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Optimization of active instability control using secondary fuel injection with model dump combustor.

机译:使用模型倾卸式燃烧器的二次燃料喷射优化主动失稳控制。

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摘要

Active control of combustion instability in a lean premixed dump combustor was studied by injecting secondary gaseous fuel into selected regions of the combustor. Two strong instabilities were sustained, for which main fuel was supplied partially premixed (case I) or fully premixed (case II), respectively. The structure of unstable flames was identified by taking phase-averaged images over one period of the instability and local Rayleigh index distributions were calculated using the images and pressure data. An examination of the local Rayleigh index distribution revealed that there are regions of driving and damping in unstable flames. It was suggested that to suppress the instability, secondary heat should be added in the local damping region to maximize the effect of control.; To investigate the effect of temporal and spatial secondary fuel distribution on the control effectiveness, both dump plane injection and upstream injection were applied to each of the two different instabilities. For case I instability, dump plane injection resulted in effective control and for case 11 instability upstream injection was effective.; For the case of controlling case I instability with dump plane injection, secondary heat was added in the damping region and the instability was suppressed at an optimal phase delay. For the case of controlling case II instability, instability was not suppressed since secondary heat was added out of phase with the pressure, but did not occur in the damping region. It was found that a control strategy such that secondary heat is added out of phase with the pressure, cannot always achieve successful suppression of instability unless it is accompanied by spatially optimized secondary heat release.; From the study of mode contribution of secondary heat release to damping, it was found that even though the injection is made at one of the sub-harmonics of the instability frequency, the greatest contribution is from a harmonic mode corresponding to the instability frequency. Therefore, tailoring the temporal heat release profile so that the harmonic component corresponding to the instability frequency was maximized resulted in performance improvement as shown in the case study.
机译:通过将二次气态燃料注入燃烧器的选定区域,研究了稀混合气预混合燃烧器中燃烧不稳定性的主动控制。持续存在两种严重的不稳定性,分别为燃料进行部分预混(情况I)或完全预混(情况II)。不稳定火焰的结构是通过在不稳定性的一个周期内拍摄相位平均图像来确定的,并使用图像和压力数据来计算局部瑞利指数分布。对局部瑞利指数分布的检查表明,不稳定火焰中存在一些驱动和阻尼区域。建议为抑制不稳定性,应在局部阻尼区域添加二次热,以最大程度地发挥控制效果。为了研究时间和空间二次燃料分配对控制有效性的影响,将倾卸面喷射和上游喷射均应用于两种不同的不稳定性。对于情况I不稳定,倾卸式飞机喷射导致有效控制,而对于情况11不稳定,上游喷射则有效。对于通过倾卸面喷射来控制情况I的不稳定性的情况,在阻尼区域中添加了二次热量,并以最佳的相位延迟抑制了不稳定性。对于控制情况II的不稳定性的情况,由于二次热与压力异相地添加,因此不抑制不稳定性,但是在阻尼区域中不发生。已发现,除非伴随着空间上优化的二次放热,否则控制策略(使二次热与压力异相添加)无法始终成功地抑制不稳定性。从二次热释放对阻尼的模式贡献的研究中发现,即使在不稳定频率的次谐波之一处进行注入,最大的贡献还是来自与不稳定频率相对应的谐波模式。因此,如案例研究所示,调整时间放热曲线以使对应于不稳定性频率的谐波分量最大化,从而导致性能提高。

著录项

  • 作者

    Kim, Kwanwoo.;

  • 作者单位

    The Pennsylvania State University.;

  • 授予单位 The Pennsylvania State University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 154 p.
  • 总页数 154
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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