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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 220 having an upstream end (208 Fig 2), 222 and a downstream end 226 aligned about a central axis A. A discharge portion 228 is positioned adjacent the downstream end. A bore 240 extends inwardly from the downstream end over the length of the discharge portion. An opening 238 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 250 extends through the discharge portion between the bore and an outer surface 252 of the nozzle body. The fuel flow branch is fluidly coupled to a main fuel conduit 214 to provide a fuel flow passage. An outer air cap 270 is positioned about the outer surface of the discharge portion of the nozzle body to form an exterior air flow passage, and the interior air flow passage and the exterior airflow passage intersect near the downstream end of the nozzle body. The nozzle may include both an interior 242 and an outer 260 air swirler.
机译:提供一种喷嘴,该喷嘴包括喷嘴主体220,该喷嘴主体具有上游端(图2中的208),222和围绕中心轴线A对准的下游端226。排放部分228位于下游端附近。孔240从下游端向内延伸超过排出部分的长度。在喷嘴主体中邻近排放部分形成有开口238。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250延伸穿过孔和喷嘴主体的外表面252之间的排出部分。燃料流分支流体连接至主燃料导管214以提供燃料流通道。外部空气帽270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,并且内部空气流动通道和外部空气流动通道在喷嘴主体的下游端附近相交。喷嘴可包括内部空气旋流器242和外部空气旋流器260。

著录项

  • 公开/公告号GB2526416A

    专利类型

  • 公开/公告日2015-11-25

    原文格式PDF

  • 申请/专利权人 DELAVAN INC.;

    申请/专利号GB20150005181

  • 发明设计人 GREGORY ZINK;

    申请日2015-03-26

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

  • 国家 GB

  • 入库时间 2022-08-21 14:07:52

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