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31. 发明授权

US07313919B2 Gas turbine combustor 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US07313919B2
公开(公告)日：2008-01-01
申请号：US10784216
申请日：2004-02-24
申请人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Isao Takehara
发明人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Isao Takehara
IPC分类号： F02C7/228
CPC分类号： F23R3/36 , F23R3/10 , F23R3/28 , F23R3/286 , F23R2900/03282
摘要： A gas turbine combustor has a combustion chamber into which fuel and air are supplied, wherein the fuel and the air are supplied into said combustion chamber as a plurality of coaxial jets.
摘要翻译：燃气轮机燃烧器具有供给燃料和空气的燃烧室，其中燃料和空气作为多个同轴喷嘴供应到所述燃烧室中。

32. 发明授权

US07043924B2 Turbine power plant, installation process and removal process of the turbine power plant 有权
标题翻译：涡轮发电厂，涡轮发电厂的安装过程和拆除过程
公开(公告)号：US07043924B2
公开(公告)日：2006-05-16
申请号：US10081202
申请日：2002-02-25
申请人： Hidetoshi Kuroki , Isao Takehara , Yasuyuki Watanabe , Seisaku Takihana
发明人： Hidetoshi Kuroki , Isao Takehara , Yasuyuki Watanabe , Seisaku Takihana
IPC分类号： F02C7/20
CPC分类号： F16M5/00 , F01D25/285 , F05D2230/60 , Y10T29/49229
摘要： A turbine power plant includes power generation apparatuses divided into a plurality of modules, a common base mounting thereon the power generation apparatuses and a supporting apparatus for supporting the common base. The common base is constructed so as to be commonly used as a part of a transportation vehicle and as a frame of the power plant.
摘要翻译：涡轮发电厂包括分为多个模块的发电装置，其上安装有发电装置的公共基座和用于支撑公共基座的支撑装置。共同基座被构造成通常用作运输车辆的一部分和作为发电厂的框架。

33. 发明申请

US20060088411A1 Ni-Fe based super alloy, process of producing the same and gas turbine 有权
标题翻译： Ni-Fe基超级合金，其制造方法和燃气轮机
公开(公告)号：US20060088411A1
公开(公告)日：2006-04-27
申请号：US11206131
申请日：2005-08-18
申请人： Shinya Imano , Hiroyuki Doi , Isao Takehara , Shigeo Sakurai
发明人： Shinya Imano , Hiroyuki Doi , Isao Takehara , Shigeo Sakurai
IPC分类号： F04D29/44
CPC分类号： C22C19/056 , C22C19/058 , C22F1/10 , F01D5/02 , F01D25/005
摘要： A Ni—Fe based super alloy having high strength and toughness at high temperatures even when used in high-temperature environments, and a process of producing the super alloy. A turbine disk using the super alloy, a process of producing the turbine disk, a turbine spacer using the super alloy, and a process of producing the turbine spacer, as well as a gas turbine are also provided. The Ni—Fe based super alloy contains not more than 0.03% by weight of C, 14-18% of Cr, 15-45% of Fe, 0.5-2.0% of Al, not more than 0.05% of N, 0.5 to 2.0% of Ti, 1.5-5.0% of Nb, and Ni as a main ingredient.
摘要翻译：即使在高温环境下使用时，也能够在高温下具有高强度和韧性的Ni-Fe系超合金，以及超合金的制造方法。还提供了使用超级合金的涡轮盘，制造涡轮盘的方法，使用超级合金的涡轮间隔件，以及制造涡轮间隔件的工艺以及燃气轮机。 Ni-Fe基超合金含有不超过0.03重量％的Cr，14-18％的Cr，15-45％的Fe，0.5-2.0％的Al，不超过0.05的N，0.5-2.0 Ti的％，Nb的1.5〜5.0％，Ni为主要成分。

34. 发明授权

US06871504B2 Turbine power plant, installation process and removal process of the turbine power plant 有权
标题翻译：涡轮发电厂，涡轮发电厂的安装过程和拆除过程
公开(公告)号：US06871504B2
公开(公告)日：2005-03-29
申请号：US10673568
申请日：2003-09-30
申请人： Hidetoshi Kuroki , Isao Takehara , Yasuyuki Watanabe , Seisaku Takihana
发明人： Hidetoshi Kuroki , Isao Takehara , Yasuyuki Watanabe , Seisaku Takihana
IPC分类号： F01K13/00 , F01D25/28 , F02C7/20 , F16M5/00 , H02K5/00
CPC分类号： F16M5/00 , F01D25/285 , F05D2230/60 , Y10T29/49229
摘要： A turbine power plant comprises power generation apparatuses divided a plurality of modules, a common base mounting thereon the power generation apparatuses and a supporting apparatus for supporting the common base, and is characterized by a construction of the common base, constructed so as to be commonly used with a part of a transportation vehicle and a frame of the power plant.
摘要翻译：涡轮动力装置包括分割多个模块的发电装置，在其上安装发电装置的公共基座和用于支撑共同基座的支撑装置，其特征在于，构成为共同的基座与运输车辆的一部分和发电厂的框架一起使用。

35. 发明授权

US08043068B2 Ni-Fe based super alloy, process of producing the same and gas turbine 有权
标题翻译： Ni-Fe基超级合金，其制造方法和燃气轮机
公开(公告)号：US08043068B2
公开(公告)日：2011-10-25
申请号：US11206131
申请日：2005-08-18
申请人： Shinya Imano , Hiroyuki Doi , Isao Takehara , Shigeo Sakurai
发明人： Shinya Imano , Hiroyuki Doi , Isao Takehara , Shigeo Sakurai
IPC分类号： F01D5/14
CPC分类号： C22C19/056 , C22C19/058 , C22F1/10 , F01D5/02 , F01D25/005
摘要： A Ni—Fe based super alloy having high strength and toughness at high temperatures even when used in high-temperature environments, and a process of producing the super alloy. A turbine disk using the super alloy, a process of producing the turbine disk, a turbine spacer using the super alloy, and a process of producing the turbine spacer, as well as a gas turbine are also provided. The Ni—Fe based super alloy contains not more than 0.03% by weight of C, 14-18% of Cr, 15-45% of Fe, 0.5-2.0% of Al, not more than 0.05% of N, 0.5 to 2.0% of Ti, 1.5-5.0% of Nb, and Ni as a main ingredient.
摘要翻译：即使在高温环境下使用时，也能够在高温下具有高强度和韧性的Ni-Fe系超合金，以及超合金的制造方法。还提供了使用超级合金的涡轮盘，制造涡轮盘的方法，使用超级合金的涡轮间隔件，以及制造涡轮间隔件的工艺以及燃气轮机。 Ni-Fe基超合金含有不超过0.03重量％的Cr，14-18％的Cr，15-45％的Fe，0.5-2.0％的Al，不超过0.05的N，0.5-2.0 Ti的％，Nb的1.5〜5.0％，Ni为主要成分。

36. 发明授权

US07891191B2 Combustor, gas turbine combustor, and air supply method for same 有权
公开(公告)号：US07891191B2
公开(公告)日：2011-02-22
申请号：US11209608
申请日：2005-08-24
申请人： Shouhei Yoshida , Yoshitaka Hirata , Hiroshi Inoue , Tomoya Murota , Toshifumi Sasao , Akinori Hayashi , Isao Takehara
发明人： Shouhei Yoshida , Yoshitaka Hirata , Hiroshi Inoue , Tomoya Murota , Toshifumi Sasao , Akinori Hayashi , Isao Takehara
IPC分类号： F02C7/057
CPC分类号： F23D11/104 , F23D11/105 , F23R3/286
摘要： A combustor comprises a liquid fuel nozzle for injecting liquid fuel to a combustion chamber, and an air supply nozzle disposed around the liquid fuel nozzle and injecting air. The air supply nozzle is disposed such that air is injected from the air supply nozzle in a direction toward an axis of the liquid fuel nozzle. A space is formed around an outlet of the liquid fuel nozzle, through which the liquid fuel is injected from the liquid fuel nozzle to the combustion chamber, upstream of a distal end of the outlet in a direction in which the liquid fuel is injected. Carbonaceous deposits on surrounding surfaces of the outlet of the liquid fuel nozzle can be suppressed regardless of the operating conditions of a combustor.

37. 发明授权

US07200998B2 Gas turbine combustor and operating method thereof 有权
公开(公告)号：US07200998B2
公开(公告)日：2007-04-10
申请号：US11136570
申请日：2005-05-25
申请人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Isao Takehara
发明人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Isao Takehara
IPC分类号： F02C7/22
CPC分类号： F23R3/10 , F02C7/22 , F02C7/232 , F23R3/28 , F23R3/286 , F23R3/36 , F23R2900/03282
摘要： A gas turbine combustor has a combustion chamber into which fuel and air are supplied, wherein the fuel and the air are supplied into said combustion chamber as a plurality of coaxial jets.

38. 发明申请

US20060053802A1 Ignition detecting method for gas turbine 失效
标题翻译：燃气轮机点火检测方法
公开(公告)号：US20060053802A1
公开(公告)日：2006-03-16
申请号：US11206732
申请日：2005-08-19
申请人： Toshifumi Sasao , Youtarou Kimura , Isao Takehara
发明人： Toshifumi Sasao , Youtarou Kimura , Isao Takehara
IPC分类号： F02C7/00
CPC分类号： F23N5/242 , F23N5/003 , F23N2027/02 , F23N2031/12 , F23N2041/20
摘要： A gas turbine which can detect ignition in a combustor regardless of startup conditions of the gas turbine, such as the hot startup or the cold startup. An ignition detecting method for the gas turbine comprises the steps of calculating a difference between the exhaust temperature detected at a particular time before outputting of an ignition command for a combustor and the exhaust temperature detected after the outputting of the ignition command, and determining that the combustor is ignited, when the calculated difference is not less than a predetermined value. As an alternative, the method includes a step of determining that the combustor is ignited, when a change amount or rate of the exhaust temperature exceeds a predetermined value in a predetermined period from the outputting time of the ignition command.
摘要翻译：一种燃气轮机，其可以检测燃烧器中的点火，而不管燃气轮机的启动条件如热启动或冷启动。燃气轮机的点火检测方法包括以下步骤：计算在输出燃烧器的点火命令之前的特定时间检测到的排气温度与在点火命令输出之后检测到的排气温度之间的差异，并且确定当计算出的差异不小于预定值时，点燃燃烧器。作为替代，该方法包括当从点火命令的输出时间起的预定时间段内的排气温度的变化量或速率超过预定值时，确定燃烧器被点燃的步骤。

39. 发明申请

US20050210880A1 Gas turbine combustor and operating method thereof 有权
标题翻译：燃气轮机燃烧器及其运行方法
公开(公告)号：US20050210880A1
公开(公告)日：2005-09-29
申请号：US11136554
申请日：2005-05-25
申请人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Isao Takehara
发明人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Isao Takehara
IPC分类号： F02C7/22 , F02C7/232 , F23R3/10 , F23R3/28 , F23R3/36
CPC分类号： F23R3/10 , F02C7/22 , F02C7/232 , F23R3/28 , F23R3/286 , F23R3/36 , F23R2900/03282
摘要： A gas turbine combustor has a combustion chamber into which fuel and air are supplied, wherein the fuel and the air are supplied into said combustion chamber as a plurality of coaxial jets.
摘要翻译：燃气轮机燃烧器具有供给燃料和空气的燃烧室，其中燃料和空气作为多个同轴喷嘴供应到所述燃烧室中。

40. 发明授权

US06813889B2 Gas turbine combustor and operating method thereof 有权
标题翻译：燃气轮机燃烧器及其运行方法
公开(公告)号：US06813889B2
公开(公告)日：2004-11-09
申请号：US10083360
申请日：2002-02-27
申请人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Isao Takehara
发明人： Hiroshi Inoue , Tomomi Koganezawa , Nariyoshi Kobayashi , Isao Takehara
IPC分类号： F02C7228
CPC分类号： F23R3/36 , F23R3/10 , F23R3/28 , F23R3/286 , F23R2900/03282
摘要： A gas turbine combustor has a combustion chamber into which fuel and air are supplied, wherein the fuel and the air are supplied into said combustion chamber as a plurality of coaxial jets.

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