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INFLUENCE OF PRE-FLAME AND POST-FLAME MIXING ON NO_X-FORMATION IN A REACTING PREMIXED JET IN HOT CROSS FLOW

机译:在热十字流动反应预混射流中NO_x形成前火焰和火焰混合的影响

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Axial staging in premixed gas turbine combustors is a promising option for the increase of firing temperature without NO_x-penalty and for the improvement of turndown ratio, which is limited by the onset of CO-emissions. The configuration of greatest interest is the combination of state of the art premixed combustion in the primary stage with secondary injectors near the turbine inlet, which feed additional jets of premixed combustible mixture into the hot cross flow. Regarding NO_x this configuration is particularly beneficial (1) if the overall mixing quality in the first stage is limited, (2) if the difference between primary zone flame temperature and turbine inlet temperature due to air addition along the combustor is large and (3) if a high degree of mixing in the second stage is achieved. The potential of this promising combustion concept was investigated in a large scale atmospheric test rig. For the study presented below scaling of the second stage according to Karlovitz number similarity was chosen. This leads to smaller jet diameters and higher injection velocities compared to scaling based on Damkohler number applied in an earlier study. The impact of the higher velocities at the injector outlet on the flow field, on the lift-off height of the flame and on NO_x-formation is analyzed. A chemical network model is presented, which illustrates the effects of pre-flame and post-flame mixing on NO_x-formation under atmospheric and high pressure conditions. In addition this model is used to study the interactions of chemistry with mixing between the reacting jet and cross flow. On the basis of atmospheric testing and reactor modeling, predictions for engine pressure are made assuming similar lift-off as well as pre- and post-flame mixing. These results are further analyzed regarding the NO_x-reduction potential at different equivalence ratios and residence times. Finally, it is discussed under which conditions the investigated configuration can be beneficially applied to reduce NO_x-emissions of real engines.
机译:预混合燃气轮机燃烧器中的轴向分级是未经NO_X-and的烧制温度的增加和调节比的提高,这是有限的,这是由共发出的发生限制。最大兴趣的构造是在涡轮机入口附近的次级喷射器中的初级阶段中最先进的燃烧的组合,其将预混合的可燃混合物的额外喷射馈送到热交叉流中。关于NO_X这种配置特别有益(1)如果第一阶段的整体混合质量是有限的,则(2)如果由于沿着燃烧器的空气添加引起的主要区域火焰温度和涡轮机入口温度,则(3)如果实现了第二阶段的高度混合。在大规模的大气试验台中研究了这一有前景燃烧概念的潜力。对于根据Karlovitz编号相似性的第二阶段提出的研究。与基于早期研究中的Damkohler号码的缩放相比,这导致较小的射流直径和更高的注射速度。分析了在流场上的喷射器出口处的较高速度的影响,在火焰和NO_x形成的升空高度上。提出了一种化学网络模型,其说明了在大气和高压条件下NO_x形成上的火焰和后火焰混合的影响。此外,该模型用于研究化学的相互作用与反应射流和交叉流动之间的混合。在大气检测和反应堆建模的基础上,假设类似的剥离以及预防和火焰后混合的预测。这些结果进一步分析了不同当量比和停留时间的NO_X降低潜力。最后,讨论了调查配置可以有利地应用于减少真正发动机的NO_X排放的条件。

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