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1. 发明授权

US08438874B2 Natural gas liquefaction plant and motive power supply equipment for same 失效
标题翻译：天然气液化站和动力供电设备相同
公开(公告)号：US08438874B2
公开(公告)日：2013-05-14
申请号：US12438804
申请日：2008-01-23
申请人： Tomomi Koganezawa , Hidefumi Araki , Shinichi Higuchi , Yasuhiro Horiuchi , Mutsumi Horitsugi
发明人： Tomomi Koganezawa , Hidefumi Araki , Shinichi Higuchi , Yasuhiro Horiuchi , Mutsumi Horitsugi
IPC分类号： F02C3/04 , F02C7/12 , F25J1/00
CPC分类号： F25J1/0055 , C10L3/10 , C10L3/102 , F02C7/18 , F25J1/0022 , F25J1/0052 , F25J1/0212 , F25J1/0242 , F25J1/0268 , F25J1/0284 , F25J1/0292 , F25J2205/50 , F25J2220/66 , F25J2240/80 , F25J2260/80 , Y02E20/16
摘要： Motive power supply equipment for a natural gas liquefaction plant includes gas turbine equipment having a compressor for compressing air, a combustor for generating combustion gases by burning a fuel and the compressed air from the compressor, and a turbine rotated by the combustion gases from the combustor. A low-temperature heat source supply system is provided which, during rated load operation of the gas turbine equipment, supplies carbon dioxide as a cooling medium to the gas turbine equipment in order to cool the gas turbine equipment. The carbon dioxide supplied is generated by separation from the natural gas in the natural gas purification equipment.
摘要翻译：用于天然气液化设备的动力供电设备包括具有用于压缩空气的压缩机的燃气轮机设备，用于通过燃烧燃料产生燃烧气体的燃烧器和来自压缩机的压缩空气的燃烧器和由来自燃烧器的燃烧气体旋转的涡轮机。提供了一种低温热源供应系统，其在燃气轮机设备的额定负载运行期间，将二氧化碳作为冷却介质提供给燃气轮机设备，以便对燃气轮机设备进行冷却。所供应的二氧化碳是通过与天然气净化设备中的天然气分离产生的。

2. 发明授权

US08419365B2 Member having internal cooling passage 有权
标题翻译：会员有内部冷却通道
公开(公告)号：US08419365B2
公开(公告)日：2013-04-16
申请号：US13093400
申请日：2011-04-25
申请人： Nobuaki Kizuka , Yasuhiro Horiuchi , Shinya Marushima , Hidetoshi Kuroki
发明人： Nobuaki Kizuka , Yasuhiro Horiuchi , Shinya Marushima , Hidetoshi Kuroki
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2260/22141
摘要： Provided is a member having an internal cooling passage 7c formed therein and having opposed partition walls 6b, 6c between which a medium flows to cool a parent material, including a first heat transfer rib 25a which extends from almost the center between the opposed partition walls 6b, 6c to one partition wall 6c and slants in a downstream direction of the medium, and a second heat transfer rib 25b which extends from almost the center between the opposed partition walls 6b, 6c to the other partition wall 6b and slants in the downstream direction of the medium, wherein a slit 70a or 70b which passes through between an upstream side of the cooling passage 7c and a downstream side thereof is formed in the first heat transfer rib 70a or the second heat transfer rib 70b.
摘要翻译：本发明提供一种具有形成在其中的内部冷却通道7c并且具有相对的分隔壁6b，6c的构件，介质在其之间流动以冷却母材，其包括第一传热肋25a，第一传热肋25a从相对的间隔壁6b之间的大致中心延伸 6c连接到一个分隔壁6c并且在介质的下游方向上倾斜;以及第二传热肋25b，其从相对的分隔壁6b，6c之间的大致中心延伸到另一分隔壁6b，并且在下游方向上倾斜其中在第一传热肋70a或第二传热肋70b中形成有在冷却通道7c的上游侧和下游侧之间通过的狭缝70a或70b。

3. 发明授权

US07950897B2 Gas turbine and gas turbine cooling method 有权
标题翻译：燃气轮机和燃气轮机冷却方式
公开(公告)号：US07950897B2
公开(公告)日：2011-05-31
申请号：US12366085
申请日：2009-02-05
申请人： Nobuaki Kizuka , Shinya Marushima , Masami Noda , Shinichi Higuchi , Yasuhiro Horiuchi
发明人： Nobuaki Kizuka , Shinya Marushima , Masami Noda , Shinichi Higuchi , Yasuhiro Horiuchi
IPC分类号： F04D27/00
CPC分类号： F01D11/025 , F01D5/081 , F01D11/001
摘要： A gas turbine includes a nozzle vane and a sealing unit engaged with the nozzle vane inside a turbine supplied with combustion gases produced by mixing and burning air for combustion and fuel. The nozzle vane and the sealing unit are disposed in a channel of the downward flowing combustion gases on the outlet side of a gas path. A plurality of engagement portions between the sealing unit and the nozzle vane are provided successively from the upstream side toward the downstream side in a direction of flow of the combustion gases, and a downstream one of the plurality of engagement portions has a contact interface formed in a direction across a turbine rotary shaft. A reduction in the thermal efficiency of the gas turbine can be suppressed.
摘要翻译：燃气轮机包括喷嘴叶片和与喷嘴叶片接合的密封单元，所述涡轮机配备有通过混合和燃烧用于燃烧和燃料的空气而产生的燃烧气体。喷嘴叶片和密封单元设置在气体通道出口侧的向下流动的燃烧气体的通道中。密封单元和喷嘴叶片之间的多个接合部分从燃烧气体的流动方向的上游侧向下游侧连续设置，并且多个接合部中的下游侧具有形成在横跨涡轮旋转轴的方向。可以抑制燃气轮机的热效率的降低。

4. 发明授权

US07587887B2 Advanced humid air turbine power plant 有权
标题翻译：先进的潮湿空气涡轮发电厂
公开(公告)号：US07587887B2
公开(公告)日：2009-09-15
申请号：US11167468
申请日：2005-06-28
申请人： Yasuhiro Horiuchi , Shinya Marushima , Hidefumi Araki , Shigeo Hatamiya
发明人： Yasuhiro Horiuchi , Shinya Marushima , Hidefumi Araki , Shigeo Hatamiya
IPC分类号： F02C3/30 , F02C7/16 , F02C7/18
CPC分类号： F02C3/30 , F02C7/18
摘要： An advanced humid air turbine power plant capable of suppressing condensation of moisture in a cooling channel, which is provided to cool a high-temperature component of a gas turbine, in a start up stage, a coast down stage, and a load varying state of the gas turbine. In the advanced humid air turbine power plant comprising a compressed air supply line for supplying compressed air generated by a compressor to the high-temperature component of the gas turbine, and a humidified air supply line for supplying humidified air generated in a humidifying tower to the high-temperature component of the gas turbine, the power plant further comprises valves capable of adjusting respective air flow rates in the compressed air supply line and the humidified air supply line. A coolant is switched over from the compressed air to the humidified air in the start up stage and the load increasing stage of the gas turbine, and from the humidified air to the compressed air in the load decreasing stage and the coast down stage, as well as in the event of an abnormality in a humidifying line.
摘要翻译：一种先进的湿式空气涡轮发电厂，其能够抑制在启动阶段，下降阶段和负载变化状态下设置用于冷却燃气轮机的高温部件的冷却通道中的水分的冷凝燃气轮机。在先进的湿式空气涡轮发电厂中，包括用于将由压缩机产生的压缩空气供给到燃气轮机的高温部件的压缩空气供给管线，以及用于将在加湿塔中产生的加湿空气供给到加湿塔燃气轮机的高温部件，发电厂还包括能够调节压缩空气供应管线和加湿空气供应管线中的相应空气流量的阀。在起动阶段和燃气轮机的负载增加阶段以及在减载阶段和下降阶段的加湿空气到压缩空气中，冷却剂从压缩空气切换到加湿空气，以及如在加湿线中发生异常的情况。

5. 发明申请

US20090196738A1 GAS TURBINE AND GAS TURBINE COOLING METHOD 有权
公开(公告)号：US20090196738A1
公开(公告)日：2009-08-06
申请号：US12405802
申请日：2009-03-17
申请人： Nobuaki KIZUKA , Shinya MARUSHIMA , Masami NODA , Shinichi HIGUCHI , Yasuhiro HORIUCHI
发明人： Nobuaki KIZUKA , Shinya MARUSHIMA , Masami NODA , Shinichi HIGUCHI , Yasuhiro HORIUCHI
IPC分类号： F01D5/14 , F01D5/02 , F01D5/30
CPC分类号： F01D11/025 , F01D5/081 , F01D11/001
摘要： A gas turbine includes a nozzle vane and a sealing unit engaged with the nozzle vane inside a turbine supplied with combustion gases produced by mixing and burning air for combustion and fuel. The nozzle vane and the sealing unit are disposed in a channel of the downward flowing combustion gases on the outlet side of a gas path. A plurality of engagement portions between the sealing unit and the nozzle vane are provided successively from the upstream side toward the downstream side in a direction of flow of the combustion gases, and a downstream one of the plurality of engagement portions has a contact interface formed in a direction across a turbine rotary shaft. A reduction in the thermal efficiency of the gas turbine can be suppressed.

6. 发明申请

US20080276059A1 APPARATUS AND METHODS FOR SETTING SECURITY TO STORAGE UNIT AND COMPUTER 有权
标题翻译：用于设置存储单元和计算机的安全性的装置和方法
公开(公告)号：US20080276059A1
公开(公告)日：2008-11-06
申请号：US12110279
申请日：2008-04-25
申请人： Yasuhiro Horiuchi , Kohsuke Ohtani , Kazunobu Umeda
发明人： Yasuhiro Horiuchi , Kohsuke Ohtani , Kazunobu Umeda
IPC分类号： G06F12/14 , G06F15/177
CPC分类号： G06F21/80 , G06F21/78
摘要： Methods and apparatus are provided for inhibiting data writing to an optical disc drive connected to a computer. A BIOS confirms presence of a security function of an optical disc drive. When the optical disc drive possesses the security function, the BIOS delivers a command to the optical disc drive to set it to a read-only mode. The optical disc drive that has received the command sets the drive per se to operate in the read-only mode. Since a command for setting it to the read-only mode and a command for releasing it are delivered to the optical disc drive only by the BIOS, when a control is transferred to an Operating System (OS), setting of the read-only mode cannot be released by the OS and other OS's, or application software.
摘要翻译：提供了用于禁止向连接到计算机的光盘驱动器的数据写入的方法和装置。 BIOS确认存在光盘驱动器的安全功能。当光盘驱动器具有安全功能时，BIOS向光盘驱动器发送命令以将其设置为只读模式。接收到该命令的光盘驱动器将驱动器本身设置为只读模式。由于只有通过BIOS将用于将其设置为只读模式的命令和用于释放它的命令才被传送到光盘驱动器，所以当将控制传送到操作系统（OS）时，设置只读模式不能由操作系统和其他操作系统或应用软件发布。

7. 发明授权

US07383817B2 Injector 有权
标题翻译：注射器
公开(公告)号：US07383817B2
公开(公告)日：2008-06-10
申请号：US11713015
申请日：2007-03-02
申请人： Yasuhiro Horiuchi , Yutaka Miyamoto
发明人： Yasuhiro Horiuchi , Yutaka Miyamoto
IPC分类号： F02M57/02 , F02M57/00
CPC分类号： F02M57/025 , F02M47/025 , F02M57/026 , F02M63/0029 , F02M63/0047
摘要： An injector includes a boosting mechanism and a nozzle. The boosting mechanism boosts fuel, and the nozzle injects and supplies the fuel boosted by the boosting mechanism. The boosting mechanism includes a tubular piston and a column piston. The tubular piston has a bore, which extends through the tubular piston in a direction of a longitudinal axis of the tubular piston. The column piston is loosely received by the tubular piston and has an end portion, which projects from the tubular piston, and which is engaged with the tubular piston. The tubular piston is slidably received by a first cylinder. The end portion of the column piston is slidably received by a second cylinder, which is provided generally coaxially to the first cylinder, and which has a diameter different from that of the first cylinder.
摘要翻译：喷射器包括升压机构和喷嘴。增压机构增加燃料，并且喷嘴喷射并提供由增压机构增压的燃料。增压机构包括管状活塞和柱塞活塞。管状活塞具有孔，其沿管状活塞的纵向轴线的方向延伸穿过管状活塞。柱形活塞被管状活塞松动地容纳，并且具有从管状活塞突出并与管状活塞接合的端部。管状活塞由第一气缸可滑动地容纳。柱式活塞的端部可滑动地被第二圆柱体容纳，该第二圆筒与第一圆柱体大致同轴地设置，并且具有不同于第一圆柱体的直径。

8. 发明申请

US20070017227A1 Advanced humid air turbine power plant 有权
标题翻译：先进的潮湿空气涡轮发电厂
公开(公告)号：US20070017227A1
公开(公告)日：2007-01-25
申请号：US11167468
申请日：2005-06-28
申请人： Yasuhiro Horiuchi , Shinya Marushima , Hidefumi Araki , Shigeo Hatamiya
发明人： Yasuhiro Horiuchi , Shinya Marushima , Hidefumi Araki , Shigeo Hatamiya
IPC分类号： F02C3/30
CPC分类号： F02C3/30 , F02C7/18
摘要： An advanced humid air turbine power plant capable of suppressing condensation of moisture in a cooling channel, which is provided to cool a high-temperature component of a gas turbine, in a start up stage, a coast down stage, and a load varying state of the gas turbine. In the advanced humid air turbine power plant comprising a compressed air supply line for supplying compressed air generated by a compressor to the high-temperature component of the gas turbine, and a humidified air supply line for supplying humidified air generated in a humidifying tower to the high-temperature component of the gas turbine, the power plant further comprises valves capable of adjusting respective air flow rates in the compressed air supply line and the humidified air supply line. A coolant is switched over from the compressed air to the humidified air in the start up stage and the load increasing stage of the gas turbine, and from the humidified air to the compressed air in the load decreasing stage and the coast down stage, as well as in the event of an abnormality in a humidifying line.
摘要翻译：一种先进的湿式空气涡轮发电厂，其能够抑制在启动阶段，下降阶段和负载变化状态下设置用于冷却燃气轮机的高温部件的冷却通道中的水分冷凝燃气轮机。在先进的湿式空气涡轮发电厂中，包括用于将由压缩机产生的压缩空气供给到燃气轮机的高温部件的压缩空气供给管线，以及用于将在加湿塔中产生的加湿空气供给到加湿塔燃气轮机的高温部件，发电厂还包括能够调节压缩空气供应管线和加湿空气供应管线中的相应空气流量的阀。在起动阶段和燃气轮机的负载增加阶段以及在减载阶段和下降阶段的加湿空气到压缩空气中，冷却剂从压缩空气切换到加湿空气，以及如在加湿线中发生异常的情况。

9. 发明授权

US06311674B1 Fuel injection system for internal combustion engine 有权
标题翻译：内燃机燃油喷射系统
公开(公告)号：US06311674B1
公开(公告)日：2001-11-06
申请号：US09291181
申请日：1999-04-14
申请人： Toshihiko Igashira , Shigeiku Enomoto , Tadaaki Makino , Yutaka Miyamoto , Yasuhiro Horiuchi , Nobuhiko Shima
发明人： Toshihiko Igashira , Shigeiku Enomoto , Tadaaki Makino , Yutaka Miyamoto , Yasuhiro Horiuchi , Nobuhiko Shima
IPC分类号： F02M4100
CPC分类号： F02D41/3845 , F02D41/408 , F02D2041/2027 , F02M59/34 , F02M63/0017 , F02M63/004 , F02M63/0225 , Y02T10/44
摘要： A fuel injection apparatus for an internal combustion engine is provided which is designed to control a fuel discharge from a fuel injection pump by regulating the quantity of fuel sucked into the fuel injection pump. The fuel injection pump is driven in synchronism with rotation of the engine to pressurize and supply the fuel to an accumulator chamber from which the fuel is injected into cylinders of the engine. The solenoid valve moves a valve member linearly to open and close a fluid path leading to the fuel injection pump. The controller actuates the solenoid valve in one of a first control mode when the engine speed is low and a second control mode when the engine speed is high. In the first control mode, a valve on-duration in which the solenoid valve is turned on to open the fluid path through the valve member and an area of the fluid path opened by the valve member are both controlled. In the second control mode, only the opened area of the fluid path is controlled. This achieves fine adjustment of quantity of fuel discharged from the fuel injection pump over a wide range of engine speeds.
摘要翻译：提供了一种用于内燃机的燃料喷射装置，其被设计成通过调节吸入燃料喷射泵的燃料量来控制来自燃料喷射泵的燃料排放。燃料喷射泵与发动机的旋转同步地驱动，以将燃料加压和供给到蓄能室，燃料从该腔室喷射到发动机的气缸中。电磁阀线性地移动阀构件以打开和关闭通向燃料喷射泵的流体路径。当发动机转速低时，控制器以第一控制模式中的一个启动电磁阀，当发动机转速高时，控制器启动第二控制模式。在第一控制模式中，控制电磁阀打开以打开通过阀构件的流体路径的阀持续时间和由阀构件打开的流体路径的区域。在第二控制模式中，仅控制流体路径的打开区域。这实现了在大范围的发动机转速下从燃料喷射泵排出的燃料量的微调。

10. 发明授权

US4469068A Fuel injection apparatus 失效
标题翻译：燃油喷射装置
公开(公告)号：US4469068A
公开(公告)日：1984-09-04
申请号：US438724
申请日：1982-11-03
申请人： Masatoshi Kuroyanagi , Masahiko Suzuki , Yasuhiro Horiuchi
发明人： Masatoshi Kuroyanagi , Masahiko Suzuki , Yasuhiro Horiuchi
IPC分类号： F02M41/12 , F02M45/12 , F02M59/22 , F02M39/00 , F02D1/06
CPC分类号： F02M45/12 , F02M41/123 , F02M59/22
摘要： A fuel injection apparatus injects a high-pressure fuel to each combustion chamber of an internal combustion engine. The fuel injection apparatus is provided with an accumulator which controls an amount of injection and an injection period of the high-pressure fuel compressed and supplied from the fuel pressure chamber in accordance with the operation of the internal combustion engine.
摘要翻译：燃料喷射装置将高压燃料喷射到内燃机的每个燃烧室。燃料喷射装置设置有蓄能器，其根据内燃机的运转来控制从燃料压力室压缩并供给的高压燃料的喷射量和喷射周期。

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