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A burner for the combustion chamber of a gas turbine power plant, a combustion chamber of a gas turbine power plant containing such a burner, and a gas turbine power plant containing such a combustion chamber

机译:用于燃气轮机电厂的燃烧室的燃烧器,包含这种燃烧器的燃气轮机电厂的燃烧室和具有这种燃烧室的燃气轮机电厂

摘要

A burner (30, 31) for a gas turbine power plant combustor (4), the burner (30, 31) having an axis (10) and comprising an inlet (32) fed by compressed air; an outlet (33) facing a combustion chamber (34); a lance (35) extending along the axis (10) and having a downstream portion (36) with a tip (37) substantially at the burner outlet (33); at least a fuel injector (38, 39) for injecting fuel in the air flow; an annular cavity (40) between at least the lance downstream portion (36) and a casing (41, 42); a swirl generator (43, 44) for generating in the annular cavity (40) an axial swirl of air or mixture air and fuel; wherein the burner (30, 31) further comprises at least a spark generator (45) at the lance tip (37).
机译:用于燃气轮机动力装置燃烧器(4)的燃烧器(30、31),该燃烧器(30、31)具有轴线(10)并且包括由压缩空气供给的入口(32);面对燃烧室(34)的出口(33);沿轴线(10)延伸的喷枪(35),其下游部分(36)具有基本上在燃烧器出口(33)处的尖端(37);至少一个燃料喷射器(38、39),用于在气流中喷射燃料;在至少喷枪下游部分(36)和壳体(41、42)之间的环形腔(40);涡流发生器(43、44),用于在环形腔(40)中产生空气或空气和燃料的混合物的轴向涡流;其中,燃烧器(30、31)在喷枪头(37)处进一步包括至少一个火花发生器(45)。

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