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Detailed characterization of the dynamics of thermoacoustic pulsations in a lean premixed swirl flame

机译:稀薄预混旋流火焰中热声脉动动力学的详细表征

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A nozzle configuration for technically premixed gas turbine flames was operated with CH_4 and air at atmospheric pressure. The flames were confined by a combustion chamber with large quartz windows, allowing the application of optical and laser diagnostics. In a distinct range of operating conditions the flames exhibited strong self-excited thermoacoustic pulsations at a frequency around 290 Hz. A flame with P = 25 kW thermal power and an equivalence ratio of Φ = 0.7 was chosen as a target flame in order to analyze the dynamics and the feedback mechanism of the periodic instability in detail. The velocity field was measured by three-component laser Doppler velocimetry, the flame structures were measured by chemiluminescence imaging and planar laser-induced fluorescence of OH, and the joint probability density functions of major species concentrations, mixture fraction, and temperature were measured by laser Raman scattering. All measuring techniques were applied in a phase-locked mode with respect to the phase angle of the periodic pulsation. In addition to the pulsating flame, a nonpulsating flame with increased fuel flow rate (P = 30 kW, Φ = 0.83) was studied for comparison. The measurements revealed significant differences between the structures of the pulsating and the nonpulsating (or "quiet") flame. Effects of finite-rate chemistry and unmixedness were observed in both flames but were more pronounced in the pulsating flame. The phase-locked measurements revealed large variations of all measured quantities during an oscillation cycle. This yielded a clear picture of the sequence of events and allowed the feedback mechanism of the instability to be identified and described quantitatively. The data set presents a very good basis for the verification of numerical combustion simulations because the boundary conditions of the experiment were well-defined and the most important quantities were measured with a high accuracy.
机译:用于技术预混燃气轮机火焰的喷嘴配置是在CH_4和大气压力下运行的。火焰由带有大石英窗的燃烧室限制,允许进行光学和激光诊断。在不同的工作条件范围内,火焰在290 Hz左右的频率下表现出强烈的自激热声脉动。选择P = 25 kW热功率且Φ= 0.7的当量比的火焰作为目标火焰,以详细分析周期性不稳定性的动力学和反馈机制。通过三分量激光多普勒测速仪测量速度场,通过化学发光成像和平面激光诱导的OH荧光测量火焰结构,并通过激光测量主要物质浓度,混合比和温度的联合概率密度函数。拉曼散射。相对于周期性脉动的相位角,所有测量技术均以锁相模式应用。除了脉动火焰外,还研究了燃料流量增加(P = 30 kW,Φ= 0.83)的非脉动火焰进行比较。测量结果表明脉动和非脉动(或“安静”)火焰的结构之间存在显着差异。在两种火焰中均观察到了有限速率化学作用和不混合的影响,但在脉动火焰中则更为明显。锁相测量揭示了一个振荡周期内所有测量量的巨大变化。这清楚地显示了事件的顺序,并允许识别和定量描述不稳定性的反馈机制。该数据集为验证燃烧数值模拟提供了很好的基础,因为实验的边界条件是明确定义的,并且最重要的量都以高精度进行了测量。

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