首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Combustion of a hydrogen jet normal to multiple pairs of opposing methane-air mixtures
【24h】

Combustion of a hydrogen jet normal to multiple pairs of opposing methane-air mixtures

机译:垂直于多对相对的甲烷-空气混合物的氢射流的燃烧

获取原文
获取原文并翻译 | 示例
           

摘要

The combustion performance of a cylindrical burner accommodating up to six multiple pairs of opposing methane-air mixtures with a cross-flow of hydrogen was addressed. The cross-flow initially duplicated the stagnation impact and enriched the vortical structures. Aided by the resulting flow strain, the transport of heat and active species from the hydrogen oxidation zone to the methane reaction zones accelerated the combustion across the opposing premixed flames and reduced the peak temperature across the outer diffusion flame. Increasing the cross-flow/opposing jets' velocity ratio to 0.89 merged the two stagnation centers and maximized the shearing stress. By the slight increase in the velocity ratio to 1.07, the H and OH pools provided for methane combustion became closer to the ports such that a hydrogen/methane mass percent of 10.3% extended the stoichiometric blowout velocity from 28.3 to 35.7m/s. Since the turbulent kinetic energy thus increased to 8.4m(2)/s(2), the firing intensity reached values as high as 48.2MW/m(3). Not only was there a reduction in the residence time for NOx formation, but also the blowout velocity relative gain overrode the relative increase in the NOx formation rates such that the NOx emission index decreased to 17g/MWhr. By the excessive increase in velocity ratio, the vortical structures shrank such that the NOx exponential increase became dominant above 21ppm. With fuel-lean mixtures, the hydrogen was partially combusted by the excess air from the opposing flames but the blowout velocity decreased to 13.1m/s at phi=0.50. The hydrogen flame NOx emissions decreased by providing the excess air at larger jets' diameter/separation ratios, thus reducing the residence times for thermal NOx formation and simultaneously interrupting the prompt NOx formation. At the lean operational limit, tripling the number of opposing jets decreased the hydrogen flame length by 54% such that the NOx emissions decreased by 38.4%.
机译:提出了一种圆柱形燃烧器的燃烧性能,该燃烧器最多可容纳六对多对相对的甲烷-空气混合物,并带有氢气交叉流。横流最初复制了停滞冲击并丰富了涡旋结构。在产生的流动应变的帮助下,热量和活性物质从氢氧化区向甲烷反应区的传输加速了相对的预混火焰的燃烧,并降低了外部扩散火焰的峰值温度。将横流/对流射流的速度比提高到0.89,可以使两个停滞中心融合在一起,并使剪切应力最大化。通过将速度比略微提高到1.07,提供给甲烷燃烧的H和OH池变得更靠近端口,从而氢气/甲烷质量百分比为10.3%,将化学计量的喷吹速度从28.3扩展到35.7m / s。由于湍动能因此增加到8.4m(2)/ s(2),因此燃烧强度达到了高达48.2MW / m(3)的值。不仅减少了NOx形成的停留时间,而且井喷速度相对增益抵消了NOx形成速率的相对增加,使得NOx排放指数降低到17g / MWhr。由于速度比的过度增加,涡旋结构收缩,使得NOx指数增加在21ppm以上占主导地位。对于贫燃料的混合物,氢被来自相反火焰的过量空气部分燃烧,但在phi = 0.50时,喷出速度降至13.1m / s。通过以较大的喷嘴直径/分离比提供过量的空气,减少了氢火焰NOx的排放,从而减少了形成热NOx的停留时间,同时中断了迅速形成NOx的过程。在稀薄运行极限时,对置喷嘴数量增加三倍,氢火焰长度减少了54%,因此NOx排放量减少了38.4%。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号