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Oil burner turbulator end cone, and method for generating counter-rotating air flow patterns

机译:燃油燃烧器涡轮锥和产生反向旋转气流模式的方法

摘要

A gun type oil burner tip having a series of orifices or nozzles annularly arranged in pairs on the end of the gun in such manner that each nozzle pair projects an air stream, the respective nozzles in each pair being in close juxtaposition such that the projected air streams cross or intersect each other immediately forward of the nozzle such as to intertwine and define an expanding, rotating cone of gases comprised of discrete swirling streams having turbulent areas there between.
机译:一种枪式喷油嘴,具有一系列在枪的末端成对环形排列的孔口或喷嘴,使得每个喷嘴对喷射出一股空气流,每对中的各个喷嘴紧密并列,以使喷射出的空气气流在喷嘴的正前方彼此交叉或相交,以便相互缠绕并限定一个膨胀的旋转圆锥体,该圆锥体由离散的涡流组成,在它们之间具有湍流区域。

著录项

  • 公开/公告号US3923251A

    专利类型

  • 公开/公告日1975-12-02

    原文格式PDF

  • 申请/专利权人 TEXACO INC.;

    申请/专利号US19720311199

  • 发明设计人 FLOURNOY;NORMAN E.;

    申请日1972-12-01

  • 分类号B05B7/10;F23D11/16;

  • 国家 US

  • 入库时间 2022-08-23 01:38:31

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