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Burner for liquid or gaseous fuel - uses air velocity and swirl to slow combustion and lower peak temp. and minimise nitrous oxides

机译:用于液体或气体燃料的燃烧器-利用空气速度和涡流来减慢燃烧速度并降低峰值温度。并尽量减少一氧化二氮

摘要

The burner for liquid or gaseous fuels comprises an axial fuel pipe (1) surrounded for part of its length by a coaxial cylindrical casing (2) closed at one end and containing an air swirler (4) with blades set at between 45 and 75 to the axis. The swirler may be fixed or free to rotate. Air enters the casing at the side and leaves via a flanged conical extension (5) on the furnace front. In this conical portion the flow area is reduced by between 40 and 80%. The swirled air is thus accelerated before it enters the furnace through a cylindrical duct (7). The air exit velocity is between 20 and 60 m/sec and in any case greater than the flame propagation speed with the fuel in question. The end of the fuel pipe should be between 0.1 and 4.0 (pref. 0.5-1.0) air duct dias. upstream of the duct end. In combination these measures slow down the initial combustion rate, flatten the combustion temp. curve and reduce its peak value. This in turn inhibits the formation of oxides of nitrogen.
机译:用于液体或气体燃料的燃烧器包括轴向燃料管(1),该燃料管的一部分长度被同轴的圆柱形外壳(2)围绕,该同轴的圆柱形外壳的一端封闭,并包含旋流器(4),其叶片设置在45至75之间,轴。旋流器可以固定或自由旋转。空气从侧面进入外壳,并通过炉前的法兰圆锥形延伸部分(5)排出。在该圆锥形部分中,流通面积减少了40%至80%。因此,涡旋空气在通过圆柱形管道(7)进入熔炉之前被加速。空气出口速度在20到60 m / sec之间,并且在任何情况下都大于所讨论燃料的火焰传播速度。燃油管的末端直径应在0.1至4.0(优选0.5-1.0)之间。管道末端的上游。这些措施结合起来会减慢初始燃烧速率,使燃烧温度趋于平坦。曲线并降低其峰值。这继而抑制了氮氧化物的形成。

著录项

  • 公开/公告号FR2339133A1

    专利类型

  • 公开/公告日1977-08-19

    原文格式PDF

  • 申请/专利权人 SUMITOMO METAL IND LTD;

    申请/专利号FR19770002139

  • 发明设计人

    申请日1977-01-26

  • 分类号F23C7/00;F23D5/00;F23D15/00;

  • 国家 FR

  • 入库时间 2022-08-22 23:45:46

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