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EFFECT OF SWIRL NUMBER AND FUEL TYPE UPON THE COMBUSTION LIMITS IN SWIRL COMBUSTORS

机译:旋流燃烧器中燃烧限制对旋流数和燃料类型的影响

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Increasing interest in lean fuel premixed swirl combustors has arisen because of reduced NO_X emissions. Alternative fuels, including hydrogen-enriched natural gas and by products of process industries such as coke oven gas are now receiving increasing attention. This gives rise to areas of concern including, flashback, temperature levels, blow-off and combustion instability. Flashback with hydrogen containing fuels is of special concern, owing to the high flame speed of hydrogen, to such an extent that diffusion combustion is commonly employed resulting in high NO_X emissions. This paper examines the effect of hydrogen containing fuels upon flashback and blow-off in a generic, compact, premixed swirl burner in swirl number regimes representative of those found in practical systems. All results are obtained at atmospheric pressure without air preheat as a precursor to pressurised tests, the burner firing freely into atmosphere for most tests. The swirler has radial tangential inlets firing into a swirl chamber, which then feed into the exhaust. A central fuel injector just extends into the exhaust and is ~40% of the exhaust diameter, a common industrial size. Four tangential inlets are used for S=1.47, while nine has been used for S= 1.04 and S=0.8. Flashback and blow-off are sensitive to the level of swirl, the exhaust configuration and the type of fuel. High swirl numbers, S=1.47, gave flashback limits with methane considerably worse than those produced at S=1.04 and S=0.8, although there were differences in exhaust nozzle configuration. At equivalence ratios ~1 total mass flow at which flashback occurred (hence velocities) was reduced by a factor of two. Changes in flashback behaviour were especially noticeable when the hydrogen content in fuel blends was > 60% by volume. Blow-off was very much a function of hydrogen content of the fuel and Swirl Number. Best blow-off limits for all fuel blends are obtained at S=0.8, the worst for S=1.47. Coke Oven gas (COG) with 65% hydrogen content gave best blow-off limits of the fuels tested, although data was not available for pure hydrogen due to rig limitations.
机译:由于减少了NO_X排放,因此由于NO_X排放量减少而导致了对瘦燃料预混旋涡燃烧器的兴趣。替代燃料,包括富含氢气的天然气和焦炭烤箱气体的工艺行业产品现在正在接受越来越长的关注。这引起了令人担忧的领域,包括闪回,温度水平,吹扫和燃烧不稳定。由于氢气的高火焰速度,含氢含氢燃料的闪蒸是特别关注的,这在一定程度上通常采用扩散燃烧导致高NO_X排放。本文研究了在实际系统中发现的旋涡,紧凑的,预混的漩涡燃烧器中闪回和吹灰对闪回和吹扫的影响。所有结果都是在大气压下获得,无空气预热作为前体,以加压测试,燃烧器可自由烧制成大气中的大多数测试。旋流器具有径向切向入口,进入旋流室,然后进入排气。中央燃料喷射器只延伸到排气中,〜40%的排气直径,常见的工业尺寸。 S = 1.47使用四个切向入口,而九已经用于S = 1.04和S = 0.8。闪回和吹气对旋流水平,排气配置和燃料类型敏感。高漩涡号码S = 1.47,给出了氟烷值的闪回限制比S = 1.04和S = 0.8产生的甲烷相当差,尽管排气喷嘴配置有差异。在等效比率〜1中闪回(因此速度)的总质量流量减少了两倍。当燃料共混物中的氢含量> 60%(体积)时,闪回行为的变化尤其明显。爆炸非常非常多的燃料和旋流数的函数。在S = 0.8中获得所有燃料混合物的最佳吹扫限制,S = 1.47的最差。焦炉气体(COG)具有65%的氢含量,使测试的燃料的最佳吹扫限制较好,尽管由于钻机限制而无法用于纯氢气。

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