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

    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
    5.
    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

    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。

    Combustor for gas turbine
    8.
    发明授权
    Combustor for gas turbine 失效
    燃气轮机燃烧器

    公开(公告)号:US4598553A

    公开(公告)日:1986-07-08

    申请号:US375582

    申请日:1982-05-06

    CPC分类号: F23R3/14 F23R3/34

    摘要: A gas turbine combustor comprises an inner cylinder provided with louvers in an outer periphery thereof, defines a head combustion chamber and a main combustion chamber located downstream of and greater in diameter than the head combustion. An outer cylinder surrounds the inner cylinder and defines an air passage therebetween. A first burner communicates with the head combustion chamber and supplies air with gaseous fuel, and a second burner being disposed in the air passage near the head combustion chamber and supplying air and gaseous fuel into the main combustion chamber. The second burner is formed with a plurality of air inlets by a plurality of vanes which are disposed in an annular passage and which swirl the air, and with gaseous fuel jet ports near the inner peripheries of the air inlets. When the flow rate of the supplied fuel is small, the fuel flows along an inner-peripheral surface of the second burner, and when the flow rate is large, the fuel from the air inlets moves from the inner-peripheral surface toward the outer-peripheral surface of the second burner so as to be mixed well with the air supplied into the main combustion chamber. Thus, the production of NO.sub.x, CO, HC etc. can be decreased over the whole operating range of the turbine.

    摘要翻译: 燃气轮机燃烧器包括在其外周设置有百叶窗的内筒,限定头部燃烧室和主燃烧室,该主燃烧室和主燃烧室位于头部燃烧的直径以下。 外筒围绕内筒并在其间形成空气通道。 第一燃烧器与头部燃烧室连通并且向空气供应气体燃料,第二燃烧器设置在靠近头部燃烧室的空气通道中并将空气和气体燃料供应到主燃烧室中。 第二燃烧器由多个叶片形成有多个空气入口,多个叶片设置在环形通道中并使空气旋转,并且在空气入口的内周边附近具有气体燃料喷射口。 当供给的燃料的流量小时,燃料沿着第二燃烧器的内周面流动,并且当流量大时,来自空气入口的燃料从内周面朝向外侧面移动, 第二燃烧器的周面,以便与供给主燃烧室的空气充分混合。 因此,可以在涡轮机的整个工作范围内降低NOx,CO,HC等的生产。

    Low boiling point medium power plant
    10.
    发明授权
    Low boiling point medium power plant 失效
    低沸点中电厂

    公开(公告)号:US4262485A

    公开(公告)日:1981-04-21

    申请号:US964818

    申请日:1978-11-30

    CPC分类号: F01K25/10 F01K27/02

    摘要: A low boiling point medium power plant in which heated waste gas, such as furnace gas, geothermic steam, etc., is used as a heat source for heating an intermediate thermal medium by means of an indirect heat exchanger, and the intermediate thermal medium is used as a heat source for heating a turbine driving low boiling point medium by means of a direct heat exchanger. The indirect heat exchanger and the direct heat exchanger are rendered into a unitary structure and contained in a sealed housing together with a turbine, a generator and a condenser, whereby a compact overall size can be obtained in a low boiling point medium power plant.

    摘要翻译: 使用诸如炉煤气,地热蒸汽等的加热废气作为通过间接热交换器对中间热介质进行加热的热源的低沸点中电厂,中间热介质是 用作通过直接热交换器加热涡轮驱动低沸点介质的热源。 间接热交换器和直接热交换器被制成整体结构并与涡轮机,发电机和冷凝器一起容纳在密封壳体中,从而可以在低沸点中等动力装置中获得紧凑的整体尺寸。