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公开(公告)号：US06351937B1
公开(公告)日：2002-03-05
申请号：US09451869
申请日：1999-12-01
IPC分类号： F02C300
CPC分类号： F01D5/082 , F01D5/087 , F04D29/321
摘要： A gas turbine plant comprises an air compressor, a gas turbine combustor and a gas turbine, which are operatively connected in series. In the gas turbine plant, an air compressor shaft is accommodated in the air compressor and composed of discs piled up along an axial direction of the air compressor shaft, a gas turbine shaft is accommodated in the gas turbine and composed of discs piled up along an axial direction of the gas turbine shaft, and an intermediate shaft is interposed between the air compressor shaft and the gas turbine shaft. At least one of the discs of the air compressor shaft and the discs of the gas turbine shaft are provided with bulged portions each having approximately a hanging bell shape or trapezoidal shape.
摘要翻译： 燃气轮机设备包括可操作地串联连接的空气压缩机，燃气轮机燃烧器和燃气轮机。 在燃气轮机设备中，空气压缩机轴容纳在空气压缩机中，由沿着空气压缩机轴的轴向堆积的圆盘构成，燃气轮机轴容纳在燃气轮机中， 燃气轮机轴的轴向，中空轴设置在空气压缩机轴与燃气轮机轴之间。 空气压缩机轴和燃气轮机轴的盘中的至少一个设置有各自具有大致悬挂形状或梯形形状的凸出部。
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公开(公告)号：US20050268973A1
公开(公告)日：2005-12-08
申请号：US10533396
申请日：2003-10-29
申请人： Fumio Ootomo , Tsutomu Ooishi , Yoshiki Niizeki , Yoshitaka Fukuyama , Hisashi Matsuda , Osamu Shindo
发明人： Fumio Ootomo , Tsutomu Ooishi , Yoshiki Niizeki , Yoshitaka Fukuyama , Hisashi Matsuda , Osamu Shindo
CPC分类号： F16K47/08 , F01D17/145 , Y10T137/7976 , Y10T137/8085 , Y10T137/86734 , Y10T137/87917 , Y10T137/87925
摘要： A steam valve in accordance with the present invention is the steam valve that houses a first valve device 21 composed of a valve seat, a valve body, a valve rod, and a driving device, and a second valve device 22 composed of the valve seat, the valve body, the valve rod, and the driving device, combined with each other in the valve casing 23, and a closing portion 41 to block a part of a main steam flow flowing from outside to inside of a strainer is formed in the strainer 27 that is housed in the valve casing 23 and that surrounds the valve body 29 of the first valve device. According to the above described configuration, the steam valve that is aimed to further decrease a pressure loss can be provided by effectively controlling the steam flow in the strainer housed in the valve casing.
摘要翻译： 根据本发明的蒸汽阀是容纳由阀座，阀体，阀杆和驱动装置构成的第一阀装置21的蒸汽阀，以及由阀座构成的第二阀装置22 ，阀体，阀杆和驱动装置，在阀壳体23中彼此结合，并且封闭部分41阻挡从过滤器的外部流入内部的主蒸汽流的一部分，形成在 过滤器27，其容纳在阀壳体23中并且围绕第一阀装置的阀体29。 根据上述结构，可以通过有效地控制容纳在阀壳体中的过滤器中的蒸汽流量来提供旨在进一步降低压力损失的蒸汽阀。
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公开(公告)号：US5624231A
公开(公告)日：1997-04-29
申请号：US364686
申请日：1994-12-28
申请人： Fumio Ohtomo , Yoshitaka Fukuyama , Yuji Nakata , Asako Inomata , Hisashi Matsuda , Shoko Ito
发明人： Fumio Ohtomo , Yoshitaka Fukuyama , Yuji Nakata , Asako Inomata , Hisashi Matsuda , Shoko Ito
CPC分类号： F01D5/187 , F01D5/186 , F05D2260/201 , F05D2260/202
摘要： A turbine blade performs internal cooling by a cooling gas flowing through internal cooling flow passages and FCFC cooling by a cooling gas jetted out through film holes arranged on the substantially whole area of the blade surface. The film holes are arranged in rows extending in the span direction at predetermined pitches in the chord direction. The dimensions of the elements of the turbine blade are determined by a mathematical formula 5.ltoreq.L/N.multidot.D.ltoreq.50, where L is the length of any interval of the surface of the cooled turbine blade, N is the number of rows of the film holes in the interval and D is an average diameter of the film holes in the interval. With this arrangement, the maximum cooling efficiency at a small amount of cooling gas flow is attained, and both the quantity of heat per unit area of the blade surface transmitted from the main flow gas to the blade surface and the thermal stresses are reduced.
摘要翻译： 涡轮叶片通过流过内部冷却流路的冷却气体进行内部冷却，并且通过冷却气体进行FCFC冷却，所述冷却气体通过布置在叶片表面的大致整个区域上的薄膜孔喷出。 薄膜孔以沿翼弦方向以预定的间距在翼展方向上延伸的排布置。 涡轮叶片的元件的尺寸由数学公式5确定，其中L是冷却的涡轮叶片的表面的任何间隔的长度，N是行数 的间隔中的膜孔，D是间隔中的膜孔的平均直径。 由此，能够实现少量冷却气体流动时的最大冷却效率，从主流动气体向叶片表面传递的叶片面积的单位面积的热量和热应力减小。
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公开(公告)号：US07604021B2
公开(公告)日：2009-10-20
申请号：US10533396
申请日：2003-10-29
申请人： Fumio Ootomo , Tsutomu Ooishi , Yoshiki Niizeki , Yoshitaka Fukuyama , Hisashi Matsuda , Osamu Shindo
发明人： Fumio Ootomo , Tsutomu Ooishi , Yoshiki Niizeki , Yoshitaka Fukuyama , Hisashi Matsuda , Osamu Shindo
CPC分类号： F16K47/08 , F01D17/145 , Y10T137/7976 , Y10T137/8085 , Y10T137/86734 , Y10T137/87917 , Y10T137/87925
摘要： A steam valve in accordance with the present invention is the steam valve that houses a first valve device 21 composed of a valve seat, a valve body, a valve rod, and a driving device, and a second valve device 22 composed of the valve seat, the valve body, the valve rod, and the driving device, combined with each other in the valve casing 23, and a closing portion 41 to block a part of a main steam flow flowing from outside to inside of a strainer is formed in the strainer 27 that is housed in the valve casing 23 and that surrounds the valve body 29 of the first valve device. According to the above described configuration, the steam valve that is aimed to further decrease a pressure loss can be provided by effectively controlling the steam flow in the strainer housed in the valve casing.
摘要翻译： 根据本发明的蒸汽阀是容纳由阀座，阀体，阀杆和驱动装置构成的第一阀装置21的蒸汽阀，以及由阀座构成的第二阀装置22 ，阀体，阀杆和驱动装置，在阀壳体23中彼此结合，并且封闭部分41阻挡从过滤器的外部流入内部的主蒸汽流的一部分，形成在 过滤器27，其容纳在阀壳体23中并且围绕第一阀装置的阀体29。 根据上述结构，可以通过有效地控制容纳在阀壳体中的过滤器中的蒸汽流量来提供旨在进一步降低压力损失的蒸汽阀。
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公开(公告)号：US5538394A
公开(公告)日：1996-07-23
申请号：US365430
申请日：1994-12-28
申请人： Asako Inomata , Hisashi Matsuda , Yoshitaka Fukuyama , Fumio Ohtomo , Yuji Nakata , Hideo Nomoto
发明人： Asako Inomata , Hisashi Matsuda , Yoshitaka Fukuyama , Fumio Ohtomo , Yuji Nakata , Hideo Nomoto
CPC分类号： F01D5/187 , F28F3/02 , F05D2240/127 , F05D2260/2212 , Y02T50/673 , Y02T50/676
摘要： A cooling flow passage assembly consisting of pressure side cooling flow passages extending in a span direction and suction side cooling flow passages extending in the span direction and serially connected to the pressure side cooling flow passages is formed in a turbine blade. A cooling medium flows through the pressure side cooling flow passages in the direction toward the tip portion and through the suction side cooling flow passages in the direction toward the root. Cooling effect is improved by a Coriolis force. The number of the suction side cooling flow passages is larger than the number of the pressure side cooling flow passages. At least one of the suction side cooling flow passages forms at least one most downstream cooling flow passage. The cooling medium flows through the most downstream cooling flow passage and is exhausted outside of the turbine blade through nozzles, whereby the flow of the cooling medium through the most downstream cooling flow passage is speeded up.
摘要翻译： 在涡轮叶片中形成有由在跨度方向上延伸的压力侧冷却流路和沿跨度方向延伸并串联连接到压力侧冷却流路的吸入侧冷却流路构成的冷却流路组件。 冷却介质沿着朝向前端部的方向流过压力侧冷却流路，并且沿着朝向根部的方向通过吸入侧冷却流路。 科里奥利力提高了冷却效果。 吸入侧冷却流路的数量大于压力侧冷却流路的数量。 吸入侧冷却流路中的至少一个形成至少一个最下游的冷却流路。 冷却介质流过最下游的冷却流道，并通过喷嘴排出涡轮叶片的外部，由此冷却介质通过最下游的冷却流道的流动被加速。
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公开(公告)号：US09133717B2
公开(公告)日：2015-09-15
申请号：US12812227
申请日：2009-01-08
IPC分类号： F01D5/18
CPC分类号： F01D5/189 , F01D5/186 , F05D2240/121 , F05D2240/122 , F05D2240/303 , F05D2240/304 , F05D2260/201 , F05D2260/205 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141
摘要： A cooling structure of a turbine airfoil cools a turbine airfoil (10) exposed to hot gas (1), using cooling air (2) of a temperature lower than that of the hot gas. The turbine airfoil (10) includes an external surface (11), an internal surface (12) opposite to the external surface, a plurality of film-cooling holes (13) blowing the cooling air from the internal surface toward the external surface to film-cool the external surface, and a plurality of heat-transfer promoting projections (14) integrally formed with the internal surface and protruding inwardly from the internal surface. The turbine airfoil further includes a hollow cylindrical insert (20) which is positioned inside the internal surface of the turbine airfoil and to which the cooling air is supplied. The insert has a plurality of impingement holes (21) for impingement-cooling the internal surface (12).
摘要翻译： 涡轮翼型件的冷却结构使用比热气体的温度低的冷却空气（2）冷却暴露于热气体（1）的涡轮机翼型件（10）。 涡轮机翼（10）包括外表面（11），与外表面相对的内表面（12），多个薄膜冷却孔（13），其将冷却空气从内表面向外表面吹向薄膜 - 冷却外表面，以及多个传热促进突起（14），其与内表面整体形成并从内表面向内突出。 涡轮机翼片还包括中空圆柱形插入件（20），该中空圆柱形插入件位于涡轮机翼片的内表面内部，并且供应冷却空气。 插入件具有用于冲击冷却内表面（12）的多个冲击孔（21）。
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公开(公告)号：US6038850A
公开(公告)日：2000-03-21
申请号：US114253
申请日：1998-07-13
申请人： Fumio Ohtomo , Yuji Nakata , Yoshitaka Fukuyama , Asako Inomata , Sachio Shibuya , Akinori Koga , Junji Ishii , Shoko Ito , Hironobu Yamamoto
发明人： Fumio Ohtomo , Yuji Nakata , Yoshitaka Fukuyama , Asako Inomata , Sachio Shibuya , Akinori Koga , Junji Ishii , Shoko Ito , Hironobu Yamamoto
摘要： A combined cycle power plant comprises a gas turbine system and a steam cycle system having a steam turbine to be driven by the steam generated by the waste heat of the exhaust gas of the gas turbine system, wherein the steam from the steam cycle system flows through a gas turbine cooling system of the gas turbine to cool the gas turbine blades and other elements of the gas turbine system to be cooled and the waste heat of the gas turbine system is effectively collected. The gas turbine cooling system has two or more than two cooling ducts formed in two or more than two elements of the gas turbine system to be cooled such as the gas turbine blades and the combustor of the gas turbine system so that steam is made to flow through the cooling ducts of these two or more than two elements to be cooled to effectively and maximally exploit the cooling potential and the waste heat collecting potential of the steam and hence improve the overall thermal efficiency of the plant.
摘要翻译： 联合循环发电厂包括燃气轮机系统和蒸汽循环系统，该蒸汽循环系统具有蒸气涡轮机，由汽轮机系统的废气的废热产生的蒸汽驱动，其中来自蒸汽循环系统的蒸汽流过 燃气轮机的燃气轮机冷却系统，用于冷却燃气轮机叶片和待冷却的燃气轮机系统的其它元件，并有效地收集燃气轮机系统的废热。 燃气轮机冷却系统具有形成在待冷却的燃气轮机系统的两个或多于两个元件中的两个或两个以上的冷却管道，例如燃气轮机叶片和燃气轮机系统的燃烧器，使得蒸汽流动 通过这两个或多于两个要冷却的元件的冷却管道，以有效地和最大限度地利用蒸汽的冷却潜力和废热收集电位，从而提高设备的整体热效率。
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公开(公告)号：US6000213A
公开(公告)日：1999-12-14
申请号：US114095
申请日：1998-07-13
申请人： Fumio Ohtomo , Yuji Nakata , Yoshitaka Fukuyama , Asako Inomata , Sachio Shibuya , Akinori Koga , Junji Ishii , Shoko Ito , Hironobu Yamamoto
发明人： Fumio Ohtomo , Yuji Nakata , Yoshitaka Fukuyama , Asako Inomata , Sachio Shibuya , Akinori Koga , Junji Ishii , Shoko Ito , Hironobu Yamamoto
摘要： A combined cycle power plant comprises a gas turbine system and a steam cycle system having a steam turbine to be driven by the steam generated by the waste heat of the exhaust gas of the gas turbine system, wherein the steam from the steam cycle system flows through a gas turbine cooling system of the gas turbine to cool the gas turbine blades and other elements of the gas turbine system to be cooled and the waste heat of the gas turbine system is effectively collected. The gas turbine cooling system has two or more than two coolooling ducts formed in two or more than two elements of the gas turbine system to be cooled such as the gas turbine blades and the combustor of the gas turbine system so that steam is made to flow through the cooling ducts of these two or more than two elements to be cooled to effectively and maximally exploit the cooling potential and the waste heat collecting potential of the steam and hence improve the overall thermal efficiency of the plant.
摘要翻译： 联合循环发电厂包括燃气轮机系统和蒸汽循环系统，该蒸汽循环系统具有蒸气涡轮机，由汽轮机系统的废气的废热产生的蒸汽驱动，其中来自蒸汽循环系统的蒸汽流过 燃气轮机的燃气轮机冷却系统，用于冷却燃气轮机叶片和待冷却的燃气轮机系统的其它元件，并有效地收集燃气轮机系统的废热。 燃气轮机冷却系统具有形成在要冷却的燃气轮机系统的两个或多于两个元件中的两个或两个以上的共沸管道，例如燃气轮机叶片和燃气轮机系统的燃烧器，使得蒸汽流动 通过这两个或多于两个要冷却的元件的冷却管道，以有效地和最大限度地利用蒸汽的冷却潜力和废热收集电位，从而提高设备的整体热效率。
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公开(公告)号：US5778657A
公开(公告)日：1998-07-14
申请号：US716868
申请日：1996-09-20
申请人： Fumio Ohtomo , Yuji Nakata , Yoshitaka Fukuyama , Asako Inomata , Sachio Shibuya , Akinori Koga , Junji Ishii , Shoko Ito , Hironobu Yamamoto
发明人： Fumio Ohtomo , Yuji Nakata , Yoshitaka Fukuyama , Asako Inomata , Sachio Shibuya , Akinori Koga , Junji Ishii , Shoko Ito , Hironobu Yamamoto
摘要： A combined cycle power plant comprises a gas turbine system and a steam cycle system having a steam turbine to be driven by the steam generated by the waste heat of the exhaust gas of the gas turbine system, wherein the steam from the steam cycle system flows through a gas turbine cooling system of the gas turbine to cool the gas turbine blades and other elements of the gas turbine system to be cooled and the waste heat of the gas turbine system is effectively collected. The gas turbine cooling system has two or more than two cooling ducts formed in two or more than two elements of the gas turbine system to be cooled such as the gas turbine blades and the combustor of the gas turbine system so that steam is made to flow through the cooling ducts of these two or more than two elements to be cooled to effectively and maximally exploit the cooling potential and the waste heat collecting potential of the steam and hence improve the overall thermal efficiency of the plant.
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10.发明授权Cooling apparatus for gas turbine moving blade and gas turbine equipped with same 失效用于燃气轮机动叶片的冷却装置和配备该冷却装置的燃气轮机
公开(公告)号：US6094905A
公开(公告)日：2000-08-01
申请号：US937516
申请日：1997-09-25
申请人： Yoshitaka Fukuyama
发明人： Yoshitaka Fukuyama
IPC分类号： F01D5/02 , F01D5/06 , F01D5/08 , F01D5/18 , F01D9/02 , F01D11/04 , F02C7/18 , F02C6/18 , F02D29/58
CPC分类号： F01D5/066 , F01D5/06 , F01D5/082 , F01D5/085 , F05D2260/205 , F05D2260/2322
摘要： A gas turbine is equipped with a moving blade cooling apparatus arranged in association with a turbine rotor in which a plurality of discs are mounted, a plurality of moving blades are mounted each to an outer peripheral portion of each of the discs and a plurality of spacers are also disposed in spaces between the respective discs at portions corresponding to a location of stationary blades and in which the moving blades are formed each with a cooling medium flowing passage and the discs and the spacers are arranged with spaces therebetween for passing a cooling medium in a radial direction of the rotor. A closed-loop cooling unit is thus formed for supplying the cooling medium to the cooling medium flowing passage formed in the moving blade and recovering the same therefrom. A passage assembly, which is provided with a cooling medium supplying passage and a cooling medium recovering passage running in parallel with each other in an axial direction of the turbine rotor, is provided at a central axis portion of the turbine rotor, the cooling medium supplying passage of the passage assembly is formed with a cooling medium supplying port in communication with a side of a cooling medium inlet of the cooling medium flowing passage formed in the moving blade, and the cooling medium recovering passage of the passage assembly is formed with a cooling medium recovering port in communication with a cooling medium outlet of the cooling medium flowing passage in the moving blade.
摘要翻译： 燃气轮机配备有与其中安装有多个盘的涡轮转子相关联地设置的动叶片冷却装置，多个活动叶片分别安装在每个盘的外周部分上，并且多个间隔件 也设置在各个盘之间的与固定叶片的位置相对应的部分处的空间中，并且其中形成有各自具有冷却介质流动通道的活动叶片，并且盘和间隔件之间设置有用于使冷却介质通过的空间 转子的径向。 因此，形成闭环冷却单元，用于将冷却介质供应到形成在动叶片中的冷却介质流动通道并从中回收。 在涡轮机转子的中心轴部设置有设置有冷却介质供给路径和在涡轮转子的轴向上彼此平行的冷却介质回收通道的通道组件，供给冷却介质 通道组件的通道形成有与形成在动叶片中的冷却介质流动通道的冷却介质入口侧相连通的冷却介质供给口，通道组件的冷却介质回收通道形成为冷却 介质回收口与动叶片中的冷却介质流动通道的冷却介质出口连通。
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