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    • 31. 发明授权
    • Combustor for gas turbine
    • 燃气轮机燃烧器
    • US4598553A
    • 1986-07-08
    • US375582
    • 1982-05-06
    • Isao SaitoYoji IshibashiTakashi OhmoriYoshimitsu MinakawaMichio Kuroda
    • Isao SaitoYoji IshibashiTakashi OhmoriYoshimitsu MinakawaMichio Kuroda
    • F23R3/14F23R3/28F23R3/30F23R3/34F02C1/00F02G3/00
    • F23R3/14F23R3/34
    • 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.
    • 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。