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Stages combustion chamber, whose full load burner also contain empty running burner

机译:分级燃烧室,其满负荷燃烧器还包含空运行的燃烧器

摘要

The invention relates to an annular combustion chamber comprising the axial walls (1, 2) connected by a bottom of chamber (3) and a plurality of fuel injectors placed in holes (4) passing through the bottom of chamber (3), said injectors being distributed on a pilot head (20) and on a high power head are radially spaced apart from the pilot head (20), the said combustion chamber having a general direction (11) of the gas flow. The pilot head (20) is fitted with n nozzles of idling, in the permeability p1, adapted to the idling speeds. The take-off head is equipped, in alternation, of low power injectors of permeability p1, adapted to the idling speed, and n take-off nozzles of permeability p2 p1, adapted to the state of full load. According to a view of the bottom of the chamber (3) from the inside of the combustion chamber, parallel to said direction of flow (11), the fuel injectors of permeability p1 of the pilot head (20) and of the high power head are disposed substantially in a staggered configuration.
机译:本发明涉及一种环形燃烧室,该环形燃烧室包括通过室(3)的底部连接的轴向壁(1、2)和放置在穿过室(3)的底部的孔(4)中的多个燃料喷射器,所述喷射器分布在引燃头(20)和大功率扬尘头上的空气与引燃头(20)在径向上间隔开,所述燃烧室具有气流的大体方向(11)。导向头(20)在磁导率p1中装有n个空转喷嘴,它们适合于空转速度。取放头交替装有适应空转速度的低渗透率p1小功率喷油嘴,以及适应满载状态的n个渗透率p2> p1的取油嘴。根据燃烧室内部的腔室(3)的底部的视图,平行于所述流动方向(11),先导头(20)和大功率头的渗透率p1的燃料喷射器基本上以交错配置布置。

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