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1. 发明授权

US06993913B2 Gas turbine plant 失效
标题翻译：燃气轮机厂
公开(公告)号：US06993913B2
公开(公告)日：2006-02-07
申请号：US10657213
申请日：2003-09-09
申请人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
发明人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
IPC分类号： F02C7/224
CPC分类号： F02C7/12 , F02C7/185 , F02C7/224 , F05D2260/205 , Y02E20/14 , Y02E20/16
摘要： A gas turbine plant comprises an air compressor, gas turbine including at least one high temperature section, a driven equipment, which are operatively connected in series, a gas turbine combustor arranged between the air compressor and the gas turbine, a fuel system disposed for supplying a fuel to the gas turbine combustor, and a heat exchange section for heating the fuel from the fuel by means of a high pressure air as a heating medium fed from the air compressor.
摘要翻译：一种燃气轮机设备包括空气压缩机，包括至少一个高温部分的燃气轮机，可操作地串联连接的驱动设备，布置在空气压缩机和燃气轮机之间的燃气涡轮机燃烧器，设置用于供应的燃料系统燃料到燃气轮机燃烧器，以及热交换部分，用于通过高压空气加热来自燃料的燃料，作为从空气压缩机供给的加热介质。

2. 发明授权

US06857270B2 Gas turbine plant 失效
标题翻译：燃气轮机厂
公开(公告)号：US06857270B2
公开(公告)日：2005-02-22
申请号：US10657212
申请日：2003-09-09
申请人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
发明人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
IPC分类号： F02C6/18 , F02C7/18 , F02C7/224
CPC分类号： F02C7/12 , F02C7/185 , F02C7/224 , F05D2260/205 , Y02E20/14 , Y02E20/16
摘要： A gas turbine plant comprises an air compressor, gas turbine including at least one high temperature section, a driven equipment, which are operatively connected in series, a gas turbine combustor arranged between the air compressor and the gas turbine, a fuel system disposed for supplying a fuel to the gas turbine combustor, and a heat exchange section for heating the fuel from the fuel by means of a high pressure air as a heating medium fed from the air compressor.
摘要翻译：一种燃气轮机设备包括空气压缩机，包括至少一个高温部分的燃气轮机，可操作地串联连接的驱动设备，布置在空气压缩机和燃气轮机之间的燃气涡轮机燃烧器，设置用于供应的燃料系统燃料到燃气轮机燃烧器，以及热交换部分，用于通过高压空气加热来自燃料的燃料，作为从空气压缩机供给的加热介质。

3. 发明申请

US20060225425A1 Gas turbine plant 失效
公开(公告)号：US20060225425A1
公开(公告)日：2006-10-12
申请号：US11305192
申请日：2005-12-19
申请人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
发明人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
IPC分类号： F02C7/12
CPC分类号： F02C7/12 , F02C7/185 , F02C7/224 , F05D2260/205 , Y02E20/14 , Y02E20/16
摘要： A gas turbine plant comprises an air compressor, gas turbine including at least one high temperature section, a driven equipment, which are operatively connected in series, a gas turbine combustor arranged between the air compressor and the gas turbine, a fuel system disposed for supplying a fuel to the gas turbine combustor, and a heat exchange section for heating the fuel from the fuel by means of a high pressure air as a heating medium fed from the air compressor.

4. 发明授权

US06679059B2 Gas turbine plant 失效
标题翻译：燃气轮机厂
公开(公告)号：US06679059B2
公开(公告)日：2004-01-20
申请号：US10286790
申请日：2002-11-04
申请人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
发明人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
IPC分类号： F02C718
CPC分类号： F02C7/12 , F02C7/185 , F02C7/224 , F05D2260/205 , Y02E20/14 , Y02E20/16
摘要： A gas turbine plant comprises an air compressor, gas turbine turbine including at least one high temperature section, a driven equipment, which are operatively connected in series, a gas turbine combustor arranged between the air compressor and the gas turbine, a fuel system disposed for supplying a fuel to the gas turbine combustor, and a heat exchange section for heating the fuel from the fuel by means of a high pressure air as a heating medium fed from the air compressor.
摘要翻译：一种燃气轮机设备包括空气压缩机，包括至少一个高温部分的燃气涡轮机涡轮机，串联地可操作地连接的驱动设备，布置在空气压缩机和燃气涡轮机之间的燃气涡轮机燃烧器，设置用于向燃气轮机燃烧器供给燃料;以及热交换部，其通过作为从空气压缩机供给的加热介质的高压空气从燃料加热燃料。

5. 发明授权

US07143581B2 Gas turbine plant 失效
公开(公告)号：US07143581B2
公开(公告)日：2006-12-05
申请号：US11305192
申请日：2005-12-19
申请人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
发明人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
IPC分类号： F02C7/224
CPC分类号： F02C7/12 , F02C7/185 , F02C7/224 , F05D2260/205 , Y02E20/14 , Y02E20/16
摘要： A gas turbine plant comprises an air compressor, gas turbine including at least one high temperature section, a driven equipment, which are operatively connected in series, a gas turbine combustor arranged between the air compressor and the gas turbine, a fuel system disposed for supplying a fuel to the gas turbine combustor, and a heat exchange section for heating the fuel from the fuel by means of a high pressure air as a heating medium fed from the air compressor.

6. 发明授权

US06253554B1 Gas turbine plant with fuel heating and turbine cooling features 有权
标题翻译：具有燃油加热和涡轮冷却功能的燃气轮机厂
公开(公告)号：US06253554B1
公开(公告)日：2001-07-03
申请号：US09154730
申请日：1998-09-17
申请人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
发明人： Tadashi Kobayashi , Takanari Okamura , Shokou Ito , Takashi Sasaki , Akinori Koga
IPC分类号： F02C718
CPC分类号： F02C7/12 , F02C7/185 , F02C7/224 , F05D2260/205 , Y02E20/14 , Y02E20/16
摘要： A gas turbine plant comprises an air compressor, gas turbine including at least one high temperature section, and driven equipment, which are operatively connected in series, a gas turbine combustor arranged between the air compressor and the gas turbine, a fuel system disposed for supplying a fuel to the gas turbine combustor, and a heat exchange section for heating the fuel from the fuel by means of a high pressure air as a heating medium fed from the air compressor.
摘要翻译：燃气轮机设备包括空气压缩机，包括至少一个高温部分的燃气轮机和可操作地串联连接的驱动设备，布置在空气压缩机和燃气轮机之间的燃气轮机燃烧器，设置用于供应的燃料系统燃料到燃气轮机燃烧器，以及热交换部分，用于通过高压空气加热来自燃料的燃料，作为从空气压缩机供给的加热介质。

7. 发明授权

US06227804B1 Gas turbine blade 有权
标题翻译：燃气轮机叶片
公开(公告)号：US06227804B1
公开(公告)日：2001-05-08
申请号：US09258194
申请日：1999-02-26
申请人： Akinori Koga , Hiroyuki Kawagishi , Takanari Okamura , Tsuneo Hijikata , Shokou Ito
发明人： Akinori Koga , Hiroyuki Kawagishi , Takanari Okamura , Tsuneo Hijikata , Shokou Ito
IPC分类号： F01D518
CPC分类号： F01D5/187 , F05D2260/2212 , F05D2260/2214
摘要： A gas turbine blade is provided with a hollow blade effective section and a blade implanted section operatively connected to the blade effective section and the gas turbine blade is formed with: a leading edge passage for guiding a cooling medium from a supply passage of the blade implanted section on a blade leading edge side of the hollow blade effective section; leading edge intermediate passages following the leading edge passage; and a trailing edge passage for guiding the cooling medium from a supply passage of a blade implanted section on a blade trailing edge side of the hollow blade effective section. The leading edge passage being provided with a heat transfer accelerating element which is arranged in a right ascendant state inclined to an advancing flow direction of the cooling medium when supplying the cooling medium from the blade implanted section to a blade tip section side or left (leading edge side) ascendant state from the blade tip section to the blade implanted section. The trailing edge passage being provided with a heat transfer accelerating element which is arranged in a left (trailing edge counter side) ascendant state inclined to the advancing flow direction of the cooling medium when supplying the cooling medium from the blade implanted section to a blade tip section side.
摘要翻译：燃气轮机叶片设置有中空叶片有效部分和可操作地连接到叶片有效部分的叶片植入部分，并且燃气轮机叶片形成有：前缘通道，用于从植入的叶片的叶片的供应通道引导冷却介质在中空叶片有效部分的叶片前缘侧的截面; 在前缘通道之后的前缘中间通道; 以及用于将冷却介质从叶片植入部分的供应通道引导到中空叶片有效部分的叶片后缘侧上的后缘通道。前缘通道设置有传热加速元件，该传热加速元件沿从冷却介质从叶片植入部分向叶片末端部分侧或左侧（前导）提供冷却介质时沿着冷却介质的前进流动方向倾斜的右上升状态边缘侧）从叶片尖端部分到叶片植入部分的上升状态。后缘通道设置有传热促进元件，该传热促进元件布置成在从叶片植入部分将冷却介质供应到叶片尖端时与冷却介质的前进流动方向倾斜的左（后缘相反侧）上升状态剖面。

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