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1. 发明授权

US5038558A Gas turbine combustor and a method of combustion thereby 失效
标题翻译：燃气轮机燃烧器及其燃烧方法
公开(公告)号：US5038558A
公开(公告)日：1991-08-13
申请号：US292345
申请日：1988-12-30
申请人： Kenichi Sohma , Shigeru Azuhata , Yasuo Iwai , Tooru Inada , Hironobu Kobayashi , Kiyoshi Narato , Stephen M. Masutani , Tadayoshi Murakami , Norio Arashi , Yoji Ishibashi , Michio Kuroda
发明人： Kenichi Sohma , Shigeru Azuhata , Yasuo Iwai , Tooru Inada , Hironobu Kobayashi , Kiyoshi Narato , Stephen M. Masutani , Tadayoshi Murakami , Norio Arashi , Yoji Ishibashi , Michio Kuroda
IPC分类号： F23R3/12 , F23R3/30 , F23R3/34
CPC分类号： F23R3/34
摘要： A gas turbine combustor comprises a combustion chamber, a premixing chamber in which hydrocarbon fuel and air are premixed, a nozzle with swirler for swirling and injecting the premixed fuel and air into the combustion chamber, to effect premixed combustion, and a fuel nozzle projecting into the combustion chamber and adapted to inject fuel at region wherein the premixed combustion is completed, so as to effect low air-ratio diffusion combustion thereby to produce reducing substance. NOx produced by the premixed combustion is reduced by reducing reaction with the reducing substances, so that the NOx concentration in the combustion gas is reduced. The combustor further includes an after-air ports on a peripheral wall defining the combustion chamber to effect combustion of unburnt substances.

2. 发明授权

US5022849A Low NOx burning method and low NOx burner apparatus 失效
标题翻译：低NOx燃烧方法和低NOx燃烧装置
公开(公告)号：US5022849A
公开(公告)日：1991-06-11
申请号：US379926
申请日：1989-07-14
申请人： Yasuo Yoshii , Shigeru Azuhata , Norio Arashi , Kenichi Sohma , Tooru Inada , Hideo Kikuchi , Masayuki Taniguchi , Kiyoshi Narato , Hironobu Kobayashi , Tadayoshi Murakami , Michio Kuroda , Yoji Ishibashi , Stephen M. Masutani
发明人： Yasuo Yoshii , Shigeru Azuhata , Norio Arashi , Kenichi Sohma , Tooru Inada , Hideo Kikuchi , Masayuki Taniguchi , Kiyoshi Narato , Hironobu Kobayashi , Tadayoshi Murakami , Michio Kuroda , Yoji Ishibashi , Stephen M. Masutani
IPC分类号： F23C5/00 , F23C6/04 , F23C7/00 , F23C13/00 , F23D14/02
CPC分类号： F23C13/00 , F23C5/00 , F23C6/047 , F23C7/00 , F23D14/02 , F23C2900/05081
摘要： A low NOx burning method and apparatus wherein a low air ratio flame burned with an amount of air less than an amount of air in a theoretical air ratio required for burning fuel perfectly is formed, and combustibles discharged from the low air ratio flame are burned at a trailing stream of the low air ratio flame while supplying air. The low air ratio flame is a premixing flame burned by premixing the fuel and air, and combustion of the premixing flames is maintained in the vicinity of the premixing flame. In this way, the generation of the NOx during the burning can be greatly decreased, and the required apparatus can be small-sized.
摘要翻译：形成低NOx燃烧方法和装置，其中形成低空燃比火焰燃烧的空气量少于燃烧燃料所需的理论空气比的空气量，并且从低空燃比火焰排出的可燃物燃烧在在供应空气的同时，低空气比火焰的尾流。低空气比火焰是通过预混合燃料和空气燃烧的预混合火焰，并且预混合火焰的燃烧保持在预混合火焰附近。以这种方式，可以大大降低燃烧期间的NOx的产生，并且所需的装置可以小型化。

3. 发明授权

US5339635A Gas turbine combustor of the completely premixed combustion type 失效
标题翻译：完全预混合燃烧式的燃气轮机燃烧器
公开(公告)号：US5339635A
公开(公告)日：1994-08-23
申请号：US918799
申请日：1992-07-27
申请人： Yasuo Iwai , Shigeru Azuhata , Kenichi Sohma , Kiyoshi Narato , Hironobu Kobayashi , Tooru Inada , Tadayoshi Murakami , Norio Arashi , Yoji Ishibashi , Michio Kuroda
发明人： Yasuo Iwai , Shigeru Azuhata , Kenichi Sohma , Kiyoshi Narato , Hironobu Kobayashi , Tooru Inada , Tadayoshi Murakami , Norio Arashi , Yoji Ishibashi , Michio Kuroda
IPC分类号： F23D14/26 , F23D23/00 , F23R3/28 , F23R3/34
CPC分类号： F23D23/00 , F23D14/26 , F23R3/286 , F23R2900/03282
摘要： A gas turbine combustor of the pre-mixed combustion system in which the pre-mixed fuel and the air are combusted. The gas turbine combustor comprises main cylindrical nozzles provided in the end wall on the upstream side of a cylindrical combustion chamber, auxiliary nozzles formed to surround the main nozzles, a main pre-mixed gas supply for supplying a pre-mixed gas to the main nozzles, and an auxiliary pre-mixed gas supply for supplying a pre-mixed gas having an fuel/air ratio smaller than that of the main pre-mixed gas to the auxiliary nozzles, and wherein it is allowed to stably burn a lean pre-mixed gas having an fuel/air ratio of greater than 1 from a low-load condition through and up to a high-load condition of the gas turbine.
摘要翻译：预混合燃料系统的燃气轮机燃烧器，其中预混合燃料和空气燃烧。燃气轮机燃烧器包括设置在圆筒形燃烧室上游侧的端壁中的主圆柱形喷嘴，形成为围绕主喷嘴的辅助喷嘴，用于向主喷嘴供应预混合气体的主预混合气体供应以及辅助预混合气体供应源，用于将具有比主预混合气体的燃料/空气比小于预混合气体的预混合气体供应到辅助喷嘴，并且其中允许稳定地燃烧稀混合从低负荷状态通过燃气轮机的高负荷状态的燃料/空气比大于1的气体。

4. 发明授权

US5216885A Combustor for burning a premixed gas 失效
标题翻译：燃烧气体的燃烧器
公开(公告)号：US5216885A
公开(公告)日：1993-06-08
申请号：US495907
申请日：1990-03-20
申请人： Masayuki Taniguchi , Yasuo Yoshii , Tadayoshi Murakami , Shigeru Azuhata , Norio Arashi , Kenichi Sohma , Michio Kuroda , Hironobu Kobayashi , Yoji Ishibashi
发明人： Masayuki Taniguchi , Yasuo Yoshii , Tadayoshi Murakami , Shigeru Azuhata , Norio Arashi , Kenichi Sohma , Michio Kuroda , Hironobu Kobayashi , Yoji Ishibashi
IPC分类号： F23R3/26 , F01K23/10 , F23C6/04 , F23C7/00 , F23C9/00 , F23D14/70 , F23R3/02 , F23R3/18 , F23R3/30 , F23R3/34
CPC分类号： F23C9/006 , F01K23/10 , F23C6/047 , F23C7/00 , F23D14/70 , F23R3/02 , F23R3/346 , F23C2202/40 , F23D2209/20
摘要： Method of burning a premixed gas and a combustor for practicing the method. A jet of the premixed gas is burnt from an inside to an outside of the jet to form a premix flame. A burned gas is mixed into the premixed gas from the outside of the jet. The burned gas is produced when premixed gas is burned.

5. 发明授权

US5239831A Burner having one or more eddy generating devices 失效
标题翻译：燃烧器有一个或多个发电装置
公开(公告)号：US5239831A
公开(公告)日：1993-08-31
申请号：US727116
申请日：1991-07-09
申请人： Michio Kuroda , Nobuyuki Iizuka , Haruo Urushidani , Kazuhiko Kumata , Isao Sato , Tetsuo Sasada , Hajime Toriya , Yoshikazu Moritomo , Yoji Ishibashi , Takashi Ohmori , Shigeru Azuhata
发明人： Michio Kuroda , Nobuyuki Iizuka , Haruo Urushidani , Kazuhiko Kumata , Isao Sato , Tetsuo Sasada , Hajime Toriya , Yoshikazu Moritomo , Yoji Ishibashi , Takashi Ohmori , Shigeru Azuhata
IPC分类号： F23R3/12 , F23R3/16 , F23R3/30 , F23R3/34
CPC分类号： F23R3/343 , F23R3/16
摘要： A burner comprises at least one swirl member for mixing a fuel with an air previously to burning of the fuel, and at least one eddy generating device which is arranged in a flow of a mixture of the fuel and air to generate an eddy flow in the flow so that the eddy flow maintains a shape of a flame of the burned fuel. The at least one eddy generating device is arranged apart from a downstream end of the swirl member by a fixed sufficient distance so that the shape of the flame maintained by the eddy flow is prevented from moving toward the downstream end of the swirler member.

6. 发明授权

US4898001A Gas turbine combustor 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US4898001A
公开(公告)日：1990-02-06
申请号：US144646
申请日：1988-01-11
申请人： Michio Kuroda , Isao Sato , Yoji Ishibashi , Yoshihiro Uchiyama , Takashi Ohmori , Shigeyuki Akatsu , Fumio Kato , Yorihide Segawa , Nobuyuki Iizuka
发明人： Michio Kuroda , Isao Sato , Yoji Ishibashi , Yoshihiro Uchiyama , Takashi Ohmori , Shigeyuki Akatsu , Fumio Kato , Yorihide Segawa , Nobuyuki Iizuka
IPC分类号： F23R3/04 , F23R3/28 , F23R3/34 , F23R3/44
CPC分类号： F23R3/44 , F23R3/04 , F23R3/28 , F23R3/346
摘要： A gas turbine combustor for reducing a production of NOx. The combustor includes a head combustion chamber and a rear combustion chamber which is larger in diameter than the head combustion chamber. The head combustion chamber is provided with an axially extending hollow frustoconical tubular member to form an annular combustion space therein, air holes for axially jetting air into the annular combustion chamber, air holes formed on a peripheral wall for injecting air and a plurality of fuel nozzles projected into the annular combustion space for injecting fuel into vortex formed by the air jet and the injected air flow whereby the flame is stabilized and lean combustion can be effected. The rear combustion chamber has a fuel and air supply means on the upstream side which includes air inlets formed by whirling vanes and fuel nozzles disposed in the air inlets so that fuel and air are mixed well. The fuel and air mixture is jetted substantially axially while whirling it so that formation of hot spots is avoided and the NOx formation is extremely limited.
摘要翻译：一种用于减少NOx生产的燃气轮机燃烧器。燃烧器包括头部燃烧室和直径大于头部燃烧室的后部燃烧室。头部燃烧室设置有轴向延伸的中空截头圆锥形管状构件以在其中形成环形燃烧空间，用于将空气轴向地喷射到环形燃烧室中的气孔，形成在用于喷射空气的周壁上的气孔和多个燃料喷嘴投射到环形燃烧空间中，用于将燃料喷射到由空气射流和喷射空气流形成的涡流中，从而使火焰稳定并且可以实现贫燃。后燃烧室在上游侧具有燃料和空气供给装置，其包括由旋转叶片形成的空气入口和设置在空气入口中的燃料喷嘴，使得燃料和空气充分混合。燃料和空气混合物在旋转时基本上轴向地喷射，从而避免形成热点并且非常限制NOx的形成。

7. 发明授权

US5121597A Gas turbine combustor and methodd of operating the same 失效
标题翻译：燃气轮机及其运行方法
公开(公告)号：US5121597A
公开(公告)日：1992-06-16
申请号：US470596
申请日：1990-01-26
申请人： Haruo Urushidani , Seiichi Kirikami , Isao Sato , Nobuo Shimizu , Osamu Arai , Akira Shimura , Michio Kuroda , Tsuguaki Koga , Tadashi Kurokawa , Yoji Ishibashi , Katsukuni Hisano
发明人： Haruo Urushidani , Seiichi Kirikami , Isao Sato , Nobuo Shimizu , Osamu Arai , Akira Shimura , Michio Kuroda , Tsuguaki Koga , Tadashi Kurokawa , Yoji Ishibashi , Katsukuni Hisano
IPC分类号： F02C7/26 , F02C9/34 , F23C99/00 , F23R3/16 , F23R3/20 , F23R3/26 , F23R3/34
CPC分类号： F02C9/34 , F02C7/26 , F23R3/16 , F23R3/26 , F23R3/34 , F05D2270/31
摘要： A gas turbine combustor and a method of operating the gas turbine combustor, with the gas turbine combustor comprising a combustion sleeve, a combustion sub-chamber disposed at an upstream side of the combustion sleeve and having an air and fuel supply system, and a combustion main chamber disposed on a downstream side of the sub-chamber and having an air and fuel supply system. The combustion sub-chamber and combustion main chamber are formed in such a manner that the start-up of the gas turbine is effected by the hot combustion gas generated in the sub-chamber. The combustion sub-chamber is provided with an inner sleeve protruding from a side wall of the sub-chamber such that a tip of the inner sleeve is located in the vicinity of a downstream end of the sub-chamber, and a fuel nozzle is provided in a tip of the inner sleeve for increasing the fuel-to-air ratio during an initiating period of an increase in the gas turbine rotation speed.

8. 发明授权

US4766721A Combustor for gas turbine 失效
标题翻译：燃气轮机燃烧器
公开(公告)号：US4766721A
公开(公告)日：1988-08-30
申请号：US917973
申请日：1986-10-14
申请人： Nobuyuki Iizuka , Yoji Ishibashi , Isao Sato , Fumiyuki Hirose , Hiroshi Inose , Katsukuni Hisano , Katsuo Wada , Seiichi Kirikami , Michio Kuroda , Yoshihiro Uchiyama
发明人： Nobuyuki Iizuka , Yoji Ishibashi , Isao Sato , Fumiyuki Hirose , Hiroshi Inose , Katsukuni Hisano , Katsuo Wada , Seiichi Kirikami , Michio Kuroda , Yoshihiro Uchiyama
IPC分类号： F23R3/00 , F02C9/18 , F23R3/04 , F23R3/26 , F23R3/28 , F23R3/34
CPC分类号： F23R3/34 , F02C9/18 , F23R3/26 , F05D2270/31
摘要： A combustor of two-stage combustion type in which fuel is supplied only from primary fuel nozzles for combustion only in primary combustion chamber under the operating condition where gas turbine load is low, and premixed mixture is supplied into a secondary combustion chamber provided on the downstream side of the primary combustion chamber for combustion in both the primary and secondary combustion chambers under the operating condition where the load is high. An air-bleed passageway opens on a downstream side of air holes for intaking secondary combustion air to be mixed with secondary fuel and communicates with the outside of the combustor. The air-bleed passageway is provided with a regulating valve and the secondary combustion air is bled at the minimum point of the load where the secondary fuel is supplied so that the fuel to air ratio of secondary premixed mixture may not be excessively lean, thereby reducing the production of non-burned components.
摘要翻译：一种二级燃烧式的燃烧器，其中，在燃气轮机负荷低的运行条件下，燃料仅从主燃料喷嘴供给燃料，仅在一级燃烧室中燃烧，并且将预混合物供给到设置在下游的二次燃烧室在一次燃烧室中，在负载高的运行条件下在一次燃烧室和二次燃烧室中燃烧。排气通道在气孔的下游侧开口，用于吸入与二次燃料混合的二次燃烧空气并与燃烧器的外部连通。排气通道设置有调节阀，二次燃烧空气在供给二次燃料的负载的最小点处排出，使得二次预混混合物的燃料与空气的比例可能不会过度减少，从而减少生产非烧成分。

9. 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。

10. 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.

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