首页|弱旋预混火焰中热声振荡多模态转换的实验与模拟研究

弱旋预混火焰中热声振荡多模态转换的实验与模拟研究

Experimental and numerical investigations on multi-mode hopping of thermoacoustic instability in a weak swirling premixed flame

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为研究弱旋预混火焰在当量比变化过程中热声不稳定的频率迁移、模态转换特征及内在机理,通过傅里叶变换、相空间重构、OH*时序及平均火焰图像等方法对实验中出现的极限环、拍振、间歇性振荡等典型燃烧不稳定状态进行分析;结合低阶热声网络与n-τ模型,对热声振荡过程中发生的模态转换现象进行模拟,其中延迟时间τ使用了对流延迟时间进行近似,其基于未燃混合物长度计算得到.实验结果表明,在当量比φ=0.5~0.7内,随着当量比的增加,一阶振荡频率向更高频率迁移;在φ=0.8时,振荡主频从一阶模态转换到二阶模态;φ=0.9~1.2内,一阶振荡频率降低,变化幅度最高达41.48%;并且当φ=1.1时,振荡主频从二阶模态转换回一阶模态;在整个当量比区间内,二阶振荡频率变化幅度小于5%.计算结果显示,振荡频率的预测值与实验值整体吻合良好,尤其是当φ=0.8时,二阶频率的增长率大于一阶频率的增长率,对应实验中发生的一阶模态到二阶模态的转换.同时在部分工况下,预测的振荡频率与实验值也有偏移,其原因是增益的增加导致偏离增大,一阶频率的最大误差为26.4%,二阶频率的最大误差小于12%.本研究表明,对流延迟时间与振荡主频的分布存在反比关系,对流延迟时间的缩短会使得一阶频率向高频迁移,过程中振荡模态会由一阶转换到二阶模态.
In order to investigate the frequency shift,mode hopping characteristics and mechanisms of ther-moacoustic instability in a premixed weak swirling burner as the equivalence ratio changes,different combustion states,such as limit cycles,beating oscillations and intermittent oscillations,are identified and analyzed using Fourier transform,phase space reconstruction,OH* time series and average flame images.The"mode hopping"phenomena occurring in the process of thermoacoustic oscillations are simulated by combining the low-order ther-moacoustic network with the n-τ model,where the delay time τ is approximated by the convective delay time cal-culated based on the length of the unburned mixture.Experimental results show that the first-order frequency in-creases with increasing equivalence ratio(φ)in the range of 0.5~0.7.At φ=0.8,the dominant frequency switches from the first to the second-order mode.Furthermore,for φ within the range of 0.9~1.2,the first-order frequency decreases,resulting in a change of up to 41.48%.For a ratio of φ=1.1,the dominant frequency switches from the second to the first-order mode.The second-order frequency varies by less than 5%over the entire equivalence ra-tio interval.The simulation results are in agreement with the experimental tests,especially at φ=0.8,the growth rate of the second-order frequency exceeds that of the first-order,leading to mode hopping occurred in the exper-iments.Meanwhile,in some conditions,the predicted oscillation frequency also deviates from the experimental results a little bit,due to the increase in gain leading to an increase in deviation.The maximum error between the numerical and experimental results is about 26.4%for the first-order frequency and less than 12%for the sec-ond-order frequency.The current work shows that there is an inverse relationship between the convective delay time and the dominant frequency,which means reducing the convective delay time causes the first-order frequen-cy to shift to the higher frequency,and the instability modes switch from first-order to second-order modes in the process.

Gas turbine combustorCombustion instabilitiesThermoacoustic instabilitiesTher-moacoustic couplingConvection delay timeLow-order thermoacoustic networkMode hopping

陆世康、季晨振、王萌铭、潘登、朱彤

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同济大学 机械与能源工程学院,上海 201800

燃气轮机燃烧室 燃烧不稳定 热声振荡 热声耦合 对流延迟时间 低阶热声网络 模态转换

2025

推进技术
航天科工集团公司三十一研究所

推进技术

北大核心
影响因子:0.631
ISSN:1001-4055
年,卷(期):2025.46(1)