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Combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel

机译:预混合室和燃烧室的组合,污染物排放量低,适用于使用液体和/或气体燃料的燃气轮机

摘要

An improved combination (110) of a premixing chamber (112) and a combustion chamber (111), with low emission of pollutants, for gas turbines running on liquid and/or gas fuel, in which the combustion chamber (111) has a truncated conical end (111a) and is surrounded by a cavity (115) for cooling air (120), the cavity (115) carrying combustion air (120a) to the premixing chamber (112), which has at its inlet apertures or ports (126) which can be constricted according to the quantity of fuel used, and at its outlet a circumferential set of burners (134) to create a corresponding set of additional flames; gas fuel supply means (125) fuel and liquid fuel injection devices (119) are provided in the premixing chamber (112), and a set of liquid fuel injectors (140) is present on the end (111a).
机译:气体排放低的预混室( 112 )和燃烧室( 111 )的改进组合( 110 )以液体和/或气体燃料运行的涡轮机,燃烧室( 111 )的圆锥形末端( 111 a )截短,并且由用于冷却空气( 120 )的空腔( 115 )包围,该空腔( 115 )携带燃烧空气( 120 a )到预混合室( 112 ),该室的入口孔或端口( 126 )可以根据使用的燃料数量,以及在其出口处的圆周燃烧器( 134 )产生相应的一组附加火焰;气体燃料供应装置( 125 )燃料和液体燃料喷射装置( 119 )设置在预混合室( 112 )中,末端( 111 a )上有100个液体燃料喷射器( 140 )。

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