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首页> 外文期刊>Journal of natural gas science and engineering >Experimental study of impact of swirl number as well as oxygen and carbon dioxide content in natural gas combustion air on flame flashback and blow-off
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Experimental study of impact of swirl number as well as oxygen and carbon dioxide content in natural gas combustion air on flame flashback and blow-off

机译:天然气燃烧空气中旋流数以及氧气和二氧化碳含量对火焰回燃和吹出影响的实验研究

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摘要

In this paper, experiments involving the combustion of natural gas in a quartz tube using a burner with three swirl generators were conducted to determine ranges of stable combustion limited by flame flashback and blow-off. The swirl generators with a tangential supply of substrates were described using the geometric swirl numbers: 0.69, 1.16, and 1.35. Effects on combustion atmospheres such as air, air enriched with up to 25 vol. % of oxygen, and oxygen-enriched air with addition of 15 vol. % of CO2 per stable combustion range were tested. The findings of the experiments proved that enriching air with oxygen leads to an expansion of the stable combustion range because the curve of flame blow-off progresses quicker than that of flashback. In terms of flame flashback, the burner with swirl generator S-g = 1.35 turned out to be the most favorable for the combustion atmospheres under consideration. The highest resistance of the flame against flashback was recorded for air. Addition of CO2 to oxygen-enriched air improved the flashback limits. The most favorable stable combustion range was calculated for the atmosphere of air enriched with up to 25 vol. % of oxygen when S-g = 135 and that of air when S-g = 0.69. The smallest stable combustion range, which was 26% smaller than the best result, was recorded for the mixture of oxygen-enriched air and 15 vol. % of CO2 when S-g = 0.69. (C) 2016 Elsevier B.V. All rights reserved.
机译:在本文中,进行了涉及使用带有三个涡流发生器的燃烧器在石英管中燃烧天然气的实验,以确定稳定的燃烧范围,该范围受火焰回燃和吹扫的限制。使用切向几何形状的旋流数:0.69、1.16和1.35描述了具有切向供给基材的旋流发生器。对燃烧气氛(例如空气)的影响,空气浓缩至25 vol。 %的氧气和添加15 vol。测试了每个稳定燃烧范围内的%CO2。实验的结果证明,用氧气富集空气会导致稳定燃烧范围的扩大,因为火焰吹散的曲线比闪回的曲线发展得更快。在火焰回火方面,带有涡流发生器S-g = 1.35的燃烧器被认为是最适合所考虑的燃烧气氛的燃烧器。记录了火焰对火焰的最高抵抗力。向富氧空气中添加CO2可改善回火极限。计算出最有利的稳定燃烧范围,该燃烧范围是富集至多25 vol。当S-g = 135时,氧气的百分含量;当S-g = 0.69时,氧气的百分含量。记录了富氧空气和15体积比的混合物的最小稳定燃烧范围,比最佳结果小26%。当S-g = 0.69时,CO2的百分比。 (C)2016 Elsevier B.V.保留所有权利。

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