is activated.

    Abstract translation: 因此,本申请提供了一种用于燃气涡轮发动机的压缩机的喇叭口的压缩机清洗系统。 压缩机洗涤系统可以包括围绕压缩机的喇叭口定位的喇叭口洗涤喷嘴和围绕喇叭口的下半部分定位的洗涤门组件,使得当喇叭口清洗喷嘴被激活时,洗涤门组件可以关闭。

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