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12 条记录 (耗时 0.011 秒)

    Gas turbine combustor
    3.
    发明公开
    Gas turbine combustor 审中-公开

    公开(公告)号：EP2423600A3

    公开(公告)日：2017-10-25

    申请号：EP11177195.2

    申请日：2011-08-11

    申请人： Mitsubishi Hitachi Power Systems, Ltd.

    发明人： Hirata, Yoshitaka ,  Yoshida, Shohei ,  Sekiguchi, Tatsuya ,  Hayashi, Akinori

    IPC分类号： F23R3/48 ,  F23R3/34 ,  F23R3/28

    CPC分类号： F23R3/48 ,  F23D2207/00 ,  F23R3/286 ,  F23R3/343

    摘要： In a gas turbine combustor, mixing of a fuel and air is accelerated in a mixing chamber of a burner as well as in air introduction passages provided in a wall of the mixing chamber, whereby NOx emissions from premixed combustion are reduced while at the same time, ignition characteristics and flame propagation characteristics improve.
    The gas turbine combustor includes a plurality of combustors 10, a spark plug 13, and a cross-fire tube 15 that propagates a flame between the combustors 10. Each combustor 10 includes the burner 30 equipped with a fuel nozzle and the mixing chamber wall 32 forming the mixing chamber 31. A plurality of air introduction holes 35, 36 for introducing combustion air, along with the fuel from the fuel nozzle, into the mixing chamber 31, are provided in the mixing chamber wall 32. The combustion air and fuel jetted from the air introduction hole 35 into the mixing chamber 31 are mixed in the form of a mixture "m1" , "m2" and directed towards the spark plug 13 and the cross-fire tube 15.

    Method and apparatus for controlling gas turbine combustor
    5.
    发明公开
    Method and apparatus for controlling gas turbine combustor 审中-公开
    控制燃气轮机燃烧室的方法和设备

    公开(公告)号：EP2426339A3

    公开(公告)日：2018-04-18

    申请号：EP11178227.2

    申请日：2011-08-22

    申请人： Mitsubishi Hitachi Power Systems, Ltd.

    发明人： Sekiguchi, Tatsuya ,  Yoshida, Shouhei ,  Hirata, Yoshitaka ,  Hayashi, Akinori ,  Saitou, Nozomi ,  Takahashi, Kazuo ,  Saitou, Takeo

    IPC分类号： F02C9/26 ,  F02C9/34

    CPC分类号： F02C9/263 ,  F02C9/28 ,  F02C9/34 ,  F02C9/46 ,  F05D2270/082 ,  F05D2270/091 ,  F05D2270/304 ,  F05D2270/309 ,  F05D2270/31 ,  F05D2270/331 ,  F23N1/002 ,  F23N2041/20

    摘要： An apparatus for controlling a gas turbine combustor having a diffusion combustion burner and a premix combustion burner comprising: a rotating speed detector for detecting a rotating speed of gas turbine, a recorder for recording the detected value of the rotating speed of gas turbine detected by the rotating speed detector, an arithmetic unit for calculating a change with time of the rotating speed of gas turbine in accordance with details of the detected value of the rotating speed of gas turbine recorded in the recorder, and a fuel control unit for judging a starting situation of reduction in the rotating speed of gas turbine on the basis of the change with time of the rotating speed of gas turbine calculated by the arithmetic unit and controlling respectively a fuel flow rate for the diffusion combustion burner to be fed to the diffusion combustion burner installed in the gas turbine combustor and a fuel flow rate for the premix combustion to be fed to the premix combustion burner.

    摘要翻译： 一种用于控制具有扩散燃烧器和预混合燃烧器的燃气轮机燃烧器的设备，该设备包括：转速检测器，用于检测燃气轮机的转速;记录器，用于记录由燃气轮机检测到的燃气轮机的转速的检测值 转速检测器，用于根据记录在记录器中的燃气轮机的转速的检测值的细节计算燃气轮机的转速随时间的变化的运算单元以及用于判断启动情况的燃料控制单元 根据由运算装置计算出的燃气轮机转速随时间的变化，分别控制燃气轮机转速的降低，并分别控制供给扩散燃烧器的燃料流量， 在燃气轮机燃烧器中的燃料流量和用于预混燃烧的燃料流量被供给到预混燃烧器 。

    Combustor
    7.
    发明公开
    Combustor 审中-公开
    燃烧室

    公开(公告)号：EP2525149A3

    公开(公告)日：2017-12-20

    申请号：EP12168521.8

    申请日：2012-05-18

    申请人： Mitsubishi Hitachi Power Systems, Ltd.

    发明人： Hirata, Yoshitaka ,  Yoshida, Shohei ,  Sekiguchi, Tatsuya ,  Hayashi, Akinori ,  Takahashi, Hirokazu

    IPC分类号： F23D11/40 ,  F23D14/62 ,  F23R3/04 ,  F23R3/12 ,  F23R3/28 ,  F23R3/36 ,  F23C7/00

    摘要： A highly-reliable combustor is provided that allows flash back of flame into a premixer to be suppressed.
    The combustor has a mixing chamber forming member 110 that forms a mixing chamber thereinside. The mixing chamber includes a first mixing chamber 200 broadening toward a downstream side. The member 110 includes air introduction holes 202, 203, 204 formed in a plurality of rows in an axial direction, with the air introduction holes being arranged plurally in a circumferential direction of the mixing chamber. The member 110 includes a fuel ejection hole 206 provided in a wall surface which forms the air introduction hole. The air introduction holes 202, 203, 204 are circumferentially eccentrically installed. The air introduction holes 202 located in the most upstream row are more inclined toward the downstream side than the air introduction holes 203, 204 located in the rows other than the most upstream row.

    摘要翻译： 提供高度可靠的燃烧器，允许火焰闪回到预混器中被抑制。 燃烧器具有在其内部形成混合室的混合室形成构件110。 混合室包括朝下游侧扩宽的第一混合室200。 构件110包括在轴向方向上形成为多行的空气引入孔202,203,204，空气引入孔沿混合室的圆周方向布置多个。 构件110包括设置在形成空气引入孔的壁表面中的燃料喷射孔206。 空气引入孔202,203,204沿圆周偏心安装。 位于最上游列的空气导入孔202比位于最上游列以外的列的空气导入孔203,204向下游侧倾斜。

    GAS TURBINE COMBINED CYCLE SYSTEM EQUIPPED WITH CONTROL DEVICE AND ITS CONTROL METHOD
    10.
    发明公开
    GAS TURBINE COMBINED CYCLE SYSTEM EQUIPPED WITH CONTROL DEVICE AND ITS CONTROL METHOD 审中-公开

    公开(公告)号：EP3450705A1

    公开(公告)日：2019-03-06

    申请号：EP18187055.1

    申请日：2018-08-02

    申请人： Mitsubishi Hitachi Power Systems, Ltd.

    发明人： Sekiguchi, Tatsuya

    IPC分类号： F01K23/10

    摘要： In addition to a first fuel gas heater (6) utilizing the heated water from the outlet of an economizer (10) of a heat recovery steam boiler (8), there is provided a second fuel gas heater (7) utilizing as the heat source the bleed air of a compressor (2) of a gas turbine (1). A control device (30) opens a bleed air control valve (17) of the piping (204) for supplying bleed air to the second fuel gas heater (7) at the time of starting the gas turbine combined cycle system (1000) to heat a fuel gas by the bleed air.