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Airblast nozzle with upstream fuel distribution and near-exit swirl

机译:带有上游燃料分配和近出口旋流的鼓风喷嘴

摘要

A nozzle is provided including a nozzle body having an upstream end and a downstream end aligned about a central axis. A discharge portion is positioned adjacent the downstream end. A bore extends inwardly from the downstream end over the length of the discharge portion. An opening is formed in the nozzle body adjacent the discharge portion. The opening is fluidly connected to the bore to provide an interior air flow passage. A main fuel channel extends from the upstream end to the discharge portion. At least one fuel flow branch extends through the discharge portion between the bore and an outer surface of the nozzle body. The fuel flow branch is fluidly coupled to the main fuel conduit to provide a fuel flow passage. The outer air cap is positioned about the outer surface of the discharge portion of the nozzle body to form an exterior air flow passage.
机译:提供一种喷嘴,该喷嘴包括喷嘴主体,该喷嘴主体具有绕中心轴线对准的上游端和下游端。排放部分位于下游端附近。孔从下游端在排出部分的长度上向内延伸。在喷嘴主体中靠近排放部分形成有开口。开口流体地连接到孔以提供内部空气流动通道。主燃料通道从上游端延伸到排放部分。至少一个燃料流分支延伸穿过孔和喷嘴主体的外表面之间的排出部分。燃料流分支流体连接至主燃料导管以提供燃料流通道。外部空气帽围绕喷嘴主体的排出部分的外表面定位以形成外部空气流动通道。

著录项

  • 公开/公告号US10295186B2

    专利类型

  • 公开/公告日2019-05-21

    原文格式PDF

  • 申请/专利权人 DELAVAN INC.;

    申请/专利号US201414228574

  • 发明设计人 GREGORY ZINK;

    申请日2014-03-28

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

  • 国家 US

  • 入库时间 2022-08-21 12:15:02

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