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1. 发明授权

US06351937B1 Gas turbine plant 有权
标题翻译：燃气轮机厂
公开(公告)号：US06351937B1
公开(公告)日：2002-03-05
申请号：US09451869
申请日：1999-12-01
申请人： Hisashi Matsuda , Kazuhiro Kitayama , Fumio Otomo , Yoshitaka Fukuyama
发明人： Hisashi Matsuda , Kazuhiro Kitayama , Fumio Otomo , Yoshitaka Fukuyama
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。

2. 发明申请

US20060126902A1 Surface roughness measuring method and apparatus and turbine deterioration diagnostic method 审中-公开
标题翻译：表面粗糙度测量方法及装置及涡轮机劣化诊断方法
公开(公告)号：US20060126902A1
公开(公告)日：2006-06-15
申请号：US11285017
申请日：2005-11-23
申请人： Hisashi Matsuda , Hiroshi Kawakami , Asako Inomata , Fumio Otomo , Hiroyuki Kawagishi
发明人： Hisashi Matsuda , Hiroshi Kawakami , Asako Inomata , Fumio Otomo , Hiroyuki Kawagishi
IPC分类号： G06K9/00
CPC分类号： G01B11/303
摘要： A surface roughness measuring method including, measuring surface roughness and a surface color image information of a plurality of representative points of a surface of a first object to be measured, and preparing a calibration information indicating the relationship between color stimulus values for the surface color image information and the surface roughness. The surface roughness measuring method further includes taking a surface color image information of a plurality of measuring points of a surface of a second object to be measured, obtaining color stimulus values from the surface color image information of the measuring points, converting the color stimulus values of the measuring points to surface roughness of the measuring points using the calibration information, and displaying the surface roughness of the measuring points of the second object to be measured as a surface information.
摘要翻译：一种表面粗糙度测量方法，包括：测量待测量的第一物体的表面的多个代表点的表面粗糙度和表面彩色图像信息，以及准备表示表面彩色图像的颜色激励值之间的关系的校准信息信息和表面粗糙度。表面粗糙度测量方法还包括获取待测量的第二物体的表面的多个测量点的表面彩色图像信息，从测量点的表面彩色图像信息获得颜色激励值，将颜色刺激值使用校准信息测量点的测量点的表面粗糙度，并将第二被测量物体的测量点的表面粗糙度显示为表面信息。

3. 发明申请

US20070081898A1 Turbine cascade structure 有权
标题翻译：涡轮级联结构
公开(公告)号：US20070081898A1
公开(公告)日：2007-04-12
申请号：US10577651
申请日：2004-10-29
申请人： Hisashi Matsuda , Asako Inomata , Fumio Otomo , Hiroyuki Kawagishi , Daisuke Nomura
发明人： Hisashi Matsuda , Asako Inomata , Fumio Otomo , Hiroyuki Kawagishi , Daisuke Nomura
IPC分类号： F01D11/00
CPC分类号： F01D5/145 , F01D5/143 , F01D9/041 , Y10S415/914 , Y10S416/02
摘要： A turbine blade cascade structure includes a plurality of blades arranged in series in a circumferential direction on a wall surface, in which a corner portion defined by the wall surface and a front edge portion of each of blade bodies supported by the wall surface, to which a working fluid flows is provided with a coating portion that extends toward an upstream side of a flow of the working fluid. The turbine blade cascade structure is capable of reducing the secondary flow loss of the secondary flow in spite of the fluctuation of an incident angle of the working fluid flowing to the front edge portion of the blade body.
摘要翻译：涡轮叶片级联结构包括在壁面上沿圆周方向串联布置的多个叶片，其中由壁表面限定的角部和由壁表面支撑的每个叶片体的前边缘部分，工作流体流动设置有朝着工作流体的流动的上游侧延伸的涂覆部分。涡轮叶栅级联结构能够减小二次流的二次流量损失，尽管工作流体流入叶片体的前边缘部分的入射角度的波动。

4. 发明授权

US5953449A Measuring apparatus and measuring method 失效
标题翻译：测量装置和测量方法
公开(公告)号：US5953449A
公开(公告)日：1999-09-14
申请号：US818669
申请日：1997-03-14
申请人： Hisashi Matsuda , Takeshi Watanabe , Fumio Otomo
发明人： Hisashi Matsuda , Takeshi Watanabe , Fumio Otomo
IPC分类号： G01K11/16 , G06K9/00
CPC分类号： G01K11/165
摘要： The disclosed measuring apparatus can measure a predetermined physical quantity (e.g., temperature) of a coloring member (e.g., liquid crystal) whose color condition changes according to change of the physical quantity. The measuring apparatus comprises: a coloring member (2) whose color condition changes according to change of a predetermined physical quantity; a color detecting section (5) for detecting the color condition of the coloring member; a data base section (8) for constructing a three-dimensional color space (10) having three coordinate axes each corresponding to each of tristimulus values of color of the coloring member, relationship between the predetermined physical quantity and the tristimulus values being represented in the three-dimensional color space; and a physical quantity calculating section (9) for calculating the physical quantity of an object (1) to be measure on the basis of the tristimulus values of color of the coloring member detected by the color detecting section (5) and with reference to the data base section (8).
摘要翻译：所公开的测量装置可以测量其颜色状况根据物理量的变化而变化的着色部件（例如液晶）的预定物理量（例如，温度）。测量装置包括：着色部件（2），其颜色状态根据预定物理量的变化而变化; 颜色检测部分（5），用于检测着色部件的颜色状况; 用于构建具有三个坐标轴的三维颜色空间（10）的数据库部分（8），每个三个坐标轴对应于着色部件的颜色的三刺激值之间的关系，预定物理量和三刺激值之间的关系表示在三维色彩空间; 以及物理量计算部（9），用于基于由所述颜色检测部（5）检测到的着色部件的颜色的三刺激值，并参照所述颜色检测部（5）计算要测量的物体（1）的物理量数据库部分（8）。

5. 发明授权

US07625181B2 Turbine cascade structure 有权
标题翻译：涡轮级联结构
公开(公告)号：US07625181B2
公开(公告)日：2009-12-01
申请号：US10577651
申请日：2004-10-29
申请人： Hisashi Matsuda , Asako Inomata , Fumio Otomo , Hiroyuki Kawagishi , Daisuke Nomura
发明人： Hisashi Matsuda , Asako Inomata , Fumio Otomo , Hiroyuki Kawagishi , Daisuke Nomura
IPC分类号： F01D5/14 , F01D9/04
CPC分类号： F01D5/145 , F01D5/143 , F01D9/041 , Y10S415/914 , Y10S416/02
摘要： A turbine blade cascade structure includes a plurality of blades arranged in series in a circumferential direction on a wall surface, in which a corner portion defined by the wall surface and a front edge portion of each of blade bodies supported by the wall surface, to which a working fluid flows, includes a cover portion (fillet) that extends toward an upstream side of a flow of the working fluid. The turbine blade cascade structure is capable of reducing the secondary flow loss of the secondary flow in spite of the fluctuation of an incident angle of the working fluid flowing to the front edge portion of the blade body.
摘要翻译：涡轮叶片级联结构包括在壁面上沿圆周方向串联布置的多个叶片，其中由壁表面限定的角部和由壁表面支撑的每个叶片体的前边缘部分，工作流体流动，包括朝向工作流体的流动的上游侧延伸的盖部分（圆角）。涡轮叶栅级联结构能够减小二次流的二次流量损失，尽管工作流体流入叶片体的前边缘部分的入射角度的波动。

6. 发明申请

US20050268973A1 Steam valve 有权
标题翻译：蒸汽阀
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
IPC分类号： F01D17/14 , F16K47/08 , F01D17/10
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。

7. 发明授权

US5624231A Cooled turbine blade for a gas turbine 失效
标题翻译：用于燃气轮机的冷却涡轮叶片
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
IPC分类号： F01D5/18 , F02C7/18
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。

8. 发明授权

US07604021B2 Steam valve 有权
标题翻译：蒸汽阀
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
IPC分类号： F01D17/10 , F16K31/06
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。

9. 发明授权

US5538394A Cooled turbine blade for a gas turbine 失效
标题翻译：用于燃气轮机的冷却涡轮叶片
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
IPC分类号： F01D5/18 , F02C7/18 , F28F3/02
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。

10. 发明授权

US09297260B2 Airflow control device and airflow control method 有权
标题翻译：气流控制装置和气流控制方法
公开(公告)号：US09297260B2
公开(公告)日：2016-03-29
申请号：US13419211
申请日：2012-03-13
申请人： Motofumi Tanaka , Hisashi Matsuda , Hiroyuki Yasui , Shohei Goshima , Naohiko Shimura , Kunihiko Wada , Tamon Ozaki , Toshiki Osako , Masahiro Asayama , Yutaka Uchida
发明人： Motofumi Tanaka , Hisashi Matsuda , Hiroyuki Yasui , Shohei Goshima , Naohiko Shimura , Kunihiko Wada , Tamon Ozaki , Toshiki Osako , Masahiro Asayama , Yutaka Uchida
IPC分类号： F17D1/16 , F17D1/18 , F15C1/04 , F15C1/06 , B64C21/00 , B64C23/00 , B64C23/06 , F01D5/14
CPC分类号： F01D5/145 , B64C23/005 , B64C2230/12 , B64C2230/14 , F05D2240/127 , F05D2270/17 , F05D2270/172 , Y10T137/0391 , Y10T137/2185 , Y10T137/2191 , Y10T137/2224
摘要： An airflow control device 10 in an embodiment includes: a vortex shedding structure portion 20 discharging an airflow flowing on a surface in a flow direction as a vortex flow; and a first electrode 40 and a second electrode 41 disposed on a downstream side of the vortex shedding structure portion 20 via a dielectric. By applying a voltage between the first electrode 40 and the second electrode 41, flow of the airflow on the downstream side of the vortex shedding structure portion 20 is controlled.
摘要翻译：在一个实施例中的气流控制装置10包括：涡流脱落结构部分20，其以流动方向排出在流动方向上流动的气流的涡流; 以及经由电介质设置在涡流脱落结构部20的下游侧的第一电极40和第二电极41。通过在第一电极40和第二电极41之间施加电压，控制涡流脱落结构部20的下游侧的气流。

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