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Development of a multiple opposing jets' burner for premixed flames

机译:研发了多种用于预混火焰的对置射流燃烧器

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摘要

A burner was developed to accommodate multiple opposing premixed flames, where the turbulence stimulated by impingement was found to extend the stability limits of methane/air mixtures. The opposing jets established closed loop flow currents in a number of sectors, which is twice that of the jets thus providing more eddies within a stronger turbulent flame structure. The stagnation zone for four opposing jets was testified to be larger than that for two jets such that it was able to sustain higher reactive jet velocities up to 14.2 m/s at larger flow shearing rates. Increasing the number of opposing jets and decreasing their separation distance provided higher rates of heat/mass transfer into the ports. As the flow deceleration zone was enlarged, the correspondingly higher burning capacities were correlated to the port diameter, the separation distance, the number of jets, Reynolds number, and the strain rate. Strain rates of growing magnitudes up to 13,080 s~(-1) were sustained at jet velocities as high as 21.8m/s. At such velocities and upon increasing the ratio of the jet diameter to the separation distance, the turbulent kinetic energy was found to exhibit one local peak, as the strain rate due to impingement became enriched by the jet radial shearing effects. A lean blowout equivalence ratio of 0.59 was pronounced as a basis for acquiring low NO_x emissions. The burner serves as a potential prototype for increasing the power-to-weight ratio of the combustion chambers like those utilized in furnaces, boilers, gas turbines, as well as jet-propelled vehicles with effectively minimized emissions of pollutants.
机译:开发了一种燃烧器,以容纳多个相对的预混火焰,在该火焰中,撞击引起的湍流扩大了甲烷/空气混合物的稳定性极限。相对的射流在多个扇区中建立了闭环流,这是射流的两倍,因此在更强的湍流火焰结构中提供了更多的涡流。事实证明,四个相对射流的停滞区要大于两个射流的停滞区,以使其在较大的剪切速率下能够维持更高的反应射流速度,最高可达14.2 m / s。增加相对喷嘴的数量并减小其分离距离可提供更高的热量/质量传递到端口的速率。随着气流减速区域的扩大,相应较高的燃烧能力与端口直径,分离距离,射流数,雷诺数和应变率相关。在高达21.8m / s的射流速度下,应变速率一直保持在13080 s〜(-1)。在这样的速度下,随着射流直径与分离距离之比的增加,湍流动能显示出一个局部峰值,这是由于冲击引起的应变率被射流径向剪切效应所丰富。稀薄的井喷当量比为0.59,这是获得低NO_x排放量的基础。该燃烧器是提高燃烧室功率/重量比的潜在原型,如燃烧室,锅炉,燃气轮机以及喷气推进车辆中使用的燃烧室,可有效地将污染物排放降至最低。

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