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Confinement Effects on Flow Dynamics in Swirling Flames

机译:约束对旋流流动动力学的影响

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Three-dimensional (3-D) flowfield data has been obtained using Particle Image Velocimetry (PIV) for varying swirl distributions in the burner. The 3-D data also allows one determine the local swirl number of the resulting flow. Flow characteristics of the resulting flowfield, both without and with combustion, have been examined for the effect of co- and counter-swirl under lean direct injection conditions using unconfined and confined combustor geometry. Experimental results of the effect of swirl and combustion are presented to simulate the flow dynamics of Lean Direct Injection (LDI) configuration gas turbine combustion. The selected configuration is typical because it does not make use a premixing zone and relies totally on the swirl and the injector to accomplish rapid mixing. Specifically, the effect of radial distribution of combustion air and swirl in a burner are examined under non-burning and burning conditions using propane as the fuel. The present study explores single swirler interaction with the use of an experimental double concentric swirl burner that simulates one swirler of a practical gas turbine combustor. Results showed that both swirl and combustion has significant effect on the characteristics of the internal and external recirculation zones. The calculated local swirl number differs significantly form that estimated using geometrical relationship derived from the vane angle only. The effect of combustion for the confined and unconfmed geometries was also been found to be different. In the confined geometry combustion decreases the size of the recirculation zone. This is in contrast to that found for the unconfmed conditions. Combustion enhances the recirculation zone in the unconfmed geometry. Combustion provides greater velocity magnitudes than their counter non-combustion conditions. The counter-swirl combination resulted in smaller and more well defined internal recirculation regions. The results provide the role of swirl and combustion on the mean and turbulence characteristics of flows over a range of swirl and shear conditions between the inner and outer flow of the burner. This data provides important insights on the flow dynamics in addition to providing data for model validation and model development.
机译:使用粒子图像测速(PIV)获得了用于改变燃烧器中旋流分布的三维(3-D)流场数据。 3-D数据还可以确定结果流的局部旋流数。在无限制和受限的燃烧室几何形状下,已经检查了在稀薄直接喷射条件下产生的流场的流动特性(不带燃烧和带燃烧)的共涡流和反涡流的影响。给出了旋流和燃烧影响的实验结果,以模拟稀薄直接喷射(LDI)配置的燃气轮机燃烧的流动动力学。选择的配置是典型的,因为它不使用预混合区,并且完全依靠涡流和喷射器来完成快速混合。具体地,在丙烷和非丙烷燃烧条件下,以丙烷为燃料,研究了燃烧空气径向分布和燃烧器中涡流的影响。本研究探索了单旋流器的相互作用,并使用了实验性的双同心旋流燃烧器,该燃烧器模拟了实际燃气轮机燃烧室的一个旋流器。结果表明,旋流和燃烧对内部和外部再循环区的特性都有重要影响。计算出的局部旋流数与仅使用从叶片角导出的几何关系所估算出的显着不同。还发现燃烧对于受限和未受限几何形状的影响是不同的。在受限的几何形状中,燃烧减小了再循环区域的尺寸。这与无限制条件下发现的相反。燃烧增强了无约束几何形状中的再循环区域。燃烧提供了比其非燃烧条件更大的速度幅值。反旋流组合产生了更小,更清晰的内部再循环区域。结果提供了旋流和燃烧对燃烧器内流和外流之间一定范围的旋流和剪切条件下的流的平均和湍流特性的作用。除了提供用于模型验证和模型开发的数据外,该数据还提供了有关流动力学的重要见解。

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