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    • 1. 发明申请
    • Gas Turbine Protection Device
    • 燃气轮机保护装置
    • US20080276595A1
    • 2008-11-13
    • US10581194
    • 2004-11-26
    • Satoshi TanakaToshimitsu MorimotoShouichi NagataKozo Toyama
    • Satoshi TanakaToshimitsu MorimotoShouichi NagataKozo Toyama
    • F02C9/00F01D21/12
    • F01D21/12F01D21/00F02C9/00F02C9/28F05D2270/303
    • A gas turbine protection apparatus, which can output a gas turbine protection signal only when a combustor is abnormal, without increasing the number of temperature sensors such as thermocouples. For this purpose, a BPT deviation change amount large automatic stop signal is outputted when a BPT deviation change amount of any of the thermocouples exceeds a BPT deviation change amount large set value, and a BPT deviation change amount large signal is outputted from a determining section (15), and when the BPT deviation change amount of any of the thermocouples adjacent bilaterally to the any thermocouple exceeds a BPT deviation change amount present set value, and a BPT deviation change amount present signal is outputted from a determining section (16a, 16b). Alternatively, a BPT deviation great automatic stop or tripping signal is outputted when a BPT deviation of any of the thermocouples exceeds a BPT deviation great set value, and a BPT deviation great signal is outputted from a determining section, and when the BPT deviation of any of the thermocouples adjacent bilaterally to the any thermocouple exceeds a BPT deviation present set value, and a BPT deviation present signal is outputted from a determining section.
    • 一种燃气轮机保护装置,其仅在燃烧器异常时才能输出燃气轮机保护信号,而不增加诸如热电偶的温度传感器的数量。 为此,当任何热电偶的BPT偏差变化量超过BPT偏差变化量大的设定值时,输出BPT偏差变化量大的自动停止信号,从判定部输出BPT偏差变化量大信号 (15),并且当与任何热电偶的双侧相邻的任何热电偶的BPT偏差变化量超过BPT偏差变化量当前设定值,并且从判定部(16a)输出BPT偏差变化量当前信号时, 16 b)。 或者,当任何热电偶的BPT偏差超过BPT偏差大设定值,并且从判定部输出BPT偏差大信号时,输出BPT偏差大的自动停止或跳闸信号,并且当任何 与双向热电偶相邻的热电偶超过BPT偏差当前设定值,并且从确定部输出BPT偏离当前信号。
    • 3. 发明授权
    • Gas turbine controller of single-shaft combined cycle power generating plant and gas turbine output calculating method
    • 单轴联合循环发电厂燃气轮机控制器和燃气轮机输出计算方法
    • US06477842B1
    • 2002-11-12
    • US09890188
    • 2001-07-30
    • Shouichi NagataHiroya Komiyama
    • Shouichi NagataHiroya Komiyama
    • F02C618
    • F01K9/00F01K9/003F01K23/101F02C6/18F02C9/00F05D2200/12F05D2200/13F05D2220/72F05D2220/74F05D2270/05F05D2270/301Y02E20/16
    • A gas turbine control apparatus for a single-shaft type combined cycle power plant is provided by which gas turbine output is accurately computed during a circulating water reversing wash operation. Vacuum down amount is computed from a generator output signal (31) immediately before the mentioned reversing wash operation and is corrected by being multiplied by a valve opening correction factor computed from a condenser reversing valve opening signal (41) and a sea water temperature correction factor computed from a condenser reversing valve inlet sea water temperature signal (47). A condenser vacuum at the time of the reversing wash operation is computed by the corrected vacuum down amount being subtracted therefrom. A vacuum correction factor is computed based on the computed condenser vacuum. A reference steam turbine output is computed based on a post-intercept valve steam pressure signal (34) and a steam turbine output signal (54) is computed by multiplying the reference steam turbine output by the vacuum correction factor. A gas turbine output signal (55) is computed by subtracting the steam turbine output signal (54) from the generator output signal (31).
    • 提供了一种用于单轴式联合循环发电厂的燃气轮机控制装置,在循环水反向洗涤操作期间,通过该燃气轮机控制装置精确地计算出燃气轮机的输出。 真空下降量是在所述反向洗涤操作之前的发电机输出信号(31)计算的,并且通过乘以由冷凝器换向阀开启信号(41)计算出的开阀校正系数和海水温度校正系数 从冷凝器换向阀入口海水温度信号(47)计算。 通过从其中减去校正后的真空减量来计算反转洗涤操作时的冷凝器真空度。 基于计算的冷凝器真空计算真空校正因子。 基于截流后阀门蒸汽压力信号(34)计算参考蒸汽涡轮机输出,并且通过将参考蒸汽涡轮机输出乘以真空校正因子来计算蒸汽涡轮机输出信号(54)。 通过从发电机输出信号(31)中减去汽轮机输出信号(54)来计算燃气轮机输出信号(55)。
    • 10. 发明授权
    • Gas turbine protection device
    • 燃气轮机保护装置
    • US07757474B2
    • 2010-07-20
    • US10581194
    • 2004-11-26
    • Satoshi TanakaToshimitsu MorimotoShouichi NagataKozo Toyama
    • Satoshi TanakaToshimitsu MorimotoShouichi NagataKozo Toyama
    • F02G3/00
    • F01D21/12F01D21/00F02C9/00F02C9/28F05D2270/303
    • A gas turbine has a plurality of combustors in a toroidal arrangement to provide combustion gases to turbine blades, thereby rotating the turbine body. Thermocouples, the number of which is the same as or greater than the number of the combustors, are arranged toroidally at the outlets of the turbine blades and measure the temperatures of the combustion gases at the respective outlets. During the operation of the gas turbine, if an abnormality, such as misfire or fuel injection nozzle obstruction, occurs in one or more of the combustors, the resulting change in gas temperature triggers a signal to stop, and thereby protect the gas turbine. Based on the measured values of the blade pass temperatures of the thermocouples and set threshold temperatures, a fuel supply system may be caused to gradually decrease the fuel supplied to the combustors to bring the gas turbine body to an automatic stop, or it may be cut off instantaneously, thus immediately stopping the gas turbine.
    • 燃气轮机具有环形布置的多个燃烧器,以向涡轮机叶片提供燃烧气体,从而使涡轮机体旋转。 其数量等于或大于燃烧器的数量的热电偶在涡轮机叶片的出口处环形地布置,并且测量各个出口处的燃烧气体的温度。 在燃气轮机的运转中,如果在一个或多个燃烧器中发生诸如失火或燃料喷射喷嘴堵塞的异常,则由此导致气体温度的变化触发信号停止,从而保护燃气轮机。 基于热电偶的叶片通过温度的测量值和设定的阈值温度,可以引起燃料供应系统逐渐减少供应到燃烧器的燃料以使燃气轮机主体自动停止,或者可以切断 从而立即停止燃气轮机。