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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室中周期燃烧不含的研究

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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 data base 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 non-premixed 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 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 which are currently under way.
机译:燃气轮机燃烧器脉动的驱动机构取决于流场,化学,热释放和声学之间的复杂相互作用。因此,在脉动时段期间需要对所有这些因素的实验数据获得进入耦合机构的洞察。为了开发一个全面的实验数据库来支持现象学理解并提供数值模拟的验证数据,建立了对光学研究的标准燃烧器,其表现出强烈的自我激发振荡。燃烧器是旋流稳定的非预混模型燃烧器,专为燃气轮机应用而设计,并在大气压下使用甲烷作为燃料操作。它安装在燃烧室中,提供几乎无阻碍的光学接入。通过基于相位分辨的激光的诊断技术研究了周期性燃烧不稳定性,锁定到主压力振荡的频率。所用测量技术是LDV,用于速度测量,平面激光诱导的荧光用于CH和OH自由基的成像,以及用于测定主要物种浓度,温度和混合级分的激光拉曼散射。相位分辨的测量显示喷嘴出口附近的所有测量量的显着变化,随着距离的增加,速度快速地关闭。观察到热释放速率和喷嘴处的轴向速度的强关系,而平均混合分数以及火焰周边的温度相对于轴向速度振荡相移。给出了对实验观察的定性解释,这将有助于在脉动反应流动中更好地理解流场,混合,热释放和温度之间的相互作用,特别是当伴随当前正在进行的相应的CFD模拟时。

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