...
首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Measurements and Modeling of the Dynamic Response of a Pilot Stabilized Premixed Flame Under Dual-Input Perturbation
【24h】

Measurements and Modeling of the Dynamic Response of a Pilot Stabilized Premixed Flame Under Dual-Input Perturbation

机译:双输入扰动下稳定先导混合火焰动态响应的测量与建模

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

Pilot flames have been widely used for flame stabilization in low-emission gas turbine combustors. Effects of pilot flame on dynamic instabilities, however, are not well understood. In this work, the dynamic interactions between main and pilot flames are studied by perturbing both flames simultaneously, i.e., with. a dual-input forcing. A burner is used to generate a premixed axisyttnnetric V-shaped methane flame stabilized by a central pilot flame. Servo valve and sirens are used to produce forcing in the pilot and main flames, respectively. A diagnostic system is applied to measure the flame structure and heat release rate. The effects of forcing frequency, forcing amplitude, phase difference between the two forcing signals as well as the Reynolds number are studied. Both the flame transfer function (FTF) and the flame dynamic position are measured and analyzed. It is found that the total flame response can be modified by the perturbation in the pilot flame. The mechanism can be attributed to the effect of pilot flame on the velocity field of the burnt side. Vortex is found to be able to amplify the pilot main dynamic interactions under certain conditions. An analytical model is developed based on the linearized G equation, to further understand the flame interactions through the velocity perturbations in the burnt side. Good agreements were found between the prediction and the experiment results.
机译:先导火焰已广泛用于低排放燃气轮机燃烧室的火焰稳定。但是,对引燃火焰对动态不稳定性的影响知之甚少。在这项工作中,主要火焰与引燃火焰之间的动态相互作用是通过同时扰动两个火焰来进行研究的。双输入强制。燃烧器用于产生通过中央引燃火焰稳定的预混合轴心式V形甲烷火焰。伺服阀和警报器分别用于在引燃火焰和主火焰中产生强迫。诊断系统用于测量火焰结构和放热率。研究了强迫频率,强迫幅度,两个强迫信号之间的相位差以及雷诺数的影响。测量并分析了火焰传递函数(FTF)和火焰动态位置。发现总火焰响应可以通过引燃火焰中的扰动来改变。该机制可归因于引燃火焰对燃烧侧速度场的影响。发现涡旋能够在一定条件下放大飞行员的主要动力相互作用。基于线性化G方程开发了一个解析模型,以通过燃烧侧的速度扰动进一步了解火焰相互作用。在预测结果与实验结果之间找到了良好的一致性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号