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1. 发明申请

US20100322286A1 QUICK-RESPONSE THERMOCOUPLE FOR HIGH-SPEED FLUID 审中-公开
标题翻译：用于高速流体的快速热电偶
公开(公告)号：US20100322286A1
公开(公告)日：2010-12-23
申请号：US12666105
申请日：2008-10-24
申请人： Kozo Toyama , Mitsuaki Mochizuki , Hiroshi Okada , Shinichi Fukushima , Junichi Sano
发明人： Kozo Toyama , Mitsuaki Mochizuki , Hiroshi Okada , Shinichi Fukushima , Junichi Sano
IPC分类号： G01K7/02
CPC分类号： G01K13/02 , G01K1/08 , G01K1/18 , G01K7/02
摘要： An object of the invention is to provide a thermocouple having a high response speed without receiving mechanical damages such as bending and curving even when it is used in a high-speed fluid. The invention provides a quick-response thermocouple for high-speed fluid in which a sheathed thermocouple having a small outer diameter that is formed by housing, in a metal sheath, a positive-side thermocouple filament and a negative-side thermocouple filament embedded within a powder of an inorganic insulating material, and by forming a temperature sensing point at a tip portion thereof by bonding the tips of the positive-side thermocouple filament and the negative-side thermocouple filament together at the tip portion thereof, is inserted in a protective tube having a large outer diameter so that the tip portion is exposed, in which a portion of the sheathed thermocouple that is exposed from the protective tube is inserted in a protective cylinder having a bottom cover with a hole on a tip side through which the sheathed thermocouple is inserted and having a plurality of through windows, the tip of the sheathed thermocouple is slightly exposed from the bottom cover of the protective cylinder, and the bottom cover of the protective cylinder and the sheathed thermocouple as well as the protective cylinder and a lower portion of the protective tube are welded.
摘要翻译：本发明的目的是提供一种具有高响应速度的热电偶，即使在高速流体中使用时也不会受到弯曲和弯曲等机械损伤。本发明提供了一种用于高速流体的快速响应热电偶，其中具有小外径的铠装热电偶通过在金属外壳中容纳正嵌入的热电偶丝和负侧热电偶丝而形成无机绝缘材料的粉末，并且通过在顶端部分处将正侧热电偶丝和负侧热电偶丝的末端接合在一起的顶端处形成温度感测点，插入保护管中具有大的外径，使得尖端部分露出，其中从保护管暴露的一部分铠装热电偶被插入到具有底盖的保护筒中，该保护筒具有在顶端侧的孔，护套热电偶插入并具有多个通孔，该护套热电偶的尖端稍微暴露于保护层的底盖 e气缸，保护筒的底盖和护套热电偶以及保护筒和保护管的下部焊接。

2. 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。

3. 发明授权

US08141335B2 Intake air heating control device for gas turbine 有权
标题翻译：燃气轮机进气加热控制装置
公开(公告)号：US08141335B2
公开(公告)日：2012-03-27
申请号：US12447382
申请日：2007-11-09
申请人： Satoshi Tanaka , Shoichi Harada , Kozo Toyama
发明人： Satoshi Tanaka , Shoichi Harada , Kozo Toyama
IPC分类号： F02C7/047 , F02C7/08
CPC分类号： F02C9/22 , F02C7/047 , F02C7/057 , F05D2270/705
摘要： Extremely cold (e.g., −20° C.) air A is heated by a heat exchanger 30, which is supplied with steam S via a control valve 32, and heated air A′ is taken into a gas turbine 10. The valve opening degree of the control valve 32 is feedback-controlled so that the deviation between the measured temperature t1 and the target temperature TO of the heated air A′ is eliminated. Further, when the number of revolutions, N, of the gas turbine 10 increases, or when an IGV opening degree OP increases, the valve opening degree of the control valve 32 is feedforward-controlled in accordance with the increase in the number N of revolutions or the increase in the IGV opening degree OP. By so doing, the temperature of air A′ can be maintained at a temperature enabling stable combustion without delay in control, and intake air can be heated without delay in control, even at the start of the gas turbine or during change in the opening degree of an inlet guide vane.
摘要翻译：非常冷（例如-20℃），空气A被热交换器30加热，热交换器30经由控制阀32供给蒸汽S，加热空气A'被吸入燃气轮机10.阀开度控制阀32被反馈控制，从而消除了加热空气A'的测量温度t1与目标温度TO之间的偏差。此外，当燃气轮机10的转数N增加时，或当IGV开度OP增加时，控制阀32的阀开度根据转数N的增加进行前馈控制或IGV开度OP的增加。通过这样做，空气A'的温度可以保持在能够在不延迟控制的情况下稳定燃烧的温度，并且即使在燃气轮机的启动时或者在开度变化的情况下，也可以不延迟地加热进气的入口导叶。

4. 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。

5. 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。

6. 发明申请

US20060005526A1 Combustor controller 有权
标题翻译：燃烧器控制器
公开(公告)号：US20060005526A1
公开(公告)日：2006-01-12
申请号：US10528408
申请日：2003-10-09
申请人： Satoshi Tanaka , Fuminori Fuji , Naoki Ujiie , Kozo Toyama
发明人： Satoshi Tanaka , Fuminori Fuji , Naoki Ujiie , Kozo Toyama
IPC分类号： F02C9/50
CPC分类号： F02C9/00 , F02C7/228 , F02C9/34
摘要： A turbine inlet temperature operating section (15) determines the turbine inlet temperature T4 based on the flow rate Gf and temperature Tf of fuel being supplied to a combustor (3) and the flow rate G3 and temperature T3 of air. Based on the turbine inlet temperature T4, a pilot ratio operating section (16) sets a pilot ratio, and a bypass valve operating section (17) and an IGV opening operating section (18) generate a bypass valve control signal and an IGV control signal, respectively.
摘要翻译：涡轮入口温度运行部分（15）基于供给到燃烧器（3）的燃料的流量Gf和温度Tf以及空气的流量G 3和温度T 3来确定涡轮机入口温度T 4。基于涡轮机入口温度T 4，先导比操作部（16）设定先导比，旁通阀操作部（17）和IGV打开操作部（18）产生旁通阀控制信号和IGV控制信号。

7. 发明授权

US4211045A Building structure 失效
标题翻译：建筑结构
公开(公告)号：US4211045A
公开(公告)日：1980-07-08
申请号：US858198
申请日：1977-12-07
申请人： Hajime Koizumi , Kozo Toyama , Mikio Kobayashi , Hajime Hatano , Toshio Saeki , Kaoru Mizukoshi , Shinichi Tamanaga , Keizo Miyakawa , Tomoyasu Kato
发明人： Hajime Koizumi , Kozo Toyama , Mikio Kobayashi , Hajime Hatano , Toshio Saeki , Kaoru Mizukoshi , Shinichi Tamanaga , Keizo Miyakawa , Tomoyasu Kato
IPC分类号： E04B1/21 , E04B5/43 , E04C3/293 , E04B5/19
CPC分类号： E04C3/065 , E04B1/21 , E04B5/43 , E04C3/293
摘要： A building structure including a beam of steel or rod reinforced concrete which is sheathed in a U-shaped cross section steel shell, a concrete column which is encased in a steel tube, diagonal bracings and connecting members thereof. The topside of the U-shaped steel shell is open to allow concrete to be filled therethrough. Steel rods are placed in the shell and a steel panel connecting member secures the opposed sidewalls of the shell. Steel bars extend from a floor slab into the beam shell through the aforesaid open topside, thereby rendering the beam integral with the slab. Frame-like steel members for confining reinforcing bars and/or shear connectors are disposed in the inside of the beam shell. A steel sleeve is also provided in the beam shell for defining a space for disposition of equipment. In addition, an opening is provided in the bottom wall of the beam shell so as to allow steel rods to extend from the wall into the beam shell, thereby rendering the beam integral with the wall. A column is coupled to the beam by means of ring stiffeners or gusset plates. Diagonal bracings are positioned in symmetric relation to the frame member of the beam or column, and the diagonal bracings are fastened to the frame member of the beam or column by means of long bolts extending through the frame member thereof. The tip portions of diagonal bracings are provided with anchor members which are embedded in the concrete contained in the beam shell.
摘要翻译：一种建筑结构，其包括被包覆在U形横截面钢壳中的钢梁或钢筋混凝土梁，包围在钢管中的混凝土柱，对角支撑及其连接构件。 U形钢壳的顶部是开放的，以允许混凝土被填充通过。钢棒放置在壳体中，钢板连接构件固定壳体的相对侧壁。钢筋通过上述敞开的顶部从地板延伸到梁壳中，从而使梁与板块成一体。用于限制钢筋和/或剪切连接器的框架状钢构件设置在梁壳的内部。梁壳中还设有一个钢套筒，用于定义设备的处理空间。此外，在梁壳的底壁中设置有开口，以允许钢杆从壁延伸到梁壳中，从而使梁与壁成一体。柱通过环加强筋或角撑板联接到梁上。对角支撑与梁或柱的框架构件对称地定位，并且对角支撑通过延伸穿过其框架构件的长螺栓紧固到梁或柱的框架构件。对角支撑的尖端部分设置有锚固构件，其嵌入在包含在梁壳中的混凝土中。

8. 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。

9. 发明授权

US07757474B2 Gas turbine protection device 有权
标题翻译：燃气轮机保护装置
公开(公告)号：US07757474B2
公开(公告)日：2010-07-20
申请号：US10581194
申请日：2004-11-26
申请人： Satoshi Tanaka , Toshimitsu Morimoto , Shouichi Nagata , Kozo Toyama
发明人： Satoshi Tanaka , Toshimitsu Morimoto , Shouichi Nagata , Kozo Toyama
IPC分类号： F02G3/00
CPC分类号： F01D21/12 , F01D21/00 , F02C9/00 , F02C9/28 , F05D2270/303
摘要： 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.
摘要翻译：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。

10. 发明授权

US07756626B2 Gas turbine output learning circuit and combustion control device for gas turbine having the same 有权
标题翻译：用于燃气轮机的燃气轮机输出学习电路和燃烧控制装置
公开(公告)号：US07756626B2
公开(公告)日：2010-07-13
申请号：US11657132
申请日：2007-01-24
申请人： Kentaro Fujii , Kozo Toyama
发明人： Kentaro Fujii , Kozo Toyama
IPC分类号： F02C9/28
CPC分类号： F02C9/28 , F05D2270/705 , F23N5/00 , F23N2023/48 , F23N2041/20 , G05B13/024
摘要： A gas turbine output learning circuit is configured to compute a current combustion gas temperature TIT at an inlet of a gas turbine by linear interpolation by use of two characteristic curves A and B respectively representing relations between a pressure ratio and an exhaust gas temperature in the cases of the combustion gas temperature at the inlet of the gas turbine at 1400° C. and 1500° C., then to compute ideal MW corresponding to this combustion gas temperature TIT at the inlet of the gas turbine by linear interpolation according to 1400° C.MW and 1500° C.MW (temperature controlled MW), and then to correct the 1400° C.MW and the 1500° C.MW so as to match the ideal MW with a measured gas turbine output (a power generator output).
摘要翻译：燃气轮机输出学习电路被配置为通过使用分别表示压力比和废气温度之间的关系的两个特性曲线A和B通过线性插值来计算燃气涡轮机入口处的当前燃烧气体温度TIT 在燃气轮机入口处的燃烧气体温度在1400℃和1500℃下，然后根据1400℃通过线性插值来计算对应于燃气轮机入口处的燃烧气体温度TIT的理想MW .MW和1500°CMW（温度控制MW），然后校正1400°CMW和1500°CMW，以使理想MW与测得的燃气轮机输出（发电机输出）匹配，。

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