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EFFECT OF THE DIFFUSER ON THE INLET ACOUSTIC BOUNDARY IN COMBUSTION-ACOUSTIC COUPLED OSCILLATION

机译:扩散器对燃烧声耦合振荡中入口声边界的影响

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Combustion instability is one of the major challenges in Lean Premixed Pre-vaporized (LPP) combustion technology. The effect of inlet conditions on combustion instability has been widely studied. But the diffuser, located between the compressor outlet and combustor inlet, has received little attention regarding its effect on combustion instability. This paper experimentally investigated the combustion instability in a single sector LPP combustor with and without a diffuser. Pressure data has been recorded and used to indicate the oscillation of the system. The results show that with the diffuser the combustor showed no prominent oscillation, and strong thermoacoustic oscillation at around 400 Hz was observed without the diffuser. Further analysis has been conducted by using acoustic net model. The resonant mode frequency of the entire combustor system and each section separately were calculated. It was found that in the case of the diffuser, the resonant frequency shifted from 400 Hz to 453 Hz, which avoiding interacting with heat release within the flame tube, thus help to stabilize the combustor system.
机译:燃烧不稳定是精益预混蒸发(LPP)燃烧技术中的主要挑战之一。入口条件对燃烧不稳定性的影响已被广泛研究。但是,位于压缩机出口和燃烧器入口之间的漫射器已经注意到其对其对燃烧不稳定的影响。本文通过漫射器实验研究了单个扇区LPP燃烧器中的燃烧不稳定。已记录压力数据并用于指示系统的振荡。结果表明,随着扩散器,燃烧器没有显示出突出的振荡,并且在没有扩散器的情况下观察到大约400Hz的强大热声振荡。通过使用声学网模型进行了进一步的分析。计算整个燃烧器系统的谐振模式频率和分别的每个部分。发现,在扩散器的情况下,谐振频率从400Hz到453Hz移位,这避免了在火焰管内与热释放相互作用,因此有助于稳定燃烧器系统。

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