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1. 发明授权

US5323614A Combustor for gas turbine 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US5323614A
公开(公告)日：1994-06-28
申请号：US3608
申请日：1993-01-13
申请人： Satoshi Tsukahara , Hiroshi Inoue , Noriyuki Hayashi , Kazumi Iwai , Tamio Innami , Yoji Ishibashi , Michio Kuroda , Yasuhiko Otawara , Hiraku Ikeda , Kazuyuki Itoh , Shozo Nakamura , Hidekazu Fujimura , Kazuhito Koyama
发明人： Satoshi Tsukahara , Hiroshi Inoue , Noriyuki Hayashi , Kazumi Iwai , Tamio Innami , Yoji Ishibashi , Michio Kuroda , Yasuhiko Otawara , Hiraku Ikeda , Kazuyuki Itoh , Shozo Nakamura , Hidekazu Fujimura , Kazuhito Koyama
IPC分类号： F02C9/28 , F23R3/28 , F23R3/34 , F02C1/00
CPC分类号： F23R3/286 , F23R3/34
摘要： A premixed combustor for a gas turbine, comprises, a combustion chamber for burning a fuel with an air therein, at least two premixed fuel/air mixture outlets which are juxtaposed with each other, and through each of which a premixed fuel/air mixture flows out into the combustion chamber, and a flow deflection member arranged between the premixed fuel/air mixture outlets, urging the permixed fuel/air mixture from one of the premixed fuel/air mixture outlets to go away from another one of the premixed fuel/air mixture outlets, and terminating in the combustion chamber so that the premixed fuel/air mixture from the one of the premixed fuel/air mixture outlets is permitted to move toward the premixed fuel/air mixture flowing out from the another one of the premixed fuel/air mixture outlets after going away from the another one of the premixed fuel/air mixture outlets.
摘要翻译：一种用于燃气轮机的预混合燃烧器包括：用于燃烧燃料的燃烧室，其中具有空气的至少两个预混合燃料/空气混合物出口彼此并置，并且通过其中预混燃料/空气混合物流动并且设置在预混燃料/空气混合物出口之间的流动偏转构件，从预混合的燃料/空气混合物出口之一推动经过混合的燃料/空气混合物以远离另一种预混燃料/空气混合物出口，并且终止于燃烧室，使得来自预混燃料/空气混合物出口之一的预混合燃料/空气混合物被允许朝向从另一个预混燃料/空气混合物出口流出的预混燃料/空气混合物移动，在离开另一个预混合燃料/空气混合物出口之后的空气混合物出口。

2. 发明授权

US5461855A Method and device for controlling combustors for gasturbine 失效
标题翻译：用于控制燃气燃烧器的方法和装置
公开(公告)号：US5461855A
公开(公告)日：1995-10-31
申请号：US193354
申请日：1994-02-03
申请人： Hiroshi Inoue , Satoshi Tsukahara , Kazumi Iwai
发明人： Hiroshi Inoue , Satoshi Tsukahara , Kazumi Iwai
IPC分类号： F02C9/00 , F01D17/08 , F23R3/26 , F23C1/00
CPC分类号： F01D17/085 , F23R3/26
摘要： A method for controlling a plurality of combustors supplying a pressurized gas to a gas turbine, with each of the combustors including a first air supply for supplying a combustion air into the combustor and a second air supply for adjusting an amount of air supplied into the combustor to change a combustion condition in the combustor. The method comprises the steps of measuring the combustion condition of each of the combustors, measuring a difference between the measured combustion condition of each of the combustors and a desired combustion condition, and changing a rate of the amount of air supplied into the combustor by the second air supply means in relation to an amount of combustion air supplied into the combustor by the first air supply in each of the combustors according to the measured difference of each of the combustors to change the combustion condition of each of the combustors so that the combustion conditions of the combustors are changed to the desired combustion condition.
摘要翻译：一种用于控制向燃气轮机供应加压气体的多个燃烧器的方法，其中每个燃烧器包括用于向燃烧器供应燃烧空气的第一空气供应器和用于调节供应到燃烧器中的空气量的第二空气供应器以改变燃烧器中的燃烧状态。该方法包括以下步骤：测量每个燃烧器的燃烧条件，测量每个燃烧器的测量的燃烧条件与期望的燃烧条件之间的差异，以及改变供应到燃烧器中的空气的量的速率第二空气供给装置相对于通过每个燃烧器中的第一空气供应供应到燃烧器中的燃烧空气的量，根据每个燃烧器的测量差异来改变每个燃烧器的燃烧条件，使得燃烧燃烧器的条件改变为期望的燃烧条件。

3. 发明授权

US5201181A Combustor and method of operating same 失效
标题翻译： COMBUSTOR及其操作方法
公开(公告)号：US5201181A
公开(公告)日：1993-04-13
申请号：US523347
申请日：1990-05-14
申请人： Takashi Ohmori , Yoji Ishibashi , Hiroshi Inoue , Fumio Kato , Takashi Hashimoto , Shigeyuki Akatsu , Michio Kuroda , Seiichi Kirikami
发明人： Takashi Ohmori , Yoji Ishibashi , Hiroshi Inoue , Fumio Kato , Takashi Hashimoto , Shigeyuki Akatsu , Michio Kuroda , Seiichi Kirikami
IPC分类号： F23R3/30 , F23C99/00 , F23R3/34
CPC分类号： F23R3/34 , F05D2270/31
摘要： A combustor includes a first premixture supply device provided in a central portion of a combustion chamber disposed generally concentric with a combustion cylinder, and a second premixture supply means provided adjacent to an outer periphery of the first premixture supply device. The first premixture supply device is operable when the combustor is under a high load, and the second premixture supply device is operable when the combustor is under a low load. A method of operating a combustor is also proposed wherein the combustor comprises a combustion cylinder having a combustion chamber therein and a premixture supply device provided on one side of the combustion cylinder for supplying a combustible mixture to the combustion chamber. The premixture supply device comprising at least two inner and outer premixture supply devices. The outer premixture supply device is operable in a low-load range of the combustor while the inner and outer premixture supply devices are operable in a high-load range of the combustor at above a predetermined load. The first and second premixture supply devices include first and second burners, respectively. The first and second burners are operated in such a manner that the ratio of the load borne by the first burner to the load borne by the second burner is 1:1 in the high-load range.

4. 发明授权

US5127229A Gas turbine combustor 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US5127229A
公开(公告)日：1992-07-07
申请号：US728729
申请日：1991-07-11
申请人： Yoji Ishibashi , Hiroshi Inoue , Takashi Ohmori , Takashi Hashimoto , Fumio Kato , Shigeyuki Akatsu , Akira Arai , Michio Kuroda , Katsukuni Hisano
发明人： Yoji Ishibashi , Hiroshi Inoue , Takashi Ohmori , Takashi Hashimoto , Fumio Kato , Shigeyuki Akatsu , Akira Arai , Michio Kuroda , Katsukuni Hisano
IPC分类号： F02C7/22 , F02C7/26 , F23C99/00 , F23R3/34
CPC分类号： F23R3/34
摘要： A gas turbine combustor including a first-stage combustion chamber being arranged to serve as a premix chamber for a second-stage combustion chamber and an auxiliary burner provided in the first-stage combustion chamber and arranged to effect, when fired, combustion and holding of a flame in the first-stage combustion chamber and to effect, when extinguished, feed a flame from the first-stage combustion chamber to the second-stage combustion chamber.
摘要翻译：一种燃气轮机燃烧器，其包括第一级燃烧室，其被设置为用作第二级燃烧室的预混合室和设置在第一级燃烧室中的辅助燃烧室，并且被布置成在燃烧时燃烧和保持第一级燃烧室中的火焰并且当熄灭时，将火焰从第一级燃烧室供给到第二级燃烧室。

5. 发明授权

US5054280A Gas turbine combustor and method of running the same 失效
标题翻译：燃气轮机燃烧器及其运行方法
公开(公告)号：US5054280A
公开(公告)日：1991-10-08
申请号：US582395
申请日：1990-09-12
申请人： Yoji Ishibashi , Hiroshi Inoue , Takashi Ohmori , Takashi Hashimoto , Fumio Kato , Shigeyuki Akatsu , Akira Arai , Michio Kuroda , Katsukuni Hisano
发明人： Yoji Ishibashi , Hiroshi Inoue , Takashi Ohmori , Takashi Hashimoto , Fumio Kato , Shigeyuki Akatsu , Akira Arai , Michio Kuroda , Katsukuni Hisano
IPC分类号： F02C7/22 , F02C7/26 , F23C99/00 , F23R3/34
CPC分类号： F23R3/34
摘要： A gas turbine combustor including a first-stage combustion chamber being arranged to serve as a premix chamber for a second-stage combustion chamber and an auxiliary burner provided in the first-stage combustion chamber and arranged to effect, when fired, combustion and holding of a flame in the first-stage combustion chamber and to effect, when extinguished, feed a flame from the first-stage combustion chamber to the second-stage combustion chamber; and a method of driving the gas turbine combustor including a step of preparing the auxiliary burner in the first stage combustion chamber, the auxiliary burner being sparked when said combustion is fired, and causing the first-stage combustion camber to serve as the premixing chamber for the second-stage combustion chamber by extinguished the auxiliary burner.
摘要翻译：一种燃气轮机燃烧器，其包括第一级燃烧室，其被设置为用作第二级燃烧室的预混合室和设置在第一级燃烧室中的辅助燃烧室，并且被布置成在燃烧时燃烧和保持第一级燃烧室中的火焰，并且当熄灭时，将火焰从第一级燃烧室供给到第二级燃烧室; 以及驱动所述燃气轮机燃烧器的方法，其包括在所述第一级燃烧室中准备所述辅助燃烧器的步骤，所述辅助燃烧器在所述燃烧被点火时被点火，并且使所述第一级燃烧室用作所述预混合室，第二级燃烧室通过熄灭辅助燃烧器。

6. 发明授权

US4546795A Solenoid valve 失效
标题翻译：电磁阀
公开(公告)号：US4546795A
公开(公告)日：1985-10-15
申请号：US662555
申请日：1984-10-19
申请人： Yoshio Okamoto , Kazumi Iwai , Hiroshi Inoue , Yoshifumi Kunugi , Tadashi Shinozaki
发明人： Yoshio Okamoto , Kazumi Iwai , Hiroshi Inoue , Yoshifumi Kunugi , Tadashi Shinozaki
IPC分类号： F16K31/06 , F16K31/02
CPC分类号： F16K31/0668 , F16K31/0648 , F25B2341/0652 , Y02B30/72 , Y10T137/86421
摘要： A solenoid valve in which a pulse signal is applied to an electromagnet thereof to eliminate an electric hysteresis. The solenoid valve includes a piston-like valve slidably supported in a cylinder, and at least one aperture, for communicating with a fluid inlet and a fluid outlet, provided in at least one of the valve and cylinder, whereby the flow rate of a fluid may be continuously controlled and the collision between the valve and a valve seat may be avoided.
摘要翻译：电磁阀，其中脉冲信号被施加到其电磁体以消除电滞后。电磁阀包括可滑动地支撑在气缸中的活塞状阀以及设置在阀和气缸中的至少一个中的至少一个用于与流体入口和流体出口连通的孔，由此流体的流速可以连续地控制并且可以避免阀和阀座之间的碰撞。

7. 发明授权

US4474551A Combustion apparatus 失效
标题翻译：燃烧装置
公开(公告)号：US4474551A
公开(公告)日：1984-10-02
申请号：US381304
申请日：1982-05-24
申请人： Kazumi Iwai , Tadashi Shinozaki , Yoshio Okamoto , Hiroshi Inoue , Yoshifumi Kunugi , Shigeyuki Yamazaki
发明人： Kazumi Iwai , Tadashi Shinozaki , Yoshio Okamoto , Hiroshi Inoue , Yoshifumi Kunugi , Shigeyuki Yamazaki
IPC分类号： F23C6/04 , F23D15/00
CPC分类号： F23C6/04 , F23C2201/101
摘要： A combustion apparatus which includes tertiary air chambers are formed on both sides of a secondary combustion chamber, with tertiary air being supplied to a combustion flame produced within the secondary combustion chamber. The secondary combustion chamber has a flow channel width greater than a width of an opening in a throttle plate provided on the upstream side thereof, thereby achieving universality with respect to enabling use of various fuel and to increase the capacity of the combustion apparatus while reducing the size thereof.
摘要翻译：包括三次空气室的燃烧装置形成在二次燃烧室的两侧，三次空气被供给到二次燃烧室内产生的燃烧火焰。二次燃烧室具有大于设置在其上游侧的节流板的开口的宽度的流路宽度，从而实现了能够使用各种燃料的普遍性，并且在减少燃烧装置的同时增加燃烧装置的容量大小。

8. 发明授权

US08371125B2 Burner and gas turbine combustor 有权
标题翻译：燃烧器和燃气轮机燃烧器
公开(公告)号：US08371125B2
公开(公告)日：2013-02-12
申请号：US13365532
申请日：2012-02-03
申请人： Keisuke Miura , Hiroshi Inoue , Kazuhito Koyama , Takeo Saito , Satoshi Dodo
发明人： Keisuke Miura , Hiroshi Inoue , Kazuhito Koyama , Takeo Saito , Satoshi Dodo
IPC分类号： F02C1/00
CPC分类号： F23R3/286 , F23D2209/20 , F23R3/10 , F23R3/12 , F23R3/343 , F23R2900/00016 , F23R2900/03343
摘要： A burner is provided that has high flame stability and reduces NOx emissions. In the burner, air holes of an air hole member have a central axis inclined relative to a burner central axis. The leading end portion of a first fuel nozzle is configured to be able to suppress turbulence of air-flow flowing on the outer circumference side of the first fuel nozzle. The tip of the first fuel nozzle is located on a fuel jetting-out directional downstream side of the inlet of the fuel hole. The tip of the second fuel nozzle is located on a fuel jetting-out directional downstream side of the air hole inlet.
摘要翻译：提供了具有高火焰稳定性和减少NOx排放的燃烧器。在燃烧器中，气孔构件的气孔具有相对于燃烧器中心轴线倾斜的中心轴线。第一燃料喷嘴的前端部能够抑制在第一燃料喷嘴的外周侧流动的气流的紊流。第一燃料喷嘴的尖端位于燃料孔的入口的燃料喷出方向下游侧。第二燃料喷嘴的尖端位于空气孔入口的燃料喷射方向下游侧。

9. 发明授权

US08104284B2 Combustor and a fuel supply method for the combustor 有权
标题翻译：燃烧器和燃料供应方法
公开(公告)号：US08104284B2
公开(公告)日：2012-01-31
申请号：US12108162
申请日：2008-04-23
申请人： Keisuke Miura , Hiroshi Inoue , Kazuhito Koyama , Takeo Saito
发明人： Keisuke Miura , Hiroshi Inoue , Kazuhito Koyama , Takeo Saito
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23D14/64 , F23R3/12 , F23R3/20 , F23R3/286
摘要： A combustor includes a chamber mixing and burning fuel and air and an air hole plate disposed on a wall surface of the chamber. The, air hole plate includes a plurality of rows disposed concentrically of a plurality of air holes jetting coaxial jets of fuel and air into the chamber. A first fuel nozzle and a second fuel nozzle are disposed near a fuel hole for jetting fuel into an air hole row on an inner peripheral side. The first fuel nozzle is structured to suppress turbulence of a surrounding air flow and the second fuel nozzle is structured to promote turbulence of a surrounding air flow. In accordance with the aspect of the present invention, good flame stability can be maintained while further reducing NOx in a combustor using coaxial jets.
摘要翻译：燃烧器包括混合并燃烧燃料和空气的空间以及设置在室的壁表面上的气孔板。气孔板包括多个排列，其多个空气孔同时喷射同时喷射的燃料和空气进入腔室。第一燃料喷嘴和第二燃料喷嘴设置在用于将燃料喷射到内周侧的空气孔排的燃料孔附近。第一燃料喷嘴被构造成抑制周围气流的湍流，并且第二燃料喷嘴被构造成促进周围气流的紊流。根据本发明的方面，可以在使用同轴射流进一步减少燃烧器中的NOx的同时保持良好的火焰稳定性。

10. 发明申请

US20090293484A1 GAS TURBINE COMBUSTOR AND METHOD FOR SUPPLYING FUEL TO THE SAME 审中-公开
标题翻译：燃气轮机燃烧器及其燃料供应方法
公开(公告)号：US20090293484A1
公开(公告)日：2009-12-03
申请号：US11865126
申请日：2007-10-01
申请人： Hiroshi Inoue , Takeo Saito , Keisuke Miura , Kazuhito Koyama
发明人： Hiroshi Inoue , Takeo Saito , Keisuke Miura , Kazuhito Koyama
IPC分类号： F02C7/22
CPC分类号： F23R3/286
摘要： A fuel flow path and a flow path of air for combustion are disposed coaxially to create a coaxial jet such that a fuel flow is embraced by an air flow. A large number of such fuel flow paths and air flow paths are arranged in a wall surface of a combustion chamber to create coaxial nozzle jets. Some of the flow paths of air for combustion are arranged inclinedly so as to create rotation for the stabilization of combustion and straight portions not having an inclination angle are added respectively to upstream ends of such inclined air flow paths. Fuel is jetted toward or within the straight portions.
摘要翻译：燃料流路和用于燃烧的空气的流路同轴地设置以产生同轴喷嘴，使得燃料流被空气流包围。在燃烧室的壁面上布置有大量这样的燃料流路和空气流路，以产生同轴喷嘴。用于燃烧的空气的一些流动路径倾斜地布置，以便产生用于燃烧稳定的旋转，而不具有倾斜角的直线部分分别添加到这种倾斜空气流动路径的上游端。燃料朝着直线部分或内部喷射。

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