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Burner for gas turbine engines with at least one for the supply of combustion air as a function of the load adjustable swirl device

机译:用于燃气涡轮发动机的燃烧器,具有至少一个根据负载可调涡流装置提供燃烧空气供应的燃烧器

摘要

The combustor proposed has, located at the head end of the combustion chamber, at least one fuel-inlet nozzle (9) and at least one swirl device (7), which can be regulated as a function of the load, for the supply of combustion air, the swirl device having radial/tangential apertures (3) between the radial walls of an annular body disposed coaxially with the nozzle. Extending into these apertures are fingers (5) located round the end of a sleeve (4) which can be moved with respect to the annular body. The sleeve with its fingers is disposed so that it can be displaced longitudinally across the outside surface of the annular body, the fingers being angled with respect to the central combustor axis so that they are parallel to the longitudinally separated walls of the apertures and extending over the whole length of the apertures. The combustor proposed, optionally combined with at least one stationary swirl device (8), gives combustion with low polluant levels.
机译:所提出的燃烧器在燃烧室的头端处具有至少一个燃料入口喷嘴(9)和至少一个旋流装置(7),这些旋流装置可以根据负载进行调节,用于供给燃料。在燃烧空气中,旋流装置在与喷嘴同轴设置的环形体的径向壁之间具有径向/切向孔(3)。围绕套筒(4)的端部延伸的指状件(5)延伸到这些孔中,该指状件可以相对于环形体运动。带有指状物的套筒被布置成使得它可以在环形本体的外表面上纵向移动,指状物相对于燃烧器的中心轴线成一定角度,从而它们平行于孔的纵向分隔壁并且在其上延伸。孔的整个长度。提出的燃烧器,可选地与至少一个固定涡旋装置(8)结合,以低污染水平进行燃烧。

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