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Characteristics and structure of inverse flames of natural gas

机译:天然气逆火焰的特征与结构

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Characteristics and structure of nominally non-premixed flames of natural gas are investigated using a burner that employs simultaneously two distinct features: fuel and oxidiser direct injection, and inverse fuel and oxidiser delivery. At low exit velocities, the result is an inverse diffusion flame that has been noted in the past for its low NO_x emissions, soot luminosity, and narrow stability limits. The present study aimed at extending the burner operating range, and it demonstrated that the inverse flame exhibits a varying degree of partial premixing dependent on the discharge nozzle conditions and the ratio of inner air jet and outer fuel jet velocities. These two variables affect the flame length, temperature distributions, and stability limits. Temperature measurements and Schlieren visualisation show areas of enhanced turbulent mixing in the shear region and the presence of a well-mixed reaction zone on the flame centreline. This reaction zone is enveloped by an outer diffusion flame, yielding a unique double-flame structure. As the fuel-air equivalence ratio is decreasing with an increase in the inner jet velocity, the well-mixed reaction zone extends considerably. These findings suggest a method for establishing a flame of uniform high temperature by optimising the coaxial nozzle geometry and flow conditions. The normalised flame length is decreasing exponentially with the air/fuel velocity ratio. Measurements demonstrate that the inverse flame stability limits change qualitatively with varying degree of partial premixing. At the low premixing level, the flame blow-out is a function of the inner and outer jet velocities and the nozzle conditions. The flame blow-out at high degree of partial premixing occurs abruptly at a single value of the inner air jet velocity, regardless of the fuel jet velocity and almost independent of the discharge nozzle conditions.
机译:使用同时具有两个明显特征的燃烧器研究了名义上非预混天然气的特征和结构:燃料和氧化剂直接喷射,以及反向燃料和氧化剂输送。在低出口速度下,结果是反向扩散火焰,该火焰过去因其NO_x排放低,烟灰光度和狭窄的稳定性限制而闻名。本研究旨在扩大燃烧器的工作范围,并证明了逆火焰表现出不同程度的部分预混合,这取决于排放喷嘴的状况以及内部空气喷射和外部燃料喷射的速度之比。这两个变量会影响火焰长度,温度分布和稳定性极限。温度测量和Schlieren可视化显示了剪切区域湍流混合增强的区域以及火焰中心线上存在充分混合的反应区域。该反应区被外部扩散火焰包围,产生独特的双重火焰结构。随着燃料-空气当量比随着内部射流速度的增加而减小,充分混合的反应区显着延伸。这些发现提出了一种通过优化同轴喷嘴的几何形状和流动条件来建立均匀高温火焰的方法。归一化的火焰长度随着空气/燃料速度比呈指数下降。测量表明,反向火焰稳定性极限随着部分预混程度的变化而发生质的变化。在低预混合水平下,火焰的吹出是内部和外部射流速度以及喷嘴条件的函数。无论燃料喷射速度如何,并且几乎与排放喷嘴的状况无关,在高度内部预混合的情况下,在内部空气喷射速度的单一值下突然发生火焰喷出。

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