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    Gas turbine combustor
    2.
    发明授权
    Gas turbine combustor 有权
    燃气轮机燃烧器

    公开(公告)号：US06837051B2

    公开(公告)日：2005-01-04

    申请号：US10671472

    申请日：2003-09-29

    申请人： Shigemi Mandai ,  Kiyoshi Suenaga ,  Kuniaki Aoyama ,  Kazufumi Ikeda ,  Katsunori Tanaka

    发明人： Shigemi Mandai ,  Kiyoshi Suenaga ,  Kuniaki Aoyama ,  Kazufumi Ikeda ,  Katsunori Tanaka

    IPC分类号： F02C7/18 ,  F23M99/00 ,  F23R3/00 ,  F23R3/06 ,  F23R3/10 ,  F23R3/30 ,  F02C7/24

    CPC分类号： F23R3/06 ,  F23D2211/00 ,  F23M20/005 ,  F23R3/005 ,  F23R2900/00001 ,  F23R2900/00014

    摘要： A gas turbine combustor includes a side wall, for defining a combustion volume, having upstream and downstream ends, a pilot nozzle, disposed adjacent the upstream end of the side wall, for discharging a pilot fuel to form a diffusion flame in the combustion volume, and a plurality of main nozzles, provided around the pilot nozzles, for discharging a fuel-air mixture to form premixed flames in the combustion volume. Film air is supplied into the combustion volume downstream of the main nozzles along the inner surface of the side wall to reduce the fuel-air ratio in a region adjacent the inner surface of the side wall and to restrain a combustion-driven oscillation in the combustion volume.

    摘要翻译： 燃气轮机燃烧器包括用于限定具有上游和下游端的燃烧体积的侧壁，邻近侧壁的上游端设置的先导喷嘴，用于排放引燃燃料以在燃烧体积中形成扩散火焰， 以及设置在先导喷嘴周围的多个主喷嘴，用于排出燃料 - 空气混合物以在燃烧体积中形成预混合火焰。 薄膜空气沿着侧壁的内表面供应到主喷嘴下游的燃烧体积中，以减小邻近侧壁内表面的区域中的燃料空气比，并且抑制燃烧驱动的燃烧驱动 卷。

    Gas turbine combustor and a gas turbine equipped therewith
    3.
    发明授权
    Gas turbine combustor and a gas turbine equipped therewith 有权
    燃气轮机燃烧器和配备有燃气轮机的燃气轮机

    公开(公告)号：US07832211B2

    公开(公告)日：2010-11-16

    申请号：US10525004

    申请日：2003-11-28

    申请人： Kazufumi Ikeda ,  Shigemi Mandai ,  Yutaka Kawata ,  Kuniaki Aoyama ,  Masaki Ono ,  Katsunori Tanaka

    发明人： Kazufumi Ikeda ,  Shigemi Mandai ,  Yutaka Kawata ,  Kuniaki Aoyama ,  Masaki Ono ,  Katsunori Tanaka

    IPC分类号： F02C7/24 ,  F23M5/00

    CPC分类号： F23R3/04 ,  F05B2260/962 ,  F23M20/005 ,  F23R2900/00014 ,  Y02T50/675

    摘要： In order to realize a stable decrease in NOx, a gas turbine combustor is supplied which can reduce combustion vibration. A combustor (3) is provided with a first box body (30), which is installed outside an object body (20) such as a combustor basket (6), a transition piece (7) or a bypass duct (11) so as to form a first internal space (31) having a predetermined capacity; and a first throat (32) having a predetermined length which has one end (32a) open to a side wall (20a) of the object body (20) and has the other end (32b) open to a first internal space (31); wherein, a first resistive element (33) having a multiple number of through-holes is inserted and engaged to one end (32a). Fluid particles serving as vibration elements of combustion vibration caused in a combustion region are effectively trapped by the first resistive element (33) and at the same time resonate with the air of the first internal space (31) being connected through the first throat (32) and vibrate in the neighborhood of the first resistive element (33), thereby damping vibration amplitude thereof.

    摘要翻译： 为了实现NOx的稳定降低，提供能够减少燃烧振动的燃气轮机燃烧器。 燃烧器（3）设置有第一箱体（30），其安装在诸如燃烧器筐（6），过渡件（7）或旁通管道（11）的物体（20）的外部，以便 以形成具有预定容量的第一内部空间（31）; 以及具有一定长度的第一喉部（32），所述第一喉部（32）的一端（32a）朝向所述物体（20）的侧壁（20a）开口，并且另一端（32b）向第一内部空间（31）开放， ; 其中，具有多个通孔的第一电阻元件（33）被插入并接合到一端（32a）。 作为在燃烧区域中产生的燃烧振动的振动元件的流体颗粒被第一电阻元件（33）有效地捕获，同时与通过第一喉部（32）连接的第一内部空间（31）的空气共振 ）并且在第一电阻元件（33）附近振动，从而阻尼振动振幅。

    Gas turbine combustor, and gas turbine with the combustor
    4.
    发明申请
    Gas turbine combustor, and gas turbine with the combustor 有权
    燃气轮机燃烧器和燃气轮机

    公开(公告)号：US20050223707A1

    公开(公告)日：2005-10-13

    申请号：US10525004

    申请日：2003-11-28

    申请人： Kazufumi Ikeda ,  Shigemi Mandai ,  Yutaka Kawata ,  Kuniaki Aoyama ,  Masaki Ono ,  Katsunori Tanaka

    发明人： Kazufumi Ikeda ,  Shigemi Mandai ,  Yutaka Kawata ,  Kuniaki Aoyama ,  Masaki Ono ,  Katsunori Tanaka

    IPC分类号： F23M99/00 ,  F23R3/04 ,  F02C7/24

    CPC分类号： F23R3/04 ,  F05B2260/962 ,  F23M20/005 ,  F23R2900/00014 ,  Y02T50/675

    摘要： In order to realize a stable decrease in NOx, a gas turbine combustor is supplied which can reduce combustion vibration. A combustor (3) is provided with a first box body (30), which is installed outside an object body (20) such as a combustor basket (6), a transition piece (7) or a bypass duct (11) so as to form a first internal space (31) having a predetermined capacity; and a first throat (32) having a predetermined length which has one end (32a) open to a side wall (20a) of the object body (20) and has the other end (32b) open to a first internal space (31); wherein, a first resistive element (33) having a multiple number of through-holes is inserted and engaged to one end (32a). Fluid particles serving as vibration elements of combustion vibration caused in a combustion region are effectively trapped by the first resistive element (33) and at the same time resonate with the air of the first internal space (31) being connected through the first throat (32) and vibrate in the neighborhood of the first resistive element (33), thereby damping vibration amplitude thereof.

    摘要翻译： 为了实现NOx的稳定降低，提供能够减少燃烧振动的燃气轮机燃烧器。 燃烧器（3）设置有第一箱体（30），其安装在诸如燃烧器筐（6），过渡件（7）或旁通管道（11）的物体（20）的外部，以便 以形成具有预定容量的第一内部空间（31）; 以及具有预定长度的第一喉部（32），所述第一喉部（32）具有与所述物体（20）的侧壁（20a）相通的一端（32a），并且另一端（32b）向第一内部空间 （31）; 其中，具有多个通孔的第一电阻元件（33）插入并接合到一端（32a）。 作为在燃烧区域中产生的燃烧振动的振动元件的流体颗粒被第一电阻元件（33）有效地捕获，同时与通过第一喉部（32）连接的第一内部空间（31）的空气共振 ）并且在第一电阻元件（33）附近振动，从而阻尼振动振幅。

    Gas turbine combustor having bypass and annular gas passage for reducing uneven temperature distribution in combustor tail cross section
    9.
    发明授权
    Gas turbine combustor having bypass and annular gas passage for reducing uneven temperature distribution in combustor tail cross section 有权
    具有旁路和环形气体通道的燃气轮机燃烧器，用于减少燃烧器尾部截面中不均匀的温度分布

    公开(公告)号：US06860098B2

    公开(公告)日：2005-03-01

    申请号：US10098146

    申请日：2002-03-15

    申请人： Kiyoshi Suenaga ,  Shigemi Mandai ,  Katsunori Tanaka

    发明人： Kiyoshi Suenaga ,  Shigemi Mandai ,  Katsunori Tanaka

    IPC分类号： F02C7/18 ,  F23R3/04 ,  F23R3/06 ,  F23R3/26 ,  F23R3/42 ,  F02C9/00

    CPC分类号： F23R3/045 ,  F23R2900/00014

    摘要： There is provided a combustor to burn fuel, comprising a bypass passage connected to one side of the combustor to supply air into the combustor; and an annular passage provided around the combustor and connected to the bypass passage, wherein air supplied through the bypass passage passes in the annular passage in the circumferential direction, and is uniformly supplied into the combustor in the circumferential direction thereof through an opening which connects the combustor and the annular passage. Accordingly, compressed air passing through the bypass passage can be supplied uniformly into a tail portion of the combustor, and unevenness of temperature distribution in a cross section of the combustor tail portion can be reduced.

    摘要翻译： 提供燃烧燃料的燃烧器，包括连接到燃烧器的一侧以将空气供入燃烧器的旁路通道; 以及环形通道，设置在燃烧器周围并连接到旁通通道，其中通过旁通通道供应的空气在圆周方向上通过环形通道，并且通过一个开口均匀地供应到燃烧器的周向， 燃烧器和环形通道。 因此，能够将通过旁通路的压缩空气均匀地供给到燃烧器的尾部，能够减少燃烧器尾部的截面的温度分布的不均匀。