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Fuel nozzle with discrete jet inner air swirler

机译:带离散射流内部空气旋流器的燃油喷嘴

摘要

A fuel nozzle includes an axial fuel circuit having a converging front surface with an axial fuel outlet formed therein, an air swirler surrounding the axial fuel circuit and having a converging front wall, a swirl chamber bounded by the converging front surface of the axial fuel circuit and the converging front wall of the air swirler, and an air cap surrounding the air swirler, such that an air circuit is defined between the air cap and the air swirler. A plurality of circumferentially disposed discrete jet passages extend through the converging front wall of the air swirler for directing atomizing air from the air circuit to the swirl chamber.
机译:燃料喷嘴包括:轴向燃料回路,其具有在其中形成有轴向燃料出口的会聚前表面;空气旋流器,其围绕轴向燃料回路并且具有会聚前壁;旋流室,其由轴向燃料回路的会聚前表面界定。空气旋流器的会聚前壁,以及围绕空气旋流器的空气帽,使得在空气帽和空气旋流器之间限定了空气回路。多个沿圆周布置的离散喷射通道延伸穿过空气旋流器的会聚前壁,以将雾化空气从空气回路引导至旋流室。

著录项

  • 公开/公告号US9284933B2

    专利类型

  • 公开/公告日2016-03-15

    原文格式PDF

  • 申请/专利权人 DELAVAN INC;

    申请/专利号US201313782969

  • 发明设计人 STEVEN JAY MYERS;

    申请日2013-03-01

  • 分类号F02M61/16;F23R3/14;F23R3/28;F23D11/10;F23D11/38;

  • 国家 US

  • 入库时间 2022-08-21 14:31:48

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