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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。

8. 发明授权

US5533864A Turbine cooling blade having inner hollow structure with improved cooling 失效
标题翻译：涡轮冷却叶片具有内部中空结构，具有改进的冷却
公开(公告)号：US5533864A
公开(公告)日：1996-07-09
申请号：US343956
申请日：1994-11-17
申请人： Hideo Nomoto , Takanari Okamura , Shoko Ito
发明人： Hideo Nomoto , Takanari Okamura , Shoko Ito
IPC分类号： F01D5/18 , F23R3/00
CPC分类号： F01D5/186 , F01D5/188 , F23R3/002 , F05D2240/81 , F05D2260/201 , F05D2260/202 , F23R2900/03044
摘要： A turbine cooling blade has a blade body defining an inner hollow portion, an insert core fitted into the inner hollow portion of the blade body with a space therebetween, and a plurality of projections formed on the insert core so as to project towards an inner surface of the blade body. The projections are formed with impingement holes through which cooling air flows from an inside of the insert core towards the space between the insert core and the blade body. The blade body is provided with a plurality of partitioning members partitioning the space into a plurality of sectioned chambers between the insert core and an inner surface of the blade body. The insert core member is formed with a number of impingement holes at portions other than the partitioning members, and the partitioning members extend in a span direction of the blade body. Cooling air flows from an inside of the insert core towards the chambers through the impingement holes, and the blade body is provided with a plurality of film cooling holes each penetrating the blade body from the chambers to an outer atmosphere side of the blade body and extending in a radial direction the blade body.
摘要翻译：涡轮冷却叶片具有限定内部中空部分的刀片体，插入到叶片本体的中空部分中的插入芯，其间具有空间;多个突起，其形成在插入芯上，以朝向内表面突出的刀片体。突起形成有冲击孔，冷却空气通过该冲击孔从插入芯的内部朝向插入芯和叶片本体之间的空间流动。叶片体设置有多个分隔构件，其将空间分隔成插入芯和叶片本体的内表面之间的多个分段室。插入芯构件在除了分隔构件之外的部分处形成有多个冲击孔，并且分隔构件在叶片体的跨度方向上延伸。冷却空气从插入芯的内部通过冲击孔流向室，并且叶片本体设置有多个薄膜冷却孔，每个薄膜冷却孔从叶片主体的腔室穿过叶片主体的外部空气侧并延伸在径向方向上的刀片体。

9. 发明授权

US6123998A Ceramic coating method for metallic substrate utilizing a transitional layer of ceramic-metal 失效
标题翻译：使用陶瓷金属过渡层的金属基体的陶瓷涂覆方法
公开(公告)号：US6123998A
公开(公告)日：2000-09-26
申请号：US779117
申请日：1997-01-06
申请人： Masashi Takahashi , Yoshiyasu Itoh , Takanari Okamura
发明人： Masashi Takahashi , Yoshiyasu Itoh , Takanari Okamura
IPC分类号： B05D1/08 , C23C4/02 , C23C4/18 , C25D5/48
CPC分类号： C23C4/02 , C23C4/18
摘要： A ceramic coating method for coating a ceramic on a metallic substrate is disclosed where a ceramic material is coated on a surface of a metallic substrate by continuously changing the composition of a mixture of a ceramic material and a metal to form a ceramic coating film on a surface of the metallic substrate. A heat treatment then is effected to the ceramic coated metallic substrate so as to induce a residual stress due to compression on a surface of the ceramic coating film, thereby improving the durability of the ceramic coating film.
摘要翻译：公开了一种在金属基材上涂覆陶瓷的陶瓷涂覆方法，其中通过连续地改变陶瓷材料和金属的混合物的组成，在金属基材的表面上涂覆陶瓷材料，以在陶瓷涂层上形成陶瓷涂层金属基材的表面。然后对陶瓷涂覆的金属基材进行热处理，以便在陶瓷涂膜的表面上引起由于压缩引起的残余应力，从而提高陶瓷涂膜的耐久性。

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