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U-tube diffusion flame burner assembly having unique flame stabilization

机译:具有独特火焰稳定性的U型管扩散式火焰燃烧器组件

摘要

A U-tube diffusion flame burner assembly having improved flame stabilization with no undesirable acoustic effects. The burners are axial units comprised of flame holders and combustors. The flame holders includes secondary air tubes to support the flow of secondary air that have helical walls forming helical passageways along at least a portion of its inner diameter to impart a swirl to the secondary air. The helical passageways impart a swirl to the secondary air exiting the passageways while simultaneously acting as a heat exchanger to heat primary air. The flame holders includes fuel tubes having first ends connected to a fuel supply and second flame ends. A plurality of radially oriented apertures are located at the second flame ends to distribute fuel in a radial direction. Primary air tube surrounds at least the flame ends of the fuel tubes and extend axially from first air supply ends to second flame ends. Air is diverted from air supply ends of the flame burners into primary air tubes through radial apertures located at the first air supply ends of the primary air tubes. Secondary air tubes surround the primary air tubes extending from first air supply ends to second ends opposite the air supply, the secondary air tubes having inner diameters larger than the outer diameters of the primary air tubes. The secondary air tubes extend for a preselected distance beyond the second flame ends of the primary air tubes and are coupled to axially-oriented conical-shaped reducers. Flame at high velocity exits the restricted end of the reducers.
机译:一种U形扩散火焰燃烧器组件,具有改进的火焰稳定性,而没有不希望的声音效果。燃烧器是由火焰保持器和燃烧器组成的轴向单元。火焰保持器包括用于支撑二次空气流的二次空气管,二次空气管具有螺旋壁,该螺旋壁沿着其内径的至少一部分形成螺旋通道,以向二次空气赋予漩涡。螺旋通道将涡旋赋予离开通道的二次空气,同时充当热交换器以加热一次空气。火焰保持器包括燃料管,该燃料管的第一端连接到燃料供应,第二火焰端。多个径向定向的孔位于第二火焰端,以沿径向分配燃料。初级空气管至少围绕燃料管的火焰端,并从第一空气供给端轴向延伸到第二火焰端。空气通过位于主空气管第一供气端的径向孔从火焰燃烧器的空气供给端转移到主空气管中。次级空气管围绕从第一空气供给端延伸到与空气供给相对的第二端的初级空气管,次级空气管的内径大于初级空气管的外径。次级空气管延伸超过初级空气管的第二火焰端的预定距离,并连接到轴向圆锥形的异径管。高速火焰离开减速器的限制端。

著录项

  • 公开/公告号US6872070B2

    专利类型

  • 公开/公告日2005-03-29

    原文格式PDF

  • 申请/专利权人 EDWARD E. MOORE;JOHN A. MARINO;

    申请/专利号US20020301329

  • 发明设计人 EDWARD E. MOORE;JOHN A. MARINO;

    申请日2002-11-21

  • 分类号F23M3/04;F23M9/00;

  • 国家 US

  • 入库时间 2022-08-21 22:20:12

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