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Combustion Instabilities With Different Degrees of Premixedness in a Separated Dual-Swirl Burner

机译:具有分离双旋光器中不同程度的预混合的燃烧不稳定性

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摘要

The effects of premixedness degrees on combustion instabilities of separated dual-swirl flames have been investigated experimentally in the Beihang Axial Swirler Independently Stratified (BASIS) burner. The degree of premixedness is modulated by the fuel split between two injection positions in the outer stream. In the spectra of pressure oscillations, both the frequency and amplitude are positively correlated with fuel split ratios under partially premixed conditions, and the mode transition between perfectly and partially premixed conditions has been observed. The location of perfectly premixed flames shows no obvious variation at different phase angles, only with a slightly wrinkling of the flame surface along the shear layer. Under partially premixed conditions, however, the flame is found to feature a large-scale periodic convective motion, accompanied by the obvious variation of heat releases due to the equivalence ratio oscillations. The local Rayleigh index map compares the thermoacoustic driving factors under perfectly and partially premixed conditions. The development of above convective motions under partially premixed conditions is explained by combining the variations of pressure oscillations and heat releases. An analysis of the thermoacoustic network and convective path is applied to explain the cause of the mode transition. The results show that the appearance of equivalence ratio oscillations and the elongated convective path under partially premixed conditions brings a longer delay time of the flame response, which could be the reason for the mode transition.
机译:预热度对分离的双旋风火焰的燃烧不稳定性的影响已经通过实验研究了北港轴向旋流器独立分层(基础)燃烧器。预混合程度由燃料在外部流中的两个注射位置之间分开来调节。在压力振荡的光谱中,频率和幅度都与部分预混合条件下的燃料分裂比呈正相关,并且已经观察到完全和部分预混合的条件之间的模式转变。完美预混的火焰的位置显示不同相位角的明显变化,仅在沿剪切层略微皱起火焰表面。然而,在部分预混合的条件下,发现火焰具有大规模的周期性对流运动,伴随着由于等效比振荡引起的热释放的明显变化。本地Rayleigh索引图在完全和部分预混合的条件下比较了热声驾驶因子。通过组合压力振荡和热释放的变化来解释部分预混条件下的上述对流运动的发展。应用热声网络和对流路径的分析来解释模式过渡的原因。结果表明,在部分预混合条件下的等效比振荡和细长的对流路径的外观带来了火焰响应的延迟时间,这可能是模式转变的原因。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2020年第6期|061012.1-061012.10|共10页
  • 作者单位

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics School of Energy and Power Engineering Beihang University Beijing 100083 China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics School of Energy and Power Engineering Beihang University Beijing 100083 China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics School of Energy and Power Engineering Beihang University Beijing 100083 China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics School of Energy and Power Engineering Beihang University Beijing 100083 China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics School of Energy and Power Engineering Beihang University Beijing 100083 China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics School of Energy and Power Engineering Beihang University Beijing 100083 China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics School of Energy and Power Engineering Beihang University Beijing 100083 China;

    Department of Mechanical Engineering Imperial College London London SW7 2AZ UK;

    Department of Mechanical Engineering University of Connecticut Storrs Mansfield CT 06269;

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