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1. 发明授权

US06250065B1 Gas turbine combustion system and combustor ignition method therefor 有权
标题翻译：燃气轮机燃烧系统及燃烧器点火方法
公开(公告)号：US06250065B1
公开(公告)日：2001-06-26
申请号：US09292385
申请日：1999-04-15
申请人： Shigemi Mandai , Tetsuo Gora , Koichi Nishida , Masataka Ota , Ichiro Fukue , Shinji Akamatsu , Satoshi Tanimura , Hideki Haruta , Tomohisa Takasaki , Teruya Tachibana
发明人： Shigemi Mandai , Tetsuo Gora , Koichi Nishida , Masataka Ota , Ichiro Fukue , Shinji Akamatsu , Satoshi Tanimura , Hideki Haruta , Tomohisa Takasaki , Teruya Tachibana
IPC分类号： F02B300
CPC分类号： F02C7/232
摘要： Liquid fuel purge device uses water, not compressed air as in the prior art, thereby prevented are rapid load change of gas turbine due to sudden discharge of liquid fuel and coking of remaining liquid fuel. Upon supply of liquid fuel to fuel nozzle (05) being stopped, water purge system (15) having stop valve (16) supplies water into fuel system including liquid fuel system (08) and fuel nozzle (05) and liquid fuel remaining therein is purged by water into combustion chamber (013) from the fuel nozzle (05).
摘要翻译：液体燃料净化装置如现有技术那样使用水而不是压缩空气，由此防止了由于液体燃料的突然排放和剩余的液体燃料的焦化引起的燃气轮机的快速负荷变化。在向燃料喷嘴（05）停止供应液体燃料时，具有截止阀（16）的净水系统（15）将水供应到包括液体燃料系统（08）和燃料喷嘴（05）的燃料系统中，其中残留的液体燃料是从燃料喷嘴（05）通过水从燃烧室（013）中清除。

2. 发明授权

US5410884A Combustor for gas turbines with diverging pilot nozzle cone 失效
标题翻译：燃气轮机燃油机具有发散的先导喷嘴锥体
公开(公告)号：US5410884A
公开(公告)日：1995-05-02
申请号：US137343
申请日：1993-10-18
申请人： Ichiro Fukue , Shigemi Mandai , Katsunori Tanaka , Hitoshi Kawabata , Nobuo Sato , Hiroyuki Nishida , Tetsuo Gora
发明人： Ichiro Fukue , Shigemi Mandai , Katsunori Tanaka , Hitoshi Kawabata , Nobuo Sato , Hiroyuki Nishida , Tetsuo Gora
IPC分类号： F23D17/00 , F23R3/28 , F23R3/34 , F23R3/36 , F02C1/00
CPC分类号： F23R3/286 , F23D17/002 , F23R3/34 , F23R3/36 , F23D2205/00
摘要： A gas turbine combustor suppresses the generation of NOx by mixing a fuel and air homogeneously. A pilot nozzle is provided at the center of the gas turbine combustor. A plurality of main nozzles surround the pilot nozzle. A diverging cone projects from the vicinity of the injection port of the pilot nozzle such that the flame from the main nozzles is sustained by the pilot nozzle and NOx is suppressed. The main nozzles can be provided upstream of the injection port of the pilot nozzle in which case an annular premixing nozzle having a throttled exit end is disposed downstream of the main nozzles. The main nozzle may also be in the form of a fuel nozzle having a plurality of tubes, a gaseous fuel being injected through one of the tubes, and liquid fuel being injected into the annular premixing nozzle through the other of the tubes so that the liquid fuel is atomized to mix the fuel and air homogeneously.
摘要翻译：燃气轮机燃烧器通过均匀混合燃料和空气来抑制NOx的产生。在燃气轮机燃烧器的中心设置有先导喷嘴。多个主喷嘴包围引燃喷嘴。发散锥从引燃喷嘴的喷射口附近突出，使得来自主喷嘴的火焰被导向喷嘴维持，并且抑制了NOx。主喷嘴可以设置在先导喷嘴的喷射口的上游，在这种情况下，具有节流出口端的环形预混喷嘴设置在主喷嘴的下游。主喷嘴也可以是具有多个管的燃料喷嘴的形式，气体燃料通过管中的一个喷射，液体燃料通过另一个管注入到环形预混合喷嘴中，使得液体燃料被雾化以均匀地混合燃料和空气。

3. 发明授权

US6116018A Gas turbine plant with combustor cooling system 失效
标题翻译：带燃烧器冷却系统的燃气轮机厂
公开(公告)号：US6116018A
公开(公告)日：2000-09-12
申请号：US35615
申请日：1998-03-05
申请人： Satoshi Tanimura , Shigemi Mandai , Tetsuo Gora , Hiroyuki Nishida
发明人： Satoshi Tanimura , Shigemi Mandai , Tetsuo Gora , Hiroyuki Nishida
IPC分类号： F02C3/30 , F02C7/16 , F02C7/18 , F23M5/08 , F23R3/42
CPC分类号： F23M5/085 , F02C3/30 , F02C7/16 , F05D2260/2322
摘要： A gas turbine plant having a compressor, gas turbine, and combustor, comprising a cooling system adapted to cool the wall of the combustor by means of air compressed by the combustor when the load of the gas turbine and/or the combustion load of the combustor is low, and an additional cooling system adapted to cool the wall of the combustor by means of a cooling medium different from the air in addition to the cooling by means of the air when the load of the gas turbine is increased.
摘要翻译：一种具有压缩机，燃气轮机和燃烧器的燃气轮机设备，包括冷却系统，该冷却系统适用于当燃气轮机的负载和/或燃烧器的燃烧负荷时由燃烧器压缩的空气来冷却燃烧器的壁以及另外的冷却系统，其适于通过不同于空气的冷却介质来冷却燃烧器的壁，以及当燃气轮机的负载增加时，借助于空气的冷却。

4. 发明授权

US5983641A Tail pipe of gas turbine combustor and gas turbine combustor having the same tail pipe 失效
标题翻译：具有相同尾管的燃气轮机燃烧器尾气管和燃气轮机燃烧器
公开(公告)号：US5983641A
公开(公告)日：1999-11-16
申请号：US846579
申请日：1997-04-30
申请人： Shigemi Mandai , Tetsuo Gora , Satoshi Tanimura , Yoshichika Sato
发明人： Shigemi Mandai , Tetsuo Gora , Satoshi Tanimura , Yoshichika Sato
IPC分类号： F01D9/02 , F02C3/14 , F23R3/42
CPC分类号： F01D9/023
摘要： In a tail pipe of gas turbine combustor, the portion just in front of the outlet 104 of tail pipe of gas turbine combustor has a shape such as to be inclined with respect to the axial direction so that the direction changes from the rearward direction to the direction toward the rear in the substantially axial direction, and at this portion, the position of center of curvature 103 in the axial direction on the rotor side lies on the upstream side from the position of center of curvature 102 on the casing side, a bent portion of tail pipe serves as a suction duct, and the occurrence of a negative pressure zone is prevented. Also, by using the tail pipe, a combustor inner tube or a burner provided on the upstream side of the tail pipe having a straight or substantially straight axis is disposed so that the axis of the combustion inner tube or the burner makes an angle with respect to the axis of the tail pipe in such a manner that combustion gas collides with the back side of the tail pipe.
摘要翻译：在燃气轮机燃烧器的尾管中，刚好在燃气轮机燃烧器尾管出口104前方的部分具有相对于轴向方向倾斜的形状，使得该方向从向后方向变为在该部分上，转子侧轴向的曲率中心位置103位于壳体侧的曲率中心位置102的上游侧，弯曲的方向尾管的一部分用作吸气管，并且防止了负压区的发生。此外，通过使用尾管，设置在具有直的或基本上直的轴线的尾管的上游侧设置的燃烧器内管或燃烧器，使得燃烧内管或燃烧器的轴线相对于以尾气管的轴线的方式使得燃烧气体与尾管的背面碰撞。

5. 发明授权

US06631614B2 Gas turbine combustor 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US06631614B2
公开(公告)日：2003-10-14
申请号：US09756188
申请日：2001-01-09
申请人： Shigemi Mandai , Tetsuo Gora , Katsunori Tanaka , Kouichi Nishida
发明人： Shigemi Mandai , Tetsuo Gora , Katsunori Tanaka , Kouichi Nishida
IPC分类号： F23R330
CPC分类号： F23D23/00 , F23D17/002 , F23D2900/00008 , F23R3/286 , F23R3/34
摘要： A gas turbine combustor, in which plural pre-mixers that inject fuel into swirling air passages are arranged to surround a pilot burner, and a pilot flame, guided by a pilot cone in the shape of a flaring pipe and provided at the rear end of the pilot burner, is mixed with a pre-mixture blown out from the pre-mixers to obtain a combustion gas, comprising flame-stabilizing means. The flame-stabilizing means lower the disturbance in a region where the pre-mixture and the pilot flame are mixed or stabilize the pilot flame, so that the flame generated by igniting the pre-mixture with the pilot flame is stabilized. By stabilizing the flame, combustion with a leaner air-fuel ratio is possible, and thereby the amount of NOx can be decreased.
摘要翻译：一种燃气轮机燃烧器，其中将燃料喷射到旋流空气通道中的多个预混合器被布置成围绕引燃燃烧器和引燃火焰，引导火焰由扩口管形式的先导锥体引导并且设置在引燃燃烧器与从预混合器吹出的预混合物混合以获得包含火焰稳定装置的燃烧气体。火焰稳定装置降低预混合物和引燃火焰混合或稳定引燃火焰的区域中的扰动，使得通过用引燃火焰点燃预混合物而产生的火焰是稳定的。通过稳定火焰，可以用较稀的空燃比进行燃烧，从而可以减少NOx的量。

6. 发明授权

US5145753A Solid electrolyte fuel cell 失效
标题翻译：固体电解质燃料电池
公开(公告)号：US5145753A
公开(公告)日：1992-09-08
申请号：US578499
申请日：1990-09-06
申请人： Mitsuhiro Irino , Tetsuo Gora , Masaharu Minami , Hitoshi Miyamoto , Masao Sumi , Nobuyoshi Tomita , Kiyoshi Watanabe , Kazumi Ogura , Masanori Nishiura , Masayuki Funatsu , Kazuhiro Yoshimoto , Koichi Takenobu , Tokuji Satake
发明人： Mitsuhiro Irino , Tetsuo Gora , Masaharu Minami , Hitoshi Miyamoto , Masao Sumi , Nobuyoshi Tomita , Kiyoshi Watanabe , Kazumi Ogura , Masanori Nishiura , Masayuki Funatsu , Kazuhiro Yoshimoto , Koichi Takenobu , Tokuji Satake
IPC分类号： H01M8/02 , H01M8/12 , H01M8/24
CPC分类号： H01M8/0271 , H01M8/1213 , H01M8/2425 , H01M4/9033 , H01M4/9066
摘要： A noble solid electrolyte fuel cell includes a generating layer (5), an interconnector layer (9), and a support layer (10) disposed between the generating and interconnector layers. The interconnector layer comprises a fuel electrode (6), an interconnector material (7) and an oxygen electrode (8). The support layer (10) forms a fuel passage and an oxidizer passage, and supporting rods (15, 102) for gas sealing are disposed at both ends of the support layer. A sealing film (110) is cemented to the contact surfaces of the supporting rods (15, 102) between the generating layer and the interconnector layer, and this sealing film becomes soft or half melted during the operation of the fuel cell. This construction provides improved cell performances due to better sealing of gases even under large temperature differences. The use of finer particles near the surface of the solid electrolyte only is also disclosed.

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