专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明专利

JP2005171873A Device for computing turbine mechanical output and device for controlling gas turbine provided with the same 有权
标题翻译：用于计算涡轮机械输出的装置和用于控制其提供的气体涡轮的装置
公开(公告)号：JP2005171873A
公开(公告)日：2005-06-30
申请号：JP2003412870
申请日：2003-12-11
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： FUJII FUMITOMO
IPC分类号： F01D17/00 , F01D15/10 , F01D17/02 , F02C7/042 , F02C7/057 , F02C9/28
CPC分类号： F01D15/10 , F02C9/28 , F05D2220/76 , F05D2270/061 , F05D2270/081 , F05D2270/304 , Y02T50/677
摘要： PROBLEM TO BE SOLVED: To provide a device for computing turbine mechanical output, capable of accurately determining gas turbine mechanical output and maintaining air fuel ratio in an appropriate range even under transient state in which generator output changes and gas turbine speed changes, and a device for controlling a gas turbine provided with the same.
SOLUTION: The device for computing gas turbine mechanical output 22 computes gas turbine mechanical output P by a formula (a) based on generator effective electric power Pe measured by a generator effective power meter 12, turbine revolution speed N measured by a gas turbine revolution speed meter 11, inertia moment J of the gas turbine and gravitational acceleration g. A combustion air quantity control device 26 controls combustion air quantity based on the gas turbine mechanical output P.
COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：为了提供一种用于计算涡轮机械输出的装置，即使在发电机输出变化和燃气轮机速度变化的瞬态下，能够精确地确定燃气轮机械输出并将空燃比维持在适当的范围内，以及用于控制设有该燃气轮机的燃气轮机的装置。解决方案：用于计算燃气涡轮机械输出22的装置基于由发电机有效功率计12测量的发电机有效电力Pe，通过公式（a）计算燃气轮机械输出P，由气体测量的涡轮转速N 涡轮转速表11，燃气轮机的惯性矩J和重力加速度g。燃烧空气量控制装置26基于燃气轮机械输出P控制燃烧空气量。（C）2005，JPO＆NCIPI

2. 发明专利

JP2013113201A Valve control device, gas turbine and valve control method 有权
标题翻译：气门控制装置，气体涡轮和阀控制方法
公开(公告)号：JP2013113201A
公开(公告)日：2013-06-10
申请号：JP2011259473
申请日：2011-11-28
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： SAITO AKIHIKO , SONODA TAKASHI , UDA KEIJI , FUJII FUMITOMO
IPC分类号： F02C9/28 , F01D17/20 , F01D17/24 , F02C7/22 , F02C9/50
CPC分类号： F02C7/232 , F02C7/22 , F02C9/263 , F02C9/28 , F02C9/32 , F02C9/50 , F05D2220/76 , F05D2270/02 , F05D2270/05 , F05D2270/061 , F05D2270/091 , F05D2270/301
摘要： PROBLEM TO BE SOLVED: To prevent the output of a gas turbine from being destabilized even when a load is suddenly reduced.SOLUTION: The valve control device 50 is provided on a gas turbine 12 including: a combustor 22 which generates combustion gas by combusting fuel; a turbine 24 which is driven by the combustion gas generated by the combustor 22; a flow adjusting valve 42 which adjusts the flow rate of the fuel to be supplied to the combustor 22; and a pressure adjusting valve 44 which is disposed on the upstream side of the flow adjusting valve 42 in a fuel flow passage 40 for supplying the fuel to the combustor 22 to adjust the fuel pressure, wherein the valve control device controls the opening of the pressure adjusting valve 44. The valve control device 50 includes a load reduction detection unit 52 which detects a reduction in load of the gas turbine 12; and a pressure control unit 56 which controls, when the load reduction is detected by the load reduction detection unit 52, the opening of the pressure adjusting valve 44 according to the output of the gas turbine 12 after the load reduction.
摘要翻译：要解决的问题：为了防止燃气轮机的输出即使在负载突然减小时也不稳定。解决方案：阀控制装置50设置在燃气轮机12上，燃气轮机12包括：燃烧器22，其通过燃烧燃料产生燃烧气体; 由燃烧器22产生的燃烧气体驱动的涡轮机24; 调节供给到燃烧器22的燃料的流量的流量调节阀42; 以及压力调节阀44，其设置在燃料流路40中的流量调节阀42的上游侧，用于将燃料供给到燃烧器22以调节燃料压力，其中，阀控制装置控制压力的打开调节阀44.阀控制装置50包括检测燃气轮机12的负载减少的负载降低检测单元52; 以及压力控制单元56，其在负载降低检测单元52检测到负荷降低时，根据燃料轮机12的输出在负载减小之后进行控制。版权所有（C）2013，JPO＆INPIT

3. 发明专利

JP2005036691A Combustion temperature quick detection device 有权
标题翻译：燃烧温度快速检测装置
公开(公告)号：JP2005036691A
公开(公告)日：2005-02-10
申请号：JP2003198913
申请日：2003-07-18
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： NAKAMURA CHIKASUKE , FUJII FUMITOMO , UCHIDA SHINYA , TOYAMA KOZO , ONO HITOI
IPC分类号： G01K7/00 , F01D21/00 , F02C9/00 , F02C9/28 , G01K7/42 , G01K13/02
CPC分类号： G01K7/42 , F01D21/003 , F02C9/28 , F05D2270/083 , F05D2270/303 , G01K13/02 , G01K2205/04
摘要： PROBLEM TO BE SOLVED: To provide a combustion temperature quick detection device capable of quickly detecting a combustion gas temperature by processing temperature detection signals.
SOLUTION: This combustion temperature quick detection device 10 comprises a phase advancement processing part 11A to detect the combustion gas temperature in a combustor 3 at high speed by offsetting the detection delay of the temperature detection signals. Also the device 10 comprises a primary delay filtering processing part 12 with a time constant of 0.25 sec, a phase delay treatment part 11B with a time constant of 10 sec, a temperature variation filtering processing part 13 with a cutoff frequency of 2 to 3 Hz, and a disturbance filtering processing part 14 having primary delay filtering processing parts 14A and 14B with time constants different from each other and a high valve selection processing part 14C. Thus, the combustion gas temperature suitable for a gas turbine device 1 can be detected quickly.
COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：提供能够通过处理温度检测信号来快速检测燃烧气体温度的燃烧温度快速检测装置。解决方案：该燃烧温度快速检测装置10包括相位提前处理部分11A，通过抵消温度检测信号的检测延迟来高速检测燃烧器3中的燃烧气体温度。另外，装置10包括时间常数为0.25秒的主延迟滤波处理部分12，时间常数为10秒的相位延迟处理部分11B，截止频率为2至3Hz的温度变化滤波处理部分13 以及具有时间常数彼此不同的主延迟滤波处理部14A，14B以及高阀选择处理部14C的扰动滤波处理部14。因此，可以快速地检测适合燃气轮机装置1的燃烧气体温度。版权所有（C）2005，JPO＆NCIPI

4. 发明专利

JP2004132255A Combustor control device 审中-公开
公开(公告)号：JP2004132255A
公开(公告)日：2004-04-30
申请号：JP2002297400
申请日：2002-10-10
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： TANAKA SATOSHI , NAKAMURA CHIKASUKE , FUJII FUMITOMO , UJIIE NAOKI , TOYAMA KOZO
IPC分类号： F01D17/00 , F02C7/00 , F02C7/228 , F02C9/00 , F02C9/28 , F02C9/34 , F02C9/50 , F23R3/28 , F23R3/30 , F23R3/34
CPC分类号： F02C9/00 , F02C7/228 , F02C9/34
摘要： PROBLEM TO BE SOLVED: To provide a combustor control device for correctly operating the turbine inlet temperature without response delay, and controlling a combustor based on the operated turbine inlet temperature.
SOLUTION: The turbine inlet temperature T4 is obtained by a turbine inlet temperature operation unit 15 based on the flow rate Gf and the temperature Tf of fuel to be fed to a combustor 3, and the flow rate G3 and the temperature T3 of air. The pilot ratio is set by a pilot ratio operation unit 16 based on the turbine inlet temperature T4, and a bypass valve control signal and an IGV control signal are generated by a bypass valve opening operation unit 17 and an IGV opening operation unit 18.
COPYRIGHT: (C)2004,JPO

5. 发明专利

JP2012117449A Gas turbine control device and power generation system 有权
标题翻译：气体涡轮控制装置和发电系统
公开(公告)号：JP2012117449A
公开(公告)日：2012-06-21
申请号：JP2010267718
申请日：2010-11-30
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： KISHI MASATO , FUJISHIMA YASUO , SONODA TAKASHI , HIRAFUJI KOICHIRO , TAKADA YASUTSUGU , FUJII FUMITOMO
IPC分类号： F02C9/28 , F01D15/10
CPC分类号： H02P9/04 , F02C9/28 , F05D2270/061 , F05D2270/702 , F05D2270/705 , F05D2270/706
摘要： PROBLEM TO BE SOLVED: To suppress hunting which occurs in the output of a power generator when a load range is lower than a rated load such as during a trial operation or immediately after adding a load.SOLUTION: A gas turbine control device is used in power generation equipment comprising a gas turbine and a power generator which generates electricity from at least rotation power transmitted from the gas turbine, and comprises a first control unit which obtains a first fuel control command in order to make the output of the power generator comply with a power generator output set value decided on the basis of a requested load. The first control unit comprises a feedback control unit 60, and the feedback control unit 60 comprises: a subtraction unit 62 for calculating deviation of the output of the power generator with respect to the power generator output set value; a PI control unit 64 disposed at a post-stage of the subtraction unit 62 in the control; and a peak suppressing unit 66 for suppressing peaks in the amplitude characteristics of the power generator or a system including the power generator.
摘要翻译：要解决的问题：当负载范围低于额定负载（例如在试运行期间或在加载之后）时，抑制在发电机的输出中发生的振荡。解决方案：一种燃气轮机控制装置用于包括燃气轮机和发电机的发电设备，所述燃气轮机和发电机从至少从燃气轮机传递的旋转动力产生电力，并且包括第一控制单元，其获得第一燃料控制命令，以使发电机的输出符合基于所请求的负载决定的发电机输出设定值。第一控制单元包括反馈控制单元60，反馈控制单元60包括：减法单元62，用于计算发电机输出相对于发电机输出设定值的偏差; 设置在控制中的减法单元62的后级的PI控制单元64; 以及用于抑制发电机或包括发电机的系统的振幅特性的峰值的峰值抑制单元66。版权所有（C）2012，JPO＆INPIT

6. 发明专利

JP2004038795A Equivalent operating time calculating device, equivalent operating time calculating system, and equivalent operating time calculating method 审中-公开
公开(公告)号：JP2004038795A
公开(公告)日：2004-02-05
申请号：JP2002197790
申请日：2002-07-05
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： FUJII FUMITOMO
IPC分类号： G05B23/02
摘要： PROBLEM TO BE SOLVED: To provide an equivalent operating time calculating device capable of accurately calculating an equivalent operating time.
SOLUTION: The equivalent operating time calculating device is provided with a controller 4-J and a data logger 6. The controller 4-J collects output values representing output of a generator 2-J connected to a turbine 1-J. The controller 4-J detects a maximum value and a minimum value of the output values within a predetermined time. The controller 4-J calculates an average rate of change of the output values within a relative time zone from detection of either one of the maximum value or minimum value to detection of the other. The controller 4-J calculates a variation representing a difference between the maximum value and minimum value. The data logger 6 calculates a start operating time representing an operating time equivalent to the number of started times of the turbine 1-J on the basis of the variation and the average rate of change. The data logger 6 collects an actual operating time representing the actual operating time of the turbine 1-J. The data logger 6 calculates the equivalent operating time of adding the start operating time to the actual operating time.
COPYRIGHT: (C)2004,JPO

7. 发明专利

JP2005002892A Automatic cooling spin control device, and gas turbine plant equipped with the same 审中-公开
标题翻译：自动冷却旋转控制装置，以及配备其的气体涡轮机
公开(公告)号：JP2005002892A
公开(公告)日：2005-01-06
申请号：JP2003167526
申请日：2003-06-12
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： FUJII FUMITOMO , TOBISHIMA HIROSHI , TANAKA SATOSHI
IPC分类号： F01D17/00 , F01D21/00 , F01K23/10 , F02C9/00 , F02C9/28 , F02C9/50
CPC分类号： Y02E20/16
摘要： PROBLEM TO BE SOLVED: To provide an automatic cooling spin control device for automatically performing a spin operation of a gas turbine after the stop of the gas turbine and opening/closing operation of a stack damper.
SOLUTION: After cutting off fuel supply to a burner 1a, the automatic cooling spin control device 7 controls the stack damper 4a and a motor 6. Therefore, the spin operation rotating the gas turbine 1 for a predetermined time after the stack damper 4a is opened to stop the rotation of the gas turbine 1 and closing the stack damper 4, is automatically repeated at a plurality of times.
COPYRIGHT: (C)2005,JPO&NCIPI
摘要翻译：要解决的问题：提供一种自动冷却旋转控制装置，用于在燃气轮机停止之后自动执行燃气涡轮机的旋转操作以及叠层减震器的打开/关闭操作。解决方案：在切断燃烧器1a的燃料供应之后，自动冷却旋转控制装置7控制堆风阀4a和电动机6.因此，在烟囱阻尼器之后，旋转操作将燃气轮机1旋转预定时间 4a打开以停止燃气轮机1的旋转并且关闭堆栈风门4，多次自动重复。版权所有（C）2005，JPO＆NCIPI

8. 发明专利

JPH1047079A ANTI-SURGE CONTROLLER 失效
公开(公告)号：JPH1047079A
公开(公告)日：1998-02-17
申请号：JP20589496
申请日：1996-08-05
申请人： MITSUBISHI HEAVY IND LTD
发明人： FUJII FUMITOMO
IPC分类号： F02C3/28 , F02C7/057 , F04D27/02 , F22B35/00
摘要： PROBLEM TO BE SOLVED: To improve the limitation of a load changing rate when a boiler load is reduced, by providing an inlet guide vane by which an inlet of supply air to a compressor is closed when the boiler load is reduced and a supply air amount to a boiler is limited, and also providing a blow-off valve which blows a part of the supply air amount to the boiler on the downstream side of the compressor. SOLUTION: A pressure fluidized bed compound power plant is equipped with a gas turbine 2 by which high temperature exhaust heat (combustion) gas is fed from a fluidized bed boiler in a pressure container 1, and a compressor 3 by which air for combustion is fed to the fluidized bed boiler, and an inlet guide vane(IGV) 4 for throttling a supply air amount to the pressure container 1 is arranged in this compressor 3. Also, a blow-off pipe 7 in which a blow-off valve 8 is interposed, is connected between the delivery port of the compressor 3 and an exhaust gas pipe 6, and the blow-off valve 8 is controlled by a controller 11 according to the output of a pressure detector 10 by which the discharge pressure of the compressor 3 is detected. That is, the supply air amount corresponding to a limit amount more than a supply air limit amount in a lowest allowable opening for preventing surging by the closing operation of the IGV 4, is blown and controlled by the blow-off valve 8.

9. 发明专利

JPH0968005A COMPRESSOR CONTROL DEVICE IN PRESSURIZED FLUIDIZED BED COMBINED POWER PLANT 失效
公开(公告)号：JPH0968005A
公开(公告)日：1997-03-11
申请号：JP22166195
申请日：1995-08-30
申请人： MITSUBISHI HEAVY IND LTD
发明人： FUJII FUMITOMO
IPC分类号： F01K23/10 , F01K23/06 , F02C7/057 , F04D27/02
摘要： PROBLEM TO BE SOLVED: To prevent the surging of a compressor wide in an air quantity range for a pressurized fluidized bed combined power plant or the like. SOLUTION: In order to prevent the surging line of an inlet guide vane IGV 24 of a compressor 1 from becoming lower than the outlet pressure of the compressor 1, a pressure transmitter 25 is provided to detect output pressure P. IGV lowest opening to the outlet pressure P is computed by a computing element 26, and an IGV adjusting device 29 is controlled to impart lower limit restriction to IGV opening.

10. 发明专利

JP2002147253A GAS TURBINE PROTECTING DEVICE AND FUEL CONTROL DEVICE 失效
公开(公告)号：JP2002147253A
公开(公告)日：2002-05-22
申请号：JP2000341837
申请日：2000-11-09
申请人： MITSUBISHI HEAVY IND LTD
发明人： TOBISHIMA HIROSHI , FUJII FUMITOMO , SUDO HITOSHI
IPC分类号： F02C9/46 , F02C7/143 , F02C9/00 , F02C9/54
摘要： PROBLEM TO BE SOLVED: To avoid a failure in a gas turbine by preventing a fuel temperature from rising while continuing the operation of the gas turbine when an intake air cooling system is abnormal. SOLUTION: Abnormality in the gas turbine intake air cooling system is detected by an abnormality detecting means 21, and the fuel flow of the gas turbine is instantly lowered to a prescribed value by a means 22 for instantly lowering fuel flow.

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式