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1. 发明授权

US06209326B1 Gas turbine combustor 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US06209326B1
公开(公告)日：2001-04-03
申请号：US09244030
申请日：1999-02-04
申请人： Shigemi Mandai , Koichi Nishida , Masataka Ota , Tatsuo Ishiguro , Mitsuru Inada , Hideki Haruta
发明人： Shigemi Mandai , Koichi Nishida , Masataka Ota , Tatsuo Ishiguro , Mitsuru Inada , Hideki Haruta
IPC分类号： F02C100
CPC分类号： F23R3/286 , F23C7/004 , F23D14/02 , F23D2205/00 , F23D2206/10 , F23D2900/14021
摘要： To prepare a more homogeneous premixture than that of the device of the prior art thereby to suppress an NOx emission and to lower a fuel feed pressure. A gas turbine combustor comprising: an outer cylinder 106 having main swirlers 101 therein and adapted to be fed with air; and an annular fuel feed manifold 110 disposed at the outer circumference of the outer cylinder 106 on the upstream or downstream side of the main swirlers 101 and having a plurality of nozzle ports 111 communicating with the inside of the outer cylinder 106, so that a fuel is injected from the outer circumference to the center of the air flowing in the outer cylinder 106.
摘要翻译：为了制备比现有技术的装置更均匀的预混合物，从而抑制NOx排放并降低燃料供给压力.1。一种燃气轮机燃烧器，包括：外筒106，其中具有主旋流器101，并适于供给空气; 以及环形燃料供给歧管110，其设置在主旋流器101的上游侧或下游侧的外筒106的外周，并具有与外筒106的内部连通的多个喷嘴口111，从外圆周喷射到在外筒106中流动的空气的中心。

2. 发明授权

US06047551A Multi-nozzle combustor 失效
标题翻译：多喷嘴燃烧器
公开(公告)号：US06047551A
公开(公告)日：2000-04-11
申请号：US35504
申请日：1998-03-05
申请人： Tatsuo Ishiguro , Shigemi Mandai , Mitsuru Inada , Satoshi Tanimura , Kouichi Nishida
发明人： Tatsuo Ishiguro , Shigemi Mandai , Mitsuru Inada , Satoshi Tanimura , Kouichi Nishida
IPC分类号： F23R3/20 , F23C99/00 , F23D11/12 , F23R3/28 , F23R3/34 , F02C7/22
CPC分类号： F23R3/286
摘要： A multi-nozzle combustor comprising a pilot nozzle for flame retention and a plurality of main nozzles arranged around the pilot nozzle, each of the nozzles including an outer cylinder, an inner cylinder, and an annular passage defined between the outer and inner cylinders and forming therein a mixture-evaporation region for a fuel ejected and atomized by an airflow.
摘要翻译：一种多喷嘴燃烧器，包括用于火焰保持的先导喷嘴和围绕引燃喷嘴布置的多个主喷嘴，每个喷嘴包括外筒，内筒和限定在外筒和内筒之间的环形通道，并形成其中用于通过气流喷射和雾化的燃料的混合物蒸发区域。

3. 发明授权

US08813502B2 Cooling structure of gas turbine combustor 有权
标题翻译：燃气轮机燃烧器的冷却结构
公开(公告)号：US08813502B2
公开(公告)日：2014-08-26
申请号：US12598100
申请日：2008-09-24
申请人： Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
发明人： Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
IPC分类号： F02C1/08 , F02G1/055 , F02C7/12 , F23R3/28 , F23R3/00 , F23R3/06
CPC分类号： F23R3/283 , F23R3/005 , F23R3/06 , F23R2900/03042 , F23R2900/03044
摘要： It is required for a gas turbine combustor to exhaust low NOx. The gas turbine combustor is provided with a combustion tube which has a cooling passage through which cooling air flows in a double wall structure. The cooling passage has a main cooling air supply opening opened to a side of a combustion zone. The cooling air supplied from the main cooling air supply opening is guided to a direction along an inner wall surface of the combustion tube by a guide. The cooling air flows through the cooling passage inside the combustion tube, and then is reused for film cooling along the inner wall surface. Thus, it is possible to save cooling air. Therefore, a more part of the air supplied from a compressor can be used as air for combustion and it becomes possible to exhaust low NOx.
摘要翻译：燃气轮机燃烧器需要排出低NOx。燃气轮机燃烧器设置有燃烧管，该燃烧管具有冷却空气以双壁结构流动的冷却通道。冷却通道具有向燃烧区侧面敞开的主冷却空气供给口。从主冷却空气供给口供给的冷却空气通过引导件被引导到燃烧管的内壁面的方向。冷却空气流过燃烧管内的冷却通道，然后再次用于沿内壁表面进行膜冷却。因此，可以节省冷却空气。因此，从压缩机供给的空气的一部分能够用作燃烧用空气，能够排出低NOx。

4. 发明授权

US08698342B2 Wind turbine generating apparatus 失效
标题翻译：风力发电机组
公开(公告)号：US08698342B2
公开(公告)日：2014-04-15
申请号：US13244383
申请日：2011-09-24
申请人： Shigeto Hirai , Shinsuke Sato , Tatsuo Ishiguro
发明人： Shigeto Hirai , Shinsuke Sato , Tatsuo Ishiguro
IPC分类号： F03D9/00 , F03D11/02
CPC分类号： F03D80/60 , F03D9/25 , F05B2240/14 , F05B2240/912 , F05B2260/2241 , F05B2260/64 , Y02E10/726 , Y02E10/728
摘要： A wind turbine generating apparatus includes a rotor head that rotates upon receiving outside wind on a wind turbine blade, a generator that generates electricity, and a nacelle interior air passage through which outside air flows isolatedly from an interior space of the nacelle.
摘要翻译：一种风力涡轮发电装置，包括：转子头，其在接收到风力涡轮机叶片上的外部风力时旋转;发电机，其产生电力;以及机舱内部空气通道，外部空气从所述机舱的内部空间隔离流动。

5. 发明授权

US08661827B2 Plates having cooling channels, and method for welding the plates and increasing a dimension of the cooling channels adjacent the welded section 有权
标题翻译：具有冷却通道的板，以及用于焊接板的方法和增加与焊接部分相邻的冷却通道的尺寸
公开(公告)号：US08661827B2
公开(公告)日：2014-03-04
申请号：US12646115
申请日：2009-12-23
申请人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
发明人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
IPC分类号： F02C1/00
CPC分类号： B23K26/30 , B23K1/0018 , B23K2101/001 , F01D9/023 , F23R3/005 , F23R3/42 , F23R2900/00017 , F23R2900/00018 , Y02T50/67 , Y02T50/675 , Y10T29/49826 , Y10T29/49893 , Y10T428/12493
摘要： A plate-like-object manufacturing method, plate-like objects, a gas-turbine combustor, and a gas turbine, in which degradation in the cooling performance can be suppressed, the time required for manufacturing a gas-turbine combustor can be shortened, and deterioration of the working environment can be prevented are provided. A plate-like-object manufacturing method includes a step of forming a plate-like object by stacking a plurality of plates and arranging a plurality of channels, through which a cooling medium flows, side-by-side between the plurality of plates; and a step of arranging a plurality of the plate-like objects side-by-side in a direction in which the channels are arranged, butting the plurality of plate-like objects against each other, and performing welding at an abutment section. The channels adjacent to the abutment section extend along the abutment section and have a greater dimension in the direction in which the channels are arranged, as compared with that of other channels.
摘要翻译：能够抑制冷却性能的劣化的板状物体，燃气轮机燃烧器和燃气轮机，能够缩短制造燃气轮机燃烧器所需的时间，并且可以防止工作环境的劣化。板状物体的制造方法包括通过堆叠多个板并且在多个板之间并排布置冷却介质流过的多个通道来形成板状物体的步骤; 以及在排列通道的方向并列配置多个板状物体的步骤，使多个板状物体彼此抵接，并在邻接部分进行焊接。与邻接部分相邻的通道相对于其它通道而言沿着邻接部分延伸并且在通道布置方向上具有更大的尺寸。

6. 发明申请

US20100180601A1 COOLING STRUCTURE OF GAS TURBINE COMBUSTOR 有权
标题翻译：燃气轮机组的冷却结构
公开(公告)号：US20100180601A1
公开(公告)日：2010-07-22
申请号：US12598100
申请日：2008-09-24
申请人： Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
发明人： Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
IPC分类号： F02C3/14
CPC分类号： F23R3/283 , F23R3/005 , F23R3/06 , F23R2900/03042 , F23R2900/03044
摘要： It is required for a gas turbine combustor to exhaust low NOx. The gas turbine combustor is provided with a combustion tube which has a cooling passage through which cooling air flows in a double wall structure. The cooling passage has a main cooling air supply opening opened to a side of a combustion zone. The cooling air supplied from the main cooling air supply opening is guided to a direction along an inner wall surface of the combustion tube by a guide. The cooling air flows through the cooling passage inside the combustion tube, and then is reused for film cooling along the inner wall surface. Thus, it is possible to save cooling air. Therefore, a more part of the air supplied from a compressor can be used as air for combustion and it becomes possible to exhaust low NOx.
摘要翻译：燃气轮机燃烧器需要排出低NOx。燃气轮机燃烧器设置有燃烧管，该燃烧管具有冷却空气以双壁结构流动的冷却通道。冷却通道具有向燃烧区侧面敞开的主冷却空气供给口。从主冷却空气供给口供给的冷却空气通过引导件被引导到燃烧管的内壁面的方向。冷却空气流过燃烧管内的冷却通道，然后再次用于沿内壁表面进行膜冷却。因此，可以节省冷却空气。因此，从压缩机供给的空气的一部分能够用作燃烧用空气，能够排出低NOx。

7. 发明授权

US07089741B2 Gas turbine combustor 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US07089741B2
公开(公告)日：2006-08-15
申请号：US10927529
申请日：2004-08-27
申请人： Kazufumi Ikeda , Tatsuo Ishiguro , Katsunori Tanaka , Satoshi Tanimura
发明人： Kazufumi Ikeda , Tatsuo Ishiguro , Katsunori Tanaka , Satoshi Tanimura
IPC分类号： F02C7/24
CPC分类号： F23R3/002 , F23M20/005 , F23R2900/00014
摘要： A gas turbine combustor includes a combustion liner in which a combustion region is formed; and a housing provided for a wall of the combustion liner in a predetermined circumferential region of the combustion liner to form a resonance space between the combustion liner and the housing. The combustion region and the resonance space are connected by a plurality of combustion liner through-holes, and a circumferential length of the housing is longer than a diameter of the combustion liner.
摘要翻译：燃气轮机燃烧器包括其中形成有燃烧区域的燃烧衬套; 以及壳体，其设置在所述燃烧衬套的预定圆周区域中的所述燃烧衬套的壁上，以在所述燃烧衬套和所述壳体之间形成共振空间。燃烧区域和共振空间通过多个燃烧衬套通孔连接，壳体的圆周长度大于燃烧衬套的直径。

8. 发明授权

US08672628B2 Wind turbine generator 有权
标题翻译：风力发电机组
公开(公告)号：US08672628B2
公开(公告)日：2014-03-18
申请号：US13549173
申请日：2012-07-13
申请人： Shinsuke Sato , Tatsuo Ishiguro
发明人： Shinsuke Sato , Tatsuo Ishiguro
IPC分类号： F03D11/04
CPC分类号： F03D80/60 , F05B2240/912 , F05B2260/64 , Y02E10/726 , Y02E10/728
摘要： With a simple and low-cost structure, it is possible to introduce a sufficient amount of external wind while suppressing power consumption, and thereby, inside a nacelle and a tower are satisfactorily cooled. A wind turbine generator, in which a rotor head generates power by driving a generator installed inside a nacelle and in which the nacelle is installed at a top end of a tower, wherein an introducing vent that takes the external wind into an internal space in the wind turbine generator is provided at a portion of an outer circumference surface of the tower or the nacelle that receives positive pressure due to the external wind; and an exhaust vent that externally exhausts cooling air in the internal space is provided at a portion of an outer circumference surface of the tower or the nacelle that receives the negative pressure due to the external wind.
摘要翻译：通过简单且低成本的结构，能够在抑制功率消耗的同时引入足够的外部风力，从而能够令人满意地冷却机舱和塔架内部。一种风力涡轮发电机，其中转子头通过驱动安装在机舱内的发电机并且其中机舱安装在塔架的顶端来产生动力，其中引入通风口将外部风进入内部空间风力发电机设置在由于外部风而接收正压的塔架或机舱的外周面的一部分; 并且外部排出内部空间中的冷却空气的排气口设置在塔架的外周面的一部分或由于外部风而承受负压的机舱。

9. 发明授权

US08476784B2 Wind turbine generating apparatus 有权
标题翻译：风力发电机组
公开(公告)号：US08476784B2
公开(公告)日：2013-07-02
申请号：US13252468
申请日：2011-10-04
申请人： Shinsuke Sato , Shigeto Hirai , Tatsuo Ishiguro
发明人： Shinsuke Sato , Shigeto Hirai , Tatsuo Ishiguro
IPC分类号： F03D9/00
CPC分类号： F03D1/0691 , F03D1/0675 , F03D9/25 , F03D13/20 , F03D80/60 , F03D80/80 , F03D80/88 , F05B2240/14 , F05B2240/221 , F05B2240/30 , F05B2240/912 , F05B2260/201 , Y02E10/721 , Y02E10/728
摘要： In a wind turbine generating apparatus, a heat generating device is provided inside the rotor head and has a hermetically-sealed structure from outside. A rotor head cooling air passage is formed through the periphery of the heat generating device to the inside of a wind turbine blade. A cooling air introduction portion through which cooling air flows and an air outlet from which the cooling air is discharged are provided in the rotor head cooling air passage to thereby form the air outlet in the wind turbine blade.
摘要翻译：在风力涡轮发电装置中，在转子头内部设置有发热装置，并且具有从外部的密封结构。转子头冷却空气通道通过发热装置的周边形成到风力涡轮机叶片的内部。在转子头冷却风通道中设置有冷却空气流过的冷却空气导入部和排出冷却空气的空气出口，从而在风力涡轮机叶片中形成空气出口。

10. 发明申请

US20110146284A1 Plate-like-object manufacturing method, plate-like objects, gas-turbine combustor, and gas turbine 有权
标题翻译：板状物体制造方法，板状物体，燃气轮机燃烧器和燃气轮机
公开(公告)号：US20110146284A1
公开(公告)日：2011-06-23
申请号：US12646115
申请日：2009-12-23
申请人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
发明人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
IPC分类号： F02C3/00 , B23P19/00 , B32B15/00
CPC分类号： B23K26/30 , B23K1/0018 , B23K2101/001 , F01D9/023 , F23R3/005 , F23R3/42 , F23R2900/00017 , F23R2900/00018 , Y02T50/67 , Y02T50/675 , Y10T29/49826 , Y10T29/49893 , Y10T428/12493
摘要： A plate-like-object manufacturing method, plate-like objects, a gas-turbine combustor, and a gas turbine, in which degradation in the cooling performance can be suppressed, the time required for manufacturing a gas-turbine combustor can be shortened, and deterioration of the working environment can be prevented are provided. A plate-like-object manufacturing method includes a step of forming a plate-like object by stacking a plurality of plates and arranging a plurality of channels, through which a cooling medium flows, side-by-side between the plurality of plates; and a step of arranging a plurality of the plate-like objects side-by-side in a direction in which the channels are arranged, butting the plurality of plate-like objects against each other, and performing welding at an abutment section. The channels adjacent to the abutment section extend along the abutment section and have a greater dimension in the direction in which the channels are arranged, as compared with that of other channels.
摘要翻译：能够抑制冷却性能的劣化的板状物体，燃气轮机燃烧器和燃气轮机，能够缩短制造燃气轮机燃烧器所需的时间，并且可以防止工作环境的劣化。板状物体的制造方法包括通过堆叠多个板并且在多个板之间并排布置冷却介质流过的多个通道来形成板状物体的步骤; 以及在排列通道的方向并列配置多个板状物体的步骤，使多个板状物体彼此抵接，并在邻接部分进行焊接。与邻接部分相邻的通道相对于其它通道而言沿着邻接部分延伸并且在通道布置方向上具有更大的尺寸。

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