利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

114 条记录 (耗时 0.024 秒)

    Method of supplying fuel into gas turbine combustor
    1.
    发明授权
    Method of supplying fuel into gas turbine combustor 失效
    向燃气轮机燃烧器供应燃料的方法

    公开(公告)号：US4603548A

    公开(公告)日：1986-08-05

    申请号：US647658

    申请日：1984-09-06

    申请人： Yoji Ishibashi ,  Isao Sato ,  Fumio Kato ,  Takashi Ohmori ,  Noriyuki Hayashi

    发明人： Yoji Ishibashi ,  Isao Sato ,  Fumio Kato ,  Takashi Ohmori ,  Noriyuki Hayashi

    IPC分类号： F02C7/22 ,  F02C9/28 ,  F23N1/00 ,  F23R3/28 ,  F23R3/34 ,  F02C9/00

    CPC分类号： F23R3/346 ,  F02C7/22 ,  F23R3/28

    摘要： A fuel supply method for a gas turbine combustor having first and second stage combustion chambers. The method comprises supplying the fuel from only first stage fuel supply from the start of the gas turbine until its low output range so as to operate only the first stage combustion chamber, supplying the fuel from both first and second stage fuel supply in a high output range of the gas turbine including its maximum output so as to operate both first and second stage combustion chambers. The method makes it possible to reduce NO.sub.x without deteriorating the combustion performance by step-wise supplying a predetermined flow rate of the fuel when the second stage fuel is to be supplied and at the same time, step-wise reducing the same quantity of the fuel that is being supplied from the first stage fuel supply.

    摘要翻译： 一种具有第一和第二级燃烧室的燃气轮机燃烧器的燃料供给方法。 该方法包括仅将燃料从燃气轮机的起始点供给燃料，直到其低的输出范围，以便仅操作第一级燃烧室，从第一和第二级燃料供应源的燃料以高输出 包括其最大输出的燃气轮机的范围，以便操作第一和第二级燃烧室。 该方法可以在不降低燃烧性能的同时，通过在供给第二级燃料时逐步提供燃料的预定流量，同时逐步减少相同量的燃料 这是从第一级燃料供应提供的。

    Gas turbine combustor
    2.
    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
    3.
    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
    4.
    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 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。

    Premixing swirling burner
    9.
    发明授权
    Premixing swirling burner 失效
    预旋转燃烧器

    公开(公告)号：US4587809A

    公开(公告)日：1986-05-13

    申请号：US677244

    申请日：1984-12-03

    申请人： Takashi Ohmori ,  Isao Sato ,  Yoji Ishibashi ,  Yoshimitsu Minakawa ,  Michio Kuroda ,  Zensuke Tamura

    发明人： Takashi Ohmori ,  Isao Sato ,  Yoji Ishibashi ,  Yoshimitsu Minakawa ,  Michio Kuroda ,  Zensuke Tamura

    IPC分类号： F23D14/02 ,  B01F5/04 ,  F23C6/04 ,  F23C15/00 ,  F23C99/00 ,  F23D14/62 ,  F23D14/82 ,  F23R3/34 ,  F02C1/00 ,  F02G3/00

    CPC分类号： F23C15/00 ,  B01F5/0451 ,  F23C6/042 ,  F23D14/62 ,  F23D14/82 ,  F23R3/346

    摘要： A premixing swirling burner including a burner body having a swirling member at one end for causing fuel introduced into the burner body to flow in vortical form through the swirling member, a burner outer frame mounting the burner body and communicated with an air line for introducing air into the burner body, and a cylindrical member located in the burner outer frame for enclosing the burner body, with an air passage being defined between the inner periphery of the cylindrical member and an outer periphery of a portion of the burner body. A premixing chamber is defined between an outer periphery of a central portion of the burner body and an inner periphery of the cylindrical member for providing a fuel-air premix flowing toward the swirling member. A fuel chamber introduces fuel into the interior of the burner body, and a fuel ejection nozzle is located along an outer surface of the central portion of the burner body. A channel defined between the inner periphery of an end portion of the cylindrical member and an outer peripheral portion of the burner body formed an inlet for the premixing chamber has a cross-sectional area smaller than a cross-sectional area of the air passage.

    摘要翻译： 一种预混合旋转燃烧器，包括一端具有旋转构件的燃烧器主体，用于使引入燃烧器本体的燃料通过旋转构件以涡卷形式流动;燃烧器外框架，其安装燃烧器主体并与用于引入空气的空气管路连通 和位于燃烧器外框架中的圆筒形构件，用于封闭燃烧器主体，空气通道限定在圆柱形构件的内周和燃烧器本体的一部分外周之间。 在燃烧器主体的中心部分的外周和圆柱形部件的内周之间限定预混合室，用于提供朝向旋转部件流动的燃料 - 空气预混物。 燃料室将燃料引入燃烧器本体的内部，并且燃料喷射嘴位于燃烧器本体的中心部分的外表面。 形成在圆筒形构件的端部的内周和形成为预混合室的入口的燃烧器主体的外周部之间的通道的横截面积小于空气通道的横截面面积。