首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.2; 20070514-17; Montreal(CA) >EXPERIMENTAL INVESTIGATION OF THE STABILITY MECHANISM AND EMISSIONS OF A LIFTED SWIRL NON-PREMIXED FLAME
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EXPERIMENTAL INVESTIGATION OF THE STABILITY MECHANISM AND EMISSIONS OF A LIFTED SWIRL NON-PREMIXED FLAME

机译:旋流式非半球形火焰稳定机理和排放的实验研究

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摘要

We report on the experimental investigation of a confined lifted swirl non-premixed flame by applying a novel Airblast nozzle [1]. 3D-Laser Doppler Anemometry, a non-intrusive, laser-based measurements technique, is adapted for the measurement of all three mean velocity components and of the six Reynolds stress components. The determination of the temperature and mixture field occurs by employing in-flame measurement techniques. Valuable information concerning the mixing procedure, the temperature distribution, the turbulence level and the velocity field of the flame is provided. The results demonstrate that there is sufficient residence time in the pre-combustion area of the lifted flame in order to achieve spatial and temporal uniformity of the mixture, leading to a quasi premixed state. It was also found that hot reaction products, carried upstream by large vortices along the jet, could possibly react with fresh unburnt mixture in a re-ignition process. The determination of the flow pattern revealed the presence of an inner weak recirculation zone in the nozzle vicinity and a dominant external recirculation zone. The examination of the probability density function (PDF) of the velocity-measurements was also found to be a very useful tool in terms of the analysis of the turbulence structure of the flow. The bimodal distribution yield the existence of large scaled eddies in the shear layer between the downstream flow and the recirculated gases. Finally, the significant reduced Nox emissions in the lean area were also shown by means of emission measurements for elevated pressure conditions.
机译:我们通过应用新型Airblast喷嘴[1]报告了有限的提升旋流未预混火焰的实验研究。 3D激光多普勒风速测定法是一种非侵入性的,基于激光的测量技术,适用于测量所有三个平均速度分量和六个雷诺应力分量。通过采用火焰测量技术确定温度和混合气场。提供了有关混合过程,温度分布,湍流水平和火焰速度场的重要信息。结果表明,在提升的火焰的预燃烧区域中有足够的停留时间,以实现混合物的时空均匀性,从而导致准预混合状态。还发现,由大涡流沿射流向上游携带的热反应产物可能在重燃过程中与新鲜的未燃烧混合物发生反应。流动模式的确定揭示了在喷嘴附近存在内部弱再循环区域和主要的外部再循环区域。速度测量的概率密度函数(PDF)的检查也被认为是分析流动湍流结构的非常有用的工具。双峰分布导致在下游流和再循环气体之间的剪切层中存在大尺度的涡流。最后,还通过在升高的压力条件下进行排放测量,显示出在贫油区NOx排放量显着降低。

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