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公开(公告)号：US06212873B1
公开(公告)日：2001-04-10
申请号：US09256106
申请日：1999-02-24
IPC分类号： F02C600
CPC分类号： F01K23/106 , Y02E20/14 , Y02E20/16
摘要： The invention provides a gas turbine combined cycle structured such that an intermediate cooling device for cooling a compression air discharged from a low pressure compressor, so as to reduce a load of a high pressure compressor, is provided. The gas turbine combined cycle in accordance with the invention is structured such as to branch water from a condenser to a steam generating device for generating steam. Exhaust gas discharged from a steam turbine is condensed to water. Compression air discharged from a low pressure compressor is cooled by being supplied to an intermediate cooling device, and is then supplied to a high pressure compressor. Steam which heats and operates the steam turbine is generated by the heat recovered by the cooling of the compression air in the intermediate cooling device. Accordingly, there can be obtained a gas turbine combined cycle having the advantage of the conventional intermediate cooling type gas turbine combined cycle, but exhibiting an improved combined efficiency.
摘要翻译： 本发明提供了一种燃气轮机联合循环，其结构使得用于冷却从低压压缩机排出的压缩空气以减少高压压缩机的负荷的中间冷却装置。 根据本发明的燃气轮机联合循环被构造为将水从冷凝器分配到用于产生蒸汽的蒸汽发生装置。 从汽轮机排出的排气被冷凝成水。 从低压压缩机排出的压缩空气通过供给到中间冷却装置而冷却，然后供给高压压缩机。 通过中间冷却装置中的压缩空气冷却回收的热量产生加热和操作蒸汽轮机的蒸汽。 因此，可以获得具有传统的中间冷却型燃气轮机联合循环的优点的燃气轮机联合循环，但是显示出提高的组合效率。
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公开(公告)号：US06244039B1
公开(公告)日：2001-06-12
申请号：US09300841
申请日：1999-04-28
申请人： Hideaki Sugishita , Yoshiaki Tsukuda , Kazuo Uematsu , Eiji Akita
发明人： Hideaki Sugishita , Yoshiaki Tsukuda , Kazuo Uematsu , Eiji Akita
IPC分类号： F02C600
CPC分类号： F01K23/106 , Y02E20/16
摘要： A combined cycle plant includes a heat exchanger (3) for recovering heat into compressed air or gas turbine fuel to be supplied into gas turbine (01). The plant is arranged such that steam is used as high temperature side working medium of the heat exchanger (3). Thus, the heating medium supply passage can be made of ordinary steam piping and piping cost is reduced. Also, gas turbine exhaust gas is led directly into a waste heat recovery boiler (02), so that gas turbine efficiency and combined efficiency can be enhanced and plant manufacturing cost is reduced.
摘要翻译： 联合循环设备包括用于将热量回收到被供应到燃气轮机（01）中的压缩空气或燃气涡轮燃料中的热交换器（3）。 该设备布置成使得蒸汽用作热交换器（3）的高温侧工作介质。 因此，加热介质供给通路可以由普通蒸汽管道制成，并且管道成本降低。 此外，燃气轮机废气直接引入废热回收锅炉（02），从而可以提高燃气轮机效率和组合效率，降低设备制造成本。
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公开(公告)号：US20070137203A1
公开(公告)日：2007-06-21
申请号：US10590014
申请日：2004-12-22
IPC分类号： G21D5/00
CPC分类号： G21D5/00 , F02C1/05 , F02C1/10 , F02C3/10 , F02C9/18 , F05D2220/76 , F05D2260/85 , G21C1/07 , G21D1/02 , Y02E30/36
摘要： A gas turbine plant, wherein a plurality of first gas turbines positioned coaxially with compressors and a second gas turbine positioned coaxially with a generator are rotated by a coolant heated by heat energy provided by the fission of a coated particle fuel. A flow in a bypass passage is controlled by controlling the opening of bypass valves of (n−1) in quantity which bypass the first gas turbines on up to (n−1) shafts in starting. Accordingly, the rotational speeds of the first gas turbines on up to (n) shafts are increased to a rated rotational speed in order starting at the initial stage on the upstream side of a high temperature gas-cooled reactor toward the lower stage for each shaft.
摘要翻译： 一种燃气轮机设备，其中与压缩机同轴定位的多个第一燃气轮机和与发电机同轴设置的第二燃气轮机由被涂覆颗粒燃料的裂变所提供的热能加热的冷却剂旋转。 旁通通道中的流动通过控制（n-1）的旁通阀的开启量来控制，该旁路阀在启动时绕过多达（n-1）个轴上的第一燃气轮机的数量。 因此，将高达（n）个轴上的第一燃气轮机的旋转速度提高到额定转速，从而在高温气冷式反应器的上游侧的初始阶段开始朝向每个轴的下段 。
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公开(公告)号：US20100086096A1
公开(公告)日：2010-04-08
申请号：US12632105
申请日：2009-12-07
IPC分类号： G21C19/28
CPC分类号： F02C1/05 , F02C1/10 , F02C9/18 , F05D2220/76 , G21D5/06
摘要： A gas turbine plant, wherein a first gas turbine positioned coaxially with a compressor and a second gas turbine positioned coaxially with a generator are rotated by a coolant heated by heat energy provided by the fission of a coated particle fuel. The rotational speed of the first gas turbine is controlled by controlling a flow in the bypass passage of the second gas turbine.
摘要翻译： 一种燃气轮机设备，其中与压缩机同轴地定位的第一燃气轮机和与发电机同轴设置的第二燃气轮机由被涂覆颗粒燃料的裂变提供的热能加热的冷却剂旋转。 通过控制第二燃气轮机的旁路通道中的流量来控制第一燃气轮机的转速。
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公开(公告)号：US07596947B2
公开(公告)日：2009-10-06
申请号：US10590014
申请日：2004-12-22
IPC分类号： G21D5/00
CPC分类号： G21D5/00 , F02C1/05 , F02C1/10 , F02C3/10 , F02C9/18 , F05D2220/76 , F05D2260/85 , G21C1/07 , G21D1/02 , Y02E30/36
摘要： A gas turbine plant, wherein a plurality of first gas turbines positioned coaxially with compressors and a second gas turbine positioned coaxially with a generator are rotated by a coolant heated by heat energy provided by the fission of a coated particle fuel. A flow in a bypass passage is controlled by controlling the opening of bypass valves of (n−1) in quantity which bypass the first gas turbines on up to (n−1) shafts in starting. Accordingly, the rotational speeds of the first gas turbines on up to (n) shafts are increased to a rated rotational speed in order starting at the initial stage on the upstream side of a high temperature gas-cooled reactor toward the lower stage for each shaft.
摘要翻译： 一种燃气轮机设备，其中与压缩机同轴定位的多个第一燃气轮机和与发电机同轴设置的第二燃气轮机由被涂覆颗粒燃料的裂变所提供的热能加热的冷却剂旋转。 旁通通道中的流动通过控制（n-1）的旁通阀的开启量来控制，该旁路阀在启动时绕过多达（n-1）个轴上的第一燃气轮机的数量。 因此，将高达（n）个轴上的第一燃气轮机的旋转速度提高到额定转速，从而在高温气冷式反应器的上游侧的初始阶段开始朝向每个轴的下段 。
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公开(公告)号：US20070183554A1
公开(公告)日：2007-08-09
申请号：US10590012
申请日：2004-12-22
IPC分类号： G21C7/32
CPC分类号： F02C1/05 , F02C1/10 , F02C9/18 , F05D2220/76 , G21D5/06
摘要： A gas turbine plant, wherein a first gas turbine positioned coaxially with a compressor and a second gas turbine positioned coaxially with a generator are rotated by a coolant heated by heat energy provided by the fission of a coated particle fuel. The rotational speed of the first gas turbine is controlled by controlling a flow in the bypass passage of the second gas turbine.
摘要翻译： 一种燃气轮机设备，其中与压缩机同轴地定位的第一燃气轮机和与发电机同轴设置的第二燃气轮机由被涂覆颗粒燃料的裂变所提供的热能加热的冷却剂旋转。 通过控制第二燃气轮机的旁路通道中的流量来控制第一燃气轮机的转速。
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公开(公告)号：US06634175B1
公开(公告)日：2003-10-21
申请号：US09762598
申请日：2001-02-09
申请人： Yutaka Kawata , Shigemi Mandai , Yoshiaki Tsukuda , Eiji Akita , Hisato Arimura
发明人： Yutaka Kawata , Shigemi Mandai , Yoshiaki Tsukuda , Eiji Akita , Hisato Arimura
IPC分类号： F23R310
CPC分类号： F23R3/04
摘要： A gas turbine combustor has homogenous air inflow by elimination of turbulence from the air, reducing combustion instability. A combustor 3 has, at its center, a pilot nozzle 8 and eight main nozzles 7 around the pilot nozzle 8. The air flows in around the individual nozzles 7 and 8 to the leading end of the combustor 3 so that it is used for combustion. An annular flow ring 20, having a semicirculat section, is disposed at the upstream end portion of a combustion cylinder 10, and a porous plate 50 and a surrounding rib 51 are disposed downstream of the flow ring 20. The air inflow is smoothly turned at first by the flow ring 20 and then straightened by the porous plate 50 so that the air flows without any disturbance around the individual nozzles 7 and 8 to the leading end, thereby reducing combustion instability.
摘要翻译： 燃气轮机燃烧器通过消除来自空气的紊流而具有均匀的空气流入，从而降低燃烧不稳定性。 燃烧器3在其中心处具有引导喷嘴8和围绕引燃喷嘴8的八个主喷嘴7.空气在单独的喷嘴7和8周围流到燃烧器3的前端，使其用于燃烧 。 具有半圆形部分的环形流动环20设置在燃烧气缸10的上游端部，并且多孔板50和周围肋51设置在流动环20的下游。空气流入平滑地转向 首先通过流动环20，然后由多孔板50拉直，使得空气在各个喷嘴7和8周围没有任何干扰地流到前端，从而减少燃烧不稳定性。
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8.发明授权
公开(公告)号：US4936089A
公开(公告)日：1990-06-26
申请号：US283270
申请日：1988-12-09
摘要： Disclosed herein is a gas turbine system which is supplied with a low-pressure industrial by-product gas as a fuel and equipped coaxially with a gas compressor for compressing the fuel gas, the system providing a bypass pipeline for returning the gas in a high-pressure gas piping on the discharge side of the fuel gas compressor into a low-pressure gas piping on the inlet side of the compressor through a pressure reducing valve and a cooler, and an emergency gas pressure stabilizer having high responsive characteristics, the stabilizer being provided in the bypass pipeline on the outlet side of the cooler, whereby the high-pressure fuel gas on the discharge side of the fuel gas compressor can be returned safely into a low-pressure industrial by-product gas pipeline.
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公开(公告)号：US5951250A
公开(公告)日：1999-09-14
申请号：US35616
申请日：1998-03-05
申请人： Kiyoshi Suenaga , Sunao Aoki , Yoshiaki Tsukuda , Youichi Iwasaki
发明人： Kiyoshi Suenaga , Sunao Aoki , Yoshiaki Tsukuda , Youichi Iwasaki
摘要： A turbine cooling apparatus comprising a turbine disk having a plurality of moving blades, a torque tube coupled coaxially to one surface side of the turbine disk and having a thick stepped inner wall portion in the central portion thereof, an air separator fitted on the torque tube with the inner surface thereof in contact with the outer surface of the torque tube so that a passage through which cooling air is supplied to the moving blades via the turbine disk is defined between the air separator and the torque tube, and a torque tube cooling hollow portion provided along and in the vicinity of the outer surface of the thick stepped wall portion of the torque tube.
摘要翻译： 一种涡轮机冷却装置，包括具有多个活动叶片的涡轮盘，与所述涡轮盘的一个表面侧同轴配置的扭矩管，并且在其中心部分具有厚的阶梯状内壁部分，安装在所述扭矩管上的空气分离器 其内表面与扭矩管的外表面接触，从而在空气分离器和扭矩管之间限定了通过涡轮盘将冷却空气供应到活动叶片的通道，以及扭矩管冷却空心管 在转矩管的厚阶梯状壁部的外表面附近设置的部分。
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公开(公告)号：US08028511B2
公开(公告)日：2011-10-04
申请号：US12007244
申请日：2008-01-08
申请人： Yoshinori Hyakutake , Yoshiaki Tsukuda , Takao Hashimoto , Satoshi Uchida , Katsuhiro Ota , Takashi Sonoda
发明人： Yoshinori Hyakutake , Yoshiaki Tsukuda , Takao Hashimoto , Satoshi Uchida , Katsuhiro Ota , Takashi Sonoda
CPC分类号： F02C3/28 , C10J3/00 , C10J3/466 , C10J3/723 , C10J3/84 , C10J2300/093 , C10J2300/0956 , C10J2300/0959 , C10J2300/165 , C10J2300/1671 , C10J2300/1675 , C10J2300/1678 , C10J2300/1884 , F01K23/068 , Y02E20/16 , Y02E20/18
摘要： A gasifying agent supply path A from an axial flow compressor 21 which boosts pressure of a gasifying agent to a gasifying furnace 2 is branched, and a gasifying agent bypass path D having an escaping pressure adjusting valve 23 is provided. The flow quantity or pressure of the gasifying agent supplied to the gasifying furnace 2 from the gasifying agent supply path A can be adjusted according to the degree of opening of the adjusting valve 23 disposed in the gasifying agent bypass path D, whereby providing a control valve in the gasifying agent supply path A is no longer necessary. Thus, pressure loss at the gasifying agent supply path A can be suppressed, and the discharge pressure of the axial flow compressor 21 can be greatly reduced.
摘要翻译： 来自将轴向压缩机21的气化剂供给路径A分支，气化炉2将气化剂的压力提高到气化炉2，并且设置有具有逸出压力调节阀23的气化剂旁路路径D. 从气化剂供给路径A向气化炉2供给的气化剂的流量或压力可以根据设置在气化剂旁通路径D中的调节阀23的开度而进行调整，由此设置控制阀 在气化剂供给路径A中不再需要。 因此，能够抑制气化剂供给路径A的压力损失，能够大幅降低轴流式压缩机21的排出压力。
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