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Laser-Based Investigations of Periodic Combustion Instabilities in a Gas Turbine Model Combustor

机译:基于激光的燃气轮机模型燃烧器周期性燃烧不稳定性研究

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The driving mechanism of pulsations in gas turbine combustors depends on a complex interaction between flow field, chemistry, heat release, and acoustics. Experimental data on all these factors are therefore required to obtain insight into the coupling mechanisms during a pulsation period. In order to develop a comprehensive experimental database to support a phenomenological understanding and to provide validation data for numerical simulation, a standard burner for optical investigations was established that exhibits strong self-excited oscillations. The burner was a swirl-stabilized nonpremixed model combustor designed for gas turbine applications and operated using methane as fuel at atmospheric pressure. It was mounted in a combustion chamber, which provides almost unobstructed optical access. The periodic combustion instabilities were studied by a variety of phase-resolved laser-based diagnostic techniques, locked to the frequency of the dominant pressure oscillation. Measurement techniques used were LDV for velocity measurements, planar laser-induced fluorescence for imaging of CH and OH radicals, and laser Raman scattering for the determination of the major species concentrations, temperature, and mixture fraction. The phase-resolved measurements revealed significant variations of all measured quantities in the vicinity of the nozzle exit, which trailed off quickly with increasing distance. A strong correlation of the heat release rate and axial velocity at the nozzle was observed, while the mean mixture fraction as well as the temperature in the periphery of the flame is phase shifted with respect to axial velocity oscillations. A qualitative interpretation of the experimental observations is given, which will help to form a better understanding of the interaction between flow field, mixing, heat release, and temperature in pulsating reacting flows, particularly when accompanied by corresponding CFD simulations that are currently underway.
机译:燃气轮机燃烧室中脉动的驱动机制取决于流场,化学物质,热释放和声学之间的复杂相互作用。因此,需要所有这些因素的实验数据来了解脉动期间的耦合机制。为了开发全面的实验数据库以支持现象学理解并为数值模拟提供验证数据,建立了用于光学研究的标准燃烧器,该燃烧器表现出强烈的自激振荡。燃烧器是涡旋稳定的非预混合模型燃烧器,设计用于燃气轮机应用,并在大气压下使用甲烷作为燃料运行。它安装在燃烧室中,可以提供几乎无障碍的光学通道。通过各种基于相位分辨的基于激光的诊断技术研究了周期性燃烧的不稳定性,并将其锁定在主要压力振荡的频率上。使用的测量技术包括:LDV用于速度测量,平面激光诱导的荧光用于CH和OH自由基成像,以及激光拉曼散射用于确定主要物质浓度,温度和混合物分数。相位分辨的测量结果表明,在喷嘴出口附近所有测量值都有明显的变化,并且随着距离的增加而迅速下降。观察到喷嘴处的放热速率和轴向速度之间有很强的相关性,而平均混合物分数以及火焰周围的温度相对于轴向速度振荡则发生了相移。给出了对实验观察的定性解释,这将有助于更好地理解脉动反应流中的流场,混合,放热和温度之间的相互作用,特别是在伴随着当前正在进行的CFD模拟的情况下。

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