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1. 发明授权

US08490379B2 Gas turbine control device 有权
标题翻译：燃气轮机控制装置
公开(公告)号：US08490379B2
公开(公告)日：2013-07-23
申请号：US12933963
申请日：2009-04-10
申请人： Masumi Nomura , Kozo Toyama , Tomo Kawakami , Kotaro Miyauchi , Kuniharu Fujibayashi
发明人： Masumi Nomura , Kozo Toyama , Tomo Kawakami , Kotaro Miyauchi , Kuniharu Fujibayashi
IPC分类号： F02C9/00
CPC分类号： F02C9/18 , F01D17/04 , F01D17/085 , F02C9/22 , F02C9/28 , F02C9/52 , F02C9/54 , F05D2270/053 , F05D2270/082 , F05D2270/14 , F05D2270/303 , F23N1/022 , F23N5/022 , F23N2021/10 , F23N2023/42 , F23N2025/13 , F23N2037/20 , F23N2041/20 , F23R2900/00013
摘要： A gas turbine controller having a first generator for setting the flow rate of fuel or air being supplied to a combustor in correspondence with a target load, a sensor for detecting intake temperature of a compressor, a second generator for setting a correction amount of a set value of fuel flow rate or air flow rate based on the value detected by the sensor, a third generator for setting a modification amount of the correction amount while taking account of the target load, a first multiplier for operating a modified correction amount from a correction amount set by the second generator and a modification amount set by the third generator, and a second multiplier for calculating the flow rate of fuel or air being supplied to a combustor by adding the modified correction amount to the set value of fuel flow rate or air flow rate.
摘要翻译：一种燃气轮机控制器，具有第一发电机，用于将燃料或空气的流量设定为与目标负荷相对应的燃烧器，用于检测压缩机的进气温度的传感器，用于设定压缩机的校正量的第二发电机基于由传感器检测的值的燃料流量或空气流量的值，用于在考虑目标负载的同时设定修正量的修正量的第三发生器，用于从校正操作修正校正量的第一乘法器由第二发生器设定的量和由第三发生器设定的修正量;以及第二乘法器，用于通过将修正校正量与燃料流量或空气的设定值相加来计算供给燃烧器的燃料或空气的流量流量。

2. 发明申请

US20110056180A1 GAS TURBINE CONTROL DEVICE 有权
标题翻译：气体涡轮控制装置
公开(公告)号：US20110056180A1
公开(公告)日：2011-03-10
申请号：US12933963
申请日：2009-04-10
申请人： Masumi Nomura , Kozo Toyama , Tomo Kawakami , Kotaro Miyauchi , Kuniharu Fujibayashi
发明人： Masumi Nomura , Kozo Toyama , Tomo Kawakami , Kotaro Miyauchi , Kuniharu Fujibayashi
IPC分类号： F02C9/00
CPC分类号： F02C9/18 , F01D17/04 , F01D17/085 , F02C9/22 , F02C9/28 , F02C9/52 , F02C9/54 , F05D2270/053 , F05D2270/082 , F05D2270/14 , F05D2270/303 , F23N1/022 , F23N5/022 , F23N2021/10 , F23N2023/42 , F23N2025/13 , F23N2037/20 , F23N2041/20 , F23R2900/00013
摘要： Occurrence of combustion vibration is prevented in a gas turbine plant by enhancing the degree of freedom in setting an airflow rate or a fuel flow rate in correspondence with a target load thereby enhancing combustion stability. A gas turbine controller comprises a first function generator (62) for setting the flow rate of fuel or air being supplied to a combustor (32) in correspondence with a target load, an suction air temperature sensor (22) for detecting intake temperature at the inlet of a compressor, a second function generator (69) for setting a correction amount of a set value of fuel flow rate or air flow rate based on the value detected by the suction air temperature sensor (22), a third function generator (66) for setting a modification amount of the correction amount while taking account of the target load, a first multiplier (68); for operating a modified correction amount from a correction amount set by the second function generator and a modification amount set by the third function generator, and a second multiplier (64) for calculating the flow rate of fuel or air being supplied to a combustor by adding the modified correction amount to the set value of fuel flow rate or air flow rate set by the first function generator.
摘要翻译：通过提高与目标负荷相对应地设定气流速度或燃料流量的自由度，从而提高燃烧稳定性，可以防止燃气轮机厂的燃烧振动的发生。一种燃气轮机控制器包括：第一功能发生器（62），用于根据目标负载设定供给到燃烧器（32）的燃料或空气的流量;吸入空气温度传感器（22），用于检测第二功能发生器（69），用于基于由吸入空气温度传感器（22）检测的值来设定燃料流量或空气流量的设定值的校正量，第三功能发生器（66）），用于在考虑目标负载的同时设定修正量的修正量，第一乘法器（68）; 用于从由第二函数发生器设定的校正量和由第三函数发生器设置的修正量操作修正校正量;以及第二乘法器（64），用于计算通过添加向燃烧器供应的燃料或空气的流量将修正校正量设定为由第一函数发生器设定的燃料流量或空气流量的设定值。

3. 发明授权

US07188019B2 Gas turbine control apparatus, gas turbine system and gas turbine control method 有权
标题翻译：燃气轮机控制装置，燃气轮机系统和燃气轮机控制方法
公开(公告)号：US07188019B2
公开(公告)日：2007-03-06
申请号：US10929927
申请日：2004-08-31
申请人： Masumi Nomura , Hiroyuki Iba , Kozo Toyama , Tomo Kawakami
发明人： Masumi Nomura , Hiroyuki Iba , Kozo Toyama , Tomo Kawakami
IPC分类号： F02C9/00 , G01C19/00
CPC分类号： F02C9/28 , F05D2270/083 , F05D2270/301
摘要： A gas turbine control apparatus, etc. are provided by which combustion fluctuation, even if arising in plural frequency bands, can be effectively suppressed. If the combustion fluctuation arises in plural frequency bands, corresponding to a predetermined priority order, adjustment is done so that the combustion fluctuation of the frequency band of a high priority order is suppressed. If the gas turbine state changes after the adjustment, this is reflected on a data base 30. If no sufficient data is stored yet in the data base 30 for any the reason, such as immediately after installation of the gas turbine, correction is made using data of countermeasures based on data of another same type gas turbine contained in a basic data base 31 and data of countermeasures based on experiences of skilled adjusting operators contained in a knowledge data base 32. Also, in a stabilized operation, operation condition may be varied so that an optimal operation condition is automatically searched.
摘要翻译：提供了一种燃气轮机控制装置等，即使能够有效地抑制多个频带中产生的燃烧波动。如果根据预定的优先级顺序在多个频带中出现燃烧波动，则进行调整，使得抑制了高优先级顺序的频带的燃烧波动。如果燃气轮机状态在调整之后改变，则这反映在数据库30上。如果由于任何原因（例如在安装燃气轮机之后立即安装）而在数据库30中没有足够的数据存储，则使用基于数据库31中的另一相同类型的燃气轮机的数据的对策的数据进行校正以及基于包含在知识数据库32中的熟练调整运算符的经验的对策数据。此外，在稳定化的动作中，可以改变操作条件，从而自动搜索最佳操作条件。

4. 发明申请

US20050107942A1 Gas turbine control apparatus, gas turbine system and gas turbine control method 有权
标题翻译：燃气轮机控制装置，燃气轮机系统和燃气轮机控制方法
公开(公告)号：US20050107942A1
公开(公告)日：2005-05-19
申请号：US10929927
申请日：2004-08-31
申请人： Masumi Nomura , Hiroyuki Iba , Kozo Toyama , Tomo Kawakami
发明人： Masumi Nomura , Hiroyuki Iba , Kozo Toyama , Tomo Kawakami
IPC分类号： F02C9/54 , F02C7/057 , F02C7/228 , F02C9/00 , F02C9/26 , F02C9/28 , F02C9/42 , F02C9/50 , F23N5/18 , F23R3/00 , G06G7/70 , G06F19/00
CPC分类号： F02C9/28 , F05D2270/083 , F05D2270/301
摘要： A gas turbine control apparatus, etc. are provided by which combustion fluctuation, even if arising in plural frequency bands, can be effectively suppressed. If the combustion fluctuation arises in plural frequency bands, corresponding to a predetermined priority order, adjustment is done so that the combustion fluctuation of the frequency band of a high priority order is suppressed. If the gas turbine state changes after the adjustment, this is reflected on a data base 30. If no sufficient data is stored yet in the data base 30 for any the reason, such as immediately after installation of the gas turbine, correction is made using data of countermeasures based on data of another same type gas turbine contained in a basic data base 31 and data of countermeasures based on experiences of skilled adjusting operators contained in a knowledge data base 32. Also, in a stabilized operation, operation condition may be varied so that an optimal operation condition is automatically searched.
摘要翻译：提供了一种燃气轮机控制装置等，即使能够有效地抑制多个频带中产生的燃烧波动。如果根据预定的优先级顺序在多个频带中出现燃烧波动，则进行调整，使得抑制了高优先级顺序的频带的燃烧波动。如果燃气轮机状态在调整之后改变，则这反映在数据库30上。如果由于任何原因（例如在燃气轮机安装之后立即安装）而没有足够的数据存储在数据库30中，则使用基于包含在基本数据库31中的另一相同类型燃气轮机的数据的对策数据以及基于包含在知识数据库32中的熟练调整操作者的经验的对策数据。此外，在稳定操作中，可以改变操作条件从而自动搜索最佳操作条件。

5. 发明授权

US08560205B2 Gas turbine control device and gas turbine system 有权
标题翻译：燃气轮机控制装置和燃气轮机系统
公开(公告)号：US08560205B2
公开(公告)日：2013-10-15
申请号：US12715491
申请日：2010-03-02
申请人： Masumi Nomura , Kozo Toyama , Hiroyuki Iba
发明人： Masumi Nomura , Kozo Toyama , Hiroyuki Iba
IPC分类号： G06F17/00 , G06F19/00 , G01N9/00 , G01N33/22 , G01L23/00
CPC分类号： F02C9/00 , F02C3/22 , F02C9/28 , F05D2270/083 , F23R2900/00013
摘要： An object of the present invention is to provide a gas turbine control device which is capable of performing correction on the basis of a fuel composition of fuel gas to be supplied to a gas turbine, and is capable of changing an amount of correction in response to variation with time of the gas turbine. To attain this, a frequency analyzing unit 25 performs a frequency analysis of combustion oscillation of a combustor and splits a result of the analysis into respective frequency bands. Then, a state grasping unit 22 checks an operating state of the gas turbine on the basis of the result of the analysis of the combustion oscillation and process value of the gas turbine, and corrects the checked operating state on the basis of a fuel composition or a heat capacity of fuel gas measured by a fuel characteristic measuring unit 200. A countermeasure determining unit 23 conducts a countermeasure for controlling an operating action of the gas turbine on the basis of the operating state thus checked.
摘要翻译：本发明的目的是提供一种燃气轮机控制装置，其能够基于要供给到燃气轮机的燃料气体的燃料成分进行校正，并且能够响应于随着燃气轮机的时间变化。为了实现这一点，频率分析单元25对燃烧器的燃烧振动进行频率分析，并将分析结果分解成各个频带。然后，状态把持部22基于燃气轮机的燃烧振动和过程值的分析结果来检查燃气轮机的运转状态，根据燃料组成或者燃料组成来校正所检查的运转状态，由燃料特性测量单元200测量的燃料气体的热容量。对策确定单元23基于所检查的操作状态，进行用于控制燃气轮机的操作动作的对策。

6. 发明申请

US20090125207A1 GAS TURBINE CONTROL DEVICE AND GAS TURBINE SYSTEM 有权
标题翻译：气体涡轮控制装置和气体涡轮机系统
公开(公告)号：US20090125207A1
公开(公告)日：2009-05-14
申请号：US11993915
申请日：2006-03-29
申请人： Masumi Nomura , Kozo Toyama , Hiroyuki Iba
发明人： Masumi Nomura , Kozo Toyama , Hiroyuki Iba
IPC分类号： F02C9/00
CPC分类号： F02C9/00 , F02C3/22 , F02C9/28 , F05D2270/083 , F23R2900/00013
摘要： An object of the present invention is to provide a gas turbine control device which is capable of performing correction on the basis of a fuel composition of fuel gas to be supplied to a gas turbine, and is capable of changing an amount of correction in response to variation with time of the gas turbine. To attain this, a frequency analyzing unit 25 performs a frequency analysis of combustion oscillation of a combustor and splits a result of the analysis into respective frequency bands. Then, a state grasping unit 22 checks an operating state of the gas turbine on the basis of the result of the analysis of the combustion oscillation and process value of the gas turbine, and corrects the checked operating state on the basis of a fuel composition or a heat capacity of fuel gas measured by a fuel characteristic measuring unit 200. A countermeasure determining unit 23 conducts a countermeasure for controlling an operating action of the gas turbine on the basis of the operating state thus checked.
摘要翻译：本发明的目的是提供一种燃气轮机控制装置，其能够基于要供给到燃气轮机的燃料气体的燃料成分进行校正，并且能够响应于随着燃气轮机的时间变化。为了实现这一点，频率分析单元25对燃烧器的燃烧振动进行频率分析，并将分析结果分解成各个频带。然后，状态把持部22基于燃气轮机的燃烧振动和过程值的分析结果来检查燃气轮机的运转状态，根据燃料组成或者燃料组成来校正所检查的运转状态，由燃料特性测量单元200测量的燃料气体的热容量。对策确定单元23基于所检查的操作状态，进行用于控制燃气轮机的操作动作的对策。

7. 发明申请

US20050262849A1 Gas turbine control apparatus and gas turbine system using the same 有权
公开(公告)号：US20050262849A1
公开(公告)日：2005-12-01
申请号：US11191945
申请日：2005-07-29
申请人： Masumi Nomura , Kozo Toyama
发明人： Masumi Nomura , Kozo Toyama
IPC分类号： F01D17/16 , F02C7/057 , F02C7/228 , F02C9/00 , F02C9/18 , F02C9/22 , F02C9/26 , F02C9/28 , F02C9/50 , F02C9/52 , F23N5/16 , F23R3/26 , F23R3/34
CPC分类号： F02C7/228 , F01D17/162 , F02C9/18 , F02C9/22 , F02C9/263 , F02C9/28 , F02C9/50 , F02C9/52 , F05D2260/96 , F05D2270/083 , F05D2270/14 , F23N5/16 , F23N2041/20 , F23R3/26 , F23R2900/00013 , F23R2900/00014
摘要： In a gas turbine control apparatus, a frequency analyzing section frequency-analyzes at least one of pressure oscillation in combustors of a gas turbine and acceleration oscillation of each of the combustors and outputs a first frequency analysis result as the result of frequency analysis for a plurality of predetermined frequency bands. A control unit controls at least one of a first fuel flow rate of fuel and a first air flow rate of air based on the first frequency analysis result for the plurality of frequency bands. The fuel and the air are supplied to the gas turbine.

8. 发明申请

US20110004390A1 GAS TURBINE CONTROL METHOD AND DEVICE 有权
标题翻译：气体涡轮机控制方法和装置
公开(公告)号：US20110004390A1
公开(公告)日：2011-01-06
申请号：US12920409
申请日：2009-04-10
申请人： Masumi Nomura , Kozo Toyama
发明人： Masumi Nomura , Kozo Toyama
IPC分类号： F02C9/00 , F02C9/28 , F02C7/057
CPC分类号： F02C9/28 , F02C9/34 , F02C9/50 , F05D2270/44
摘要： Provided is a gas turbine control method and control device whereby a design performance and an operating state based on ideal fuel flow rate and air flow rate simulated at the time of designing can be maintained by preventing an operation deviated from an operating condition that is based on ideal fuel flow rate and air flow rate simulated by initial design values, in a gas turbine control method designed to search optimal operating conditions automatically using control inputs such as a pilot ratio. The gas turbine controller comprises a second database that stores load sensitivity, i.e. the correlation between the load amount of a gas turbine and control inputs such as a fuel flow rate, air flow rate, pilot fuel ratio, and top hat fuel ratio in the gas turbine, wherein the amount of load variation for at least one of control inputs, a fuel flow rate or an air flow rate supplied to a combustor is predicted according to operational conditions obtained by searching using the load sensitivity, regulation is made according to the prediction results, and the regulation results are stored in the second database.
摘要翻译：本发明提供一种燃气轮机控制方法和控制装置，通过防止从基于以下的运行状态偏离的动作，能够维持基于理想的燃料流量和设计时的空气流量的运转状态在燃气轮机控制方法中，通过初始设计值模拟的理想燃料流量和空气流量，设计为使用诸如导频比等控制输入自动搜索最佳工作条件。燃气轮机控制器包括存储负载灵敏度的第二数据库，即燃气轮机的负载量与气体中的燃料流量，空气流量，先导燃料比和顶帽燃料比等控制输入之间的相关性涡轮机，其中根据通过使用负载灵敏度的搜索而获得的操作条件来预测提供给燃烧器的至少一个控制输入，燃料流量或空气流量的负载变化量，根据预测进行调节结果，调节结果存储在第二个数据库中。

9. 发明授权

US07234305B2 Gas turbine control apparatus and gas turbine system using the same 有权
标题翻译：燃气轮机控制装置和使用其的燃气轮机系统
公开(公告)号：US07234305B2
公开(公告)日：2007-06-26
申请号：US11191945
申请日：2005-07-29
申请人： Masumi Nomura , Kozo Toyama
发明人： Masumi Nomura , Kozo Toyama
IPC分类号： F02C9/00
CPC分类号： F02C7/228 , F01D17/162 , F02C9/18 , F02C9/22 , F02C9/263 , F02C9/28 , F02C9/50 , F02C9/52 , F05D2260/96 , F05D2270/083 , F05D2270/14 , F23N5/16 , F23N2041/20 , F23R3/26 , F23R2900/00013 , F23R2900/00014
摘要： In a gas turbine control apparatus, a frequency analyzing section frequency-analyzes at least one of pressure oscillation in combustors of a gas turbine and acceleration oscillation of each of the combustors and outputs a first frequency analysis result as the result of frequency analysis for a plurality of predetermined frequency bands. A control unit controls at least one of a first fuel flow rate of fuel and a first air flow rate of air based on the first frequency analysis result for the plurality of frequency bands. The fuel and the air are supplied to the gas turbine.
摘要翻译：在燃气轮机控制装置中，频率分析部对燃气轮机的燃烧室的压力振动和各燃烧器的加速振动进行频率分析，并且，作为多个燃烧器的频率分析结果，输出第一频率分析结果的预定频带。控制单元基于多个频带的第一频率分析结果来控制燃料的第一燃料流量和空气的第一空气流量中的至少一个。燃料和空气被供应到燃气轮机。

10. 发明授权

US06955039B2 Gas turbine control apparatus and gas turbine system using the same 有权
标题翻译：燃气轮机控制装置和使用其的燃气轮机系统
公开(公告)号：US06955039B2
公开(公告)日：2005-10-18
申请号：US10225356
申请日：2002-08-22
申请人： Masumi Nomura , Kozo Toyama
发明人： Masumi Nomura , Kozo Toyama
IPC分类号： F01D17/16 , F02C7/057 , F02C7/228 , F02C9/00 , F02C9/18 , F02C9/22 , F02C9/26 , F02C9/28 , F02C9/50 , F02C9/52 , F23N5/16 , F23R3/26 , F23R3/34
CPC分类号： F02C7/228 , F01D17/162 , F02C9/18 , F02C9/22 , F02C9/263 , F02C9/28 , F02C9/50 , F02C9/52 , F05D2260/96 , F05D2270/083 , F05D2270/14 , F23N5/16 , F23N2041/20 , F23R3/26 , F23R2900/00013 , F23R2900/00014
摘要： In a gas turbine control apparatus, a frequency analyzing section frequency-analyzes at least one of pressure oscillation in combustors of a gas turbine and acceleration oscillation of each of the combustors and outputs a first frequency analysis result as the result of frequency analysis for a plurality of predetermined frequency bands. A control unit controls at least one of a first fuel flow rate of fuel and a first air flow rate of air based on the first frequency analysis result for the plurality of frequency bands. The fuel and the air are supplied to the gas turbine.
摘要翻译：在燃气轮机控制装置中，频率分析部对燃气轮机的燃烧室的压力振动和各燃烧器的加速振动进行频率分析，并且，作为多个燃烧器的频率分析结果，输出第一频率分析结果的预定频带。控制单元基于多个频带的第一频率分析结果来控制燃料的第一燃料流量和空气的第一空气流量中的至少一个。燃料和空气被供应到燃气轮机。

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