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Correspondence Between “Stable” Flame Macrostructure and Thermo-acoustic Instability in Premixed Swirl-Stabilized Turbulent Combustion

机译:预混涡流稳定湍流燃烧中“稳定”火焰宏观结构与热声不稳定性之间的对应关系

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摘要

Copyright © 2015 by ASME. In this paper, we conduct an experimental investigation to study the link between the flame macroscale structure - or flame brush spatial distribution - and thermo-acoustic instabilities, in a premixed swirl-stabilized dump combustor. We operate the combustor with premixed methane-air in the range of equivalence ratio (Φ) from the lean blowout limit to Φ = 0. 75. First, we observe the different dynamic modes in this lean range as Φ is raised. We also document the effect of Φ on the flame macrostructure. Next, we examine the correspondence between dynamic mode transitions and changes in flame macrostructure. To do so, we modify the combustor length - by downstream truncation - without changing the underlying flow upstream. Thus, the resonant frequencies of the geometry are altered allowing for decoupling the heat release rate fluctuations and the acoustic feedback. Mean flame configurations in the modified combustor and for the same range of equivalence ratio are examined, following the same experimental protocol. It is found that not only the same sequence of flame macrostructures is observed in both combustors but also that the transitions occur at a similar set of equivalence ratio. In particular, the appearance of the flame in the outside recirculation zone (ORZ) in the long combustor - which occurs simultaneously with the onset of instability at the fundamental frequency - happens at similar Φ when compared to the short combustor, but without being in latter case accompanied by a transition to thermo-acoustic instability. Then, we interrogate the flow field by analyzing the streamlines, mean, and rms velocities for the nonreacting flow and the different flame types. Finally, we focus on the transition of the flame to the ORZ in the acoustically decoupled case. Our analysis of this transition shows that it occurs gradually with an intermittent appearance of a flame in the ORZ and an increasing probability with Φ. The spectral analysis of this phenomenon - we refer to as "ORZ flame flickering" - shows the presence of unsteady events occurring at two distinct low frequency ranges. A broad band at very low frequency in the range ∼(1 Hz-10 Hz) associated with the expansion and contraction of the inner recirculation zone (IRZ) and a narrow band centered around 28 Hz which is the frequency of rotation of the flame as it is advected by the ORZ flow.
机译:ASME版权所有©2015。在本文中,我们进行了实验研究,以研究预混合旋流稳定的排风燃烧室中火焰宏观结构(或火焰刷空间分布)与热声不稳定性之间的联系。我们在从稀燃极限到Φ= 0的当量比(Φ)范围内,使用预混合的甲烷-空气运行燃烧器。首先,随着Φ的升高,我们观察到该稀燃范围内的不同动态模式。我们还记录了Φ对火焰宏观结构的影响。接下来,我们检查动态模式转换与火焰宏观结构变化之间的对应关系。为此,我们修改了燃烧器的长度-通过下游截断-而不改变上游的基础流量。因此,改变了几何形状的谐振频率,从而允许将热释放速率波动和声反馈去耦。按照相同的实验方案,检查改进的燃烧室中的平均火焰构型以及当量比的相同范围。发现不仅在两个燃烧器中观察到相同的火焰宏观结构序列,而且还以相似的当量比组发生过渡。特别是,长燃烧器中外部再循环区(ORZ)中的火焰出现(与基波频率不稳定性的发生同时发生)与短燃烧器相比在相似的Φ处发生,但在短燃烧器中没有出现伴有向热声不稳定的过渡。然后,我们通过分析非反应流和不同火焰类型的流线,均值和均方根速度来询问流场。最后,我们着眼于在声学上分离的情况下火焰向ORZ的过渡。我们对这种转变的分析表明,这种转变是逐渐发生的,在ORZ中出现断断续续的火焰现象,而随着Φ的出现概率增加。这种现象的频谱分析-我们称为“ ORZ火焰闪烁”-显示了在两个不同的低频范围内发生的不稳定事件的存在。与内部再循环区(IRZ)的膨胀和收缩相关的在〜(1 Hz-10 Hz)范围内的非常低频率的宽频带和以28 Hz为中心的窄带,该窄带以火焰的旋转频率为中心它受ORZ流的影响。

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