首页> 外文会议>2003 ASME(American Society of Mechanical Engineers) Turbo Expo; Jun 16-19, 2003; Atlanta, Georgia >MODELING THE RESPONSE OF PREMIXED FLAMES TO MIXTURE RATIO PERTURBATIONS
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MODELING THE RESPONSE OF PREMIXED FLAMES TO MIXTURE RATIO PERTURBATIONS

机译:模拟预混合火焰对混合比扰动的响应

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Combustion instabilities continue to cause significant reliability and availability problems in low emissions gas turbine combustors. It is known that these instabilities are often caused by a self-exciting feedback loop between unsteady heat release rate and reactive mixture equivalence ratio perturbations. We present an analysis of the flame's response to equivalence ratio perturbations by considering the kinematic equations for the flame front. This response is controlled by three processes: heat of reaction, flame speed, and flame area. The first two are directly generated by equivalence ratio oscillations. The third is indirect, as it is generated by the flame speed fluctuations. The first process dominates the response of the flame at low Strouhal numbers, roughly defined as frequency times flame length divided by mean flow velocity. All three processes play equal roles at Strouhal numbers of O(1). The mean equivalence ratio exerts little effect upon this transfer function at low Strouhal numbers. At O(1) Strouhal numbers, the flame response increases with decreasing values of the mean equivalence ratio. Thus, these results are in partial agreement with heuristic arguments made in prior studies that the flame response to equivalence ratio oscillations increases as the fuel/air ratio becomes leaner. In addition, a result is derived for the sensitivity of this transfer function to uncertainties in mean flame position. For example, a sensitivity of 10 means that a 5% uncertainty in flame position translates into a 50% uncertainty in transfer function. This sensitivity is of O(1) for St1, but has very high values for St~O(1).
机译:燃烧不稳定性继续在低排放燃气轮机燃烧器中引起严重的可靠性和可用性问题。众所周知,这些不稳定性通常是由不稳定的放热速率和反应性混合物当量比扰动之间的自激反馈回路引起的。通过考虑火焰前沿的运动学方程,我们对火焰对当量比扰动的响应进行了分析。该响应由三个过程控制:反应热,火焰速度和火焰面积。前两个是通过当量比振荡直接生成的。第三个是间接的,因为它是由火焰速度波动产生的。第一个过程在低Strouhal数(主要定义为频率乘以火焰长度除以平均流速)时控制火焰的响应。所有三个过程在Strouhal数为O(1)时都发挥相同的作用。在低Strouhal数下,平均当量比对该传递函数几乎没有影响。在O(1)Strouhal数下,火焰响应随平均当量比值的减小而增加。因此,这些结果与先前研究中的启发式论点部分一致,即当燃料/空气比变稀时,火焰对当量比振荡的响应会增加。另外,得出该传递函数对平均火焰位置的不确定性的敏感性的结果。例如,灵敏度为10意味着火焰位置不确定性5%转换为传递函数不确定性50%。对于St << 1,此灵敏度为O(1),但对于St〜O(1),其灵敏度非常高。

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