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    • 1. 发明申请
    • Ultra-low NOx burner assembly
    • 超低NOx燃烧器组件
    • US20070254251A1
    • 2007-11-01
    • US11412006
    • 2006-04-26
    • Jin CaoMahendra JoshiAleksandar Slavejkov
    • Jin CaoMahendra JoshiAleksandar Slavejkov
    • F23C5/00
    • F23D14/22F23C6/047F23D14/32F23D14/583F23D14/74
    • Burner assembly comprising (a) an elongated body having a periphery, a discharge end adjacent a combustion zone, and an axis, wherein the axis extends into the combustion zone; (b) one or more oxidant nozzles disposed at the discharge end of the elongated body and adapted to discharge a gaseous oxidant into the combustion zone; and (c) one or more fuel nozzles disposed at the discharge end of the elongated body and adapted to discharge a fuel into the combustion zone. At least one of the oxidant and fuel nozzles is characterized by a shape factor, σ, that is greater than about 10, wherein σ is a dimensionless parameter defined as σ=P2/2A where P is the perimeter dimension of the discharge opening and A is the area of the discharge opening.
    • 燃烧器组件,其包括(a)具有周边的细长主体,与燃烧区相邻的排出端和轴,其中所述轴延伸到所述燃烧区中; (b)一个或多个氧化剂喷嘴,设置在细长体的排放端,并适于将气态氧化剂排放到燃烧区中; 和(c)一个或多个燃料喷嘴,设置在细长主体的排放端,并适于将燃料排放到燃烧区。 氧化剂和燃料喷嘴中的至少一个的特征在于大于约10的形状因子σ,其中σ是定义为σ= P 2 / 2A的无量纲参数,其中P是 排出口的周长尺寸A为排出口的面积。
    • 10. 发明授权
    • Liquid-fuel combustion system
    • 液体燃料燃烧系统
    • US06688876B2
    • 2004-02-10
    • US09870500
    • 2001-06-01
    • Olivier DelabroyPierre BodelinMahendra JoshiBernard LabegoreFrançois Lacas
    • Olivier DelabroyPierre BodelinMahendra JoshiBernard LabegoreFrançois Lacas
    • F23D1100
    • F23M5/025F23D11/002F23D2209/20F23D2900/00006
    • A process for combustion with the aid of a liquid fuel and a gaseous oxidizer containing from 20% to 100% volume of oxygen, in which the fuel is injected with the aid of an injector. The injector, which has a height “d”, is placed inside a glory hole. The glory hole has a height “D” at the end thereof corresponding to the ejection of the gaseous mixture towards the zone of heating of a charge. A coefficient “S” in the following equation is maintained at a value less than or equal to 1 for substantially the entire duration of combustion to ensure the stability of the flame. S = a 1 ⁢ V equivalent - a 2 ⁢ L a 3 ⁢ d ⁡ ( 2 - e - L / 10 ⁢ D ) with a1=2.5·10−11 a2=1·10−9, dimensionless a3=(0.875·&ggr;+0.525)·10−6, dimensionless. In the above equation, “L” is defined as the distance between the end of the liquid fuel injector and the downstream end in the fluid flow direction of the glory hole. “Vequivalent” is defined either as the equivalent velocity representative of the average velocity of the spray of drops of liquid fuel in the case of mechanical atomizers and being equal to 2.4 M/(&rgr;&pgr;d2), or a velocity equal to 0.5 times Vatomization, in other cases. “&ggr;” is defined as the overall (volume) percentage of oxygen in the gases at the exit of the glory hole.
    • 借助于液体燃料和含有20%至100%体积的氧的气态氧化剂的燃烧过程,其中借助于喷射器喷射燃料。 具有高度“d”的喷射器放置在光亮孔内。 荣耀孔在其端部具有高度“D”,其对应于气体混合物向加料区域的喷射。 在几乎整个燃烧持续时间内,下列公式中的系数“S”保持在小于或等于1的值,以确保火焰的稳定性.a1 = 2.5.10 <-11> a2 = 1.10 <-9 >,无量纲3 =(0.875.gamma + 0.525).10 -6,无量纲。在上式中,“L”定义为液体燃料喷射器的端部与流体流动方向上的下游端之间的距离 的荣耀之穴。 “Vequivalent”定义为等效速度,表示在机械雾化器情况下液体燃料滴喷射的平均速度等于2.4M /(rhopid2)或等于0.5倍的速度的等效速度 在其他情况下,分解。 “伽马”定义为荣耀孔出口处气体中氧气的总体积(体积)百分比。