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    • 2. 发明申请
    • Gas Turbine Combustor
    • 燃气轮机燃烧器
    • US20120192568A1
    • 2012-08-02
    • US13358227
    • 2012-01-25
    • Keisuke MIURATomomi KoganezawaSatoshi DodoTakeo Saito
    • Keisuke MIURATomomi KoganezawaSatoshi DodoTakeo Saito
    • F02C7/22F23R3/26
    • F23R3/286F23R3/343F23R2900/00014
    • A combustor of the prior art that defines the outlet position and direction of an air hole and suppresses adhesion of flame to an air hole outlet can reduce a discharge amount of NOx by increasing a distance over which fuel and air are mixed with each other. However, such a combustor is not sufficiently discussed for measures to suppress the occurrence of combustion oscillation resulting from the variation of a flame surface.A combustor 2 according to the present invention includes a combustion chamber 5 to which fuel and air are supplied; air holes 32 adapted to supply air to the combustion chamber 5; fuel nozzles 25 adapted to supply gaseous fuel to the air holes 32; and orifices 24 adapted to allow the gaseous fuel supplied to the air holes 32 to cause a pressure drop.
    • 限定空气孔的出口位置和方向并且抑制火焰与空气孔出口的粘附的现有技术的燃烧器可以通过增加燃料和空气彼此混合的距离来减少NOx的排放量。 但是,为了抑制由火焰表面的变化引起的燃烧振动的发生的措施,这种燃烧器没有充分的讨论。 根据本发明的燃烧器2包括供应燃料和空气的燃烧室5; 适于向燃烧室5供应空气的气孔32; 适于向气孔32供应气体燃料的燃料喷嘴25; 以及适于允许供应到气孔32的气体燃料引起压降的孔口24。