Influence of fuel plenum on thermoacoustic oscillations inside a swirl combustor

被引:15
|
作者
Chen, Zhi X. [1 ]
Swaminathan, Nedunchezhian [1 ]
机构
[1] Univ Cambridge, Dept Engn, Cambridge CB2 1PZ, England
基金
英国工程与自然科学研究理事会; 欧盟地平线“2020”;
关键词
Large Eddy Simulation; Fuel plenum; Swirl combustor; Thermoacoustic oscillations; Self-excited instability; LARGE-EDDY SIMULATION; TURBULENT PREMIXED FLAMES; TURBINE MODEL COMBUSTOR; NONLINEAR RESPONSE; AZIMUTHAL MODES; INSTABILITY; DYNAMICS; PREDICTION;
D O I
10.1016/j.fuel.2020.117868
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Large eddy simulation (LES) of a lean methane/air flame exhibiting self-excited thermoacoustic oscillations inside a swirl combustor is performed. The influence of fuel plenum on the combustor dynamics is studied. The velocity, temperature and mixture fraction statistics computed from the two LES cases are compared with the measurements. The results show good overall agreement for both cases with slight improvements by including the fuel plenum. In particular, the near-field mixing and flame lift-off height are captured more accurately. The dominant unstable Helmholtz frequency (approximate to 270 Hz) computed by including the plenum is closer to the measured value (approximate to 290 Hz) compared to that (approximate to 250 Hz) obtained without the plenum. Mode shape analysis shows that including the fuel plenum is necessary for obtaining the phase difference between the pressure oscillations in the combustion chamber and air plenum. It is also found that self-excited oscillations are amplified with an increase by 6% in the mean Rayleigh index and 50% in the gain of the flame transfer function due to the equivalence ratio fluctuations when the fuel plenum is included.
引用
收藏
页数:13
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