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    Gas turbine combustor
    1.
    发明授权
    Gas turbine combustor 失效
    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。

    Gas turbine combustor and method of running the same
    2.
    发明授权
    Gas turbine combustor and method of running the same 失效
    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。

    Combustor and method of operating same
    3.
    发明授权
    Combustor and method of operating same 失效
    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.

    Combustor for gas turbine
    5.
    发明授权
    Combustor for gas turbine 失效
    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。

    Combustor for a gas turbine
    6.
    发明授权
    Combustor for a gas turbine 失效
    燃气轮机用燃烧器

    公开(公告)号：US5081843A

    公开(公告)日：1992-01-21

    申请号：US423749

    申请日：1989-10-19

    申请人： Yoji Ishibashi ,  Takashi Ohmori ,  Fumio Kato ,  Michio Kuroda ,  Nobuyuki Iizuka

    发明人： Yoji Ishibashi ,  Takashi Ohmori ,  Fumio Kato ,  Michio Kuroda ,  Nobuyuki Iizuka

    IPC分类号： F23R3/04 ,  F23C99/00 ,  F23R3/26 ,  F23R3/34

    CPC分类号： F23R3/34 ,  F23R3/26 ,  F05D2270/31

    摘要： A combustor for driving a gas turbine includes a first burning stage and a second burning stage. The combustor further comprises a primary combustion chamber in which air from the associated compressor and fuel are burnt, a pre-mixing chamber in which air from the associated compressor and fuel are pre-mixed, a main combustion chamber in which fuel/air mixture is burnt and forwarded to the gas turbine, an air passage provided in a wall of the main combustion chamber, through which air from the compressor flows to cool the wall thereof, and an intercommunicating air passage for intercommunicating the air passage to the pre-mixing chamber, whereby cooling air for the main combustion chamber wall is used to supplement the air in the pre-mixing chamber.

    摘要翻译： 用于驱动燃气轮机的燃烧器包括第一燃烧阶段和第二燃烧阶段。 燃烧器还包括主燃烧室，其中来自相关联的压缩机和燃料的空气被燃烧，预混合室，其中来自相关联的压缩机和燃料的空气被预混合，主燃烧室，其中燃料/空气混合物是 燃烧并传送到燃气轮机，设置在主燃烧室的壁中的空气通道，来自压缩机的空气通过该空气流动以冷却其壁;以及相互连通的空气通道，用于将空气通道相互连通到预混合室 ，由此用于主燃烧室壁的冷却空气用于补充预混合室中的空气。

    Method of starting gas turbine plant
    7.
    发明授权
    Method of starting gas turbine plant 失效
    启动燃气轮机厂的方法

    公开(公告)号：US4683715A

    公开(公告)日：1987-08-04

    申请号：US807945

    申请日：1985-12-12

    申请人： Nobuyuki Iizuka ,  Katsukuni Hisano ,  Ryoichiro Oshima ,  Katsuo Wada ,  Fumiyuki Hirose ,  Michio Kuroda ,  Yoshihiro Uchiyama ,  Yoji Ishibashi ,  Isao Sato ,  Hiroshi Inose

    发明人： Nobuyuki Iizuka ,  Katsukuni Hisano ,  Ryoichiro Oshima ,  Katsuo Wada ,  Fumiyuki Hirose ,  Michio Kuroda ,  Yoshihiro Uchiyama ,  Yoji Ishibashi ,  Isao Sato ,  Hiroshi Inose

    IPC分类号： F01K23/10 ,  F02C7/26 ,  F02C9/18 ,  F02C9/28 ,  F02C9/52 ,  F23R3/26 ,  F23R3/34

    CPC分类号： F23R3/26 ,  F02C7/26 ,  F02C9/18 ,  F23R3/34 ,  F05D2270/31 ,  Y02E20/16

    摘要： A method of starting a gas turbine plant, which plant has at least one combustor including a primary combustion chamber into which primary fuel nozzles open and a secondary combustion chamber into which secondary fuel nozzles open, a compressor for supplying the combustor with compressed combustion air, and a gas turbine driven by the combustion gas generated in the combustor and adapted to drive a load such as an electric power generator. When the gas turbine is being accelerated to a rated speed or while the load is still below a normal load range, a fuel is supplied only to the primary fuel nozzle, whereas, in other loaded operation range, the fuel is supplied to both the primary and secondary fuel nozzles. Before the fuel supply to the secondary fuel nozzles is commenced, a part of the compressed air is bled through at least one air bleed pipe leading from the compressor and having an air bleed valve. The air bleed valve is controlled in such a manner that the opening degree thereof is maximized when the fuel supply to the secondary fuel nozzles is commenced and is progressively decreased in accordance with the increase of the load such as to become substantially zero when the load has been increased to the normal load range.

    摘要翻译： 一种启动燃气轮机设备的方法，该设备具有至少一个燃烧器，该燃烧器包括初级燃料喷嘴打开的初级燃烧室和次级燃料喷嘴打开的二级燃烧室，用于向燃烧室供应压缩的燃烧空气的压缩机， 以及由在燃烧器中产生的燃烧气体驱动并适于驱动诸如发电机的负载的燃气轮机。 当燃气轮机正在加速到额定转速或负载仍然低于正常负载范围时，仅向主燃料喷嘴供应燃料，而在其他装载操作范围内，将燃料供应给主燃料 和二次燃料喷嘴。 在开始向二次燃料喷嘴供应燃料之前，一部分压缩空气通过至少一个从压缩机引出的排气管排出并具有排气阀。 控制排气阀，使得当向二次燃料喷嘴供应的燃料开始时，其开度最大化，并且随着负载的增加逐渐减小，当负载已经变为基本为零时 增加到正常负载范围。