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首页> 外文期刊>Combustion Science and Technology >EFFECTS OF NONUNIFORM REACTANT STOICHIOMETRY ON THERMOACOUSTIC INSTABILITY IN A LEAN-PREMIXED GAS TURBINE COMBUSTOR
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EFFECTS OF NONUNIFORM REACTANT STOICHIOMETRY ON THERMOACOUSTIC INSTABILITY IN A LEAN-PREMIXED GAS TURBINE COMBUSTOR

机译:非均匀反应化学计量法对贫油燃气轮机燃烧器热声不稳定性的影响

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Detailed experimental investigations of the amplitude dependence of flame describing Junctions (FDF) were performed using a stratified swirl-stabilized combustor, in order to understand the combustion-acoustic interactions of CHjIair flames propagating into nonhomogeneous reactant stoichiometry. Phase-synchronized OH planar laser induced fluorescence (OH PLIF) measurements were used to investigate local reaction zone structures of forced flames. To determine the amplitude- and frequency-dependent forced flame response, simultaneous measurements of inlet velocity and heat release rate oscillations were made using a constant temperature anemometer andphotomultiplier tubes with narrow-band OH'ICH* interference filters. The measurements were made over a wide range of stratification ratios, including inner stream enrichment (φ_1 > φ_0) and outer stream enrichment ((φ_0 > φ_1) conditions, and compared to the baseline condition of spatially and temporally homogeneous cases (φ_1 = φ_0). Results show that for the inlet conditions investigated, fuel stratification has a significant influence on local and global flame structures of unforced and forced flames. Under stratified conditions, length scales of local contours were found to be much larger than the homogeneous case due to high kinematic viscosities associated with high temperature. Stratification has a remarkable effect on flame-vortex interactions when the flame is subjected to high-amplitude acoustic forcing, leading to different evolution patterns of FDF (amplitude and disturbance convective time) in response to the amplitude of the imposed inlet velocity oscillation. The present experimental investigation reveals that intentional stratification has the potential to eliminate or suppress the occurrence of detrimental combustion instability problems in lean-premixed gas turbine combustion systems.
机译:使用分层旋流稳定的燃烧器对描述结点(FDF)的火焰的幅度依赖性进行了详细的实验研究,以了解传播到非均相反应化学计量的CHiIair火焰的燃烧声相互作用。相同步OH平面激光诱导荧光(OH PLIF)测量用于研究强制火焰的局部反应区结构。为了确定振幅和频率相关的强制火焰响应,使用恒温风速计和带有窄带OH'ICH *干涉滤光片的光电倍增管,同时测量入口速度和放热速率振荡。在广泛的分层比率范围内进行测量,包括内部流富集(φ_1>φ_0)和外部流富集((φ_0>φ_1)条件),并将其与时空均一的情况的基线条件进行比较(φ_1=φ_0)结果表明,在所研究的进气条件下,燃料分层对非强迫和强迫火焰的局部和整体火焰结构有显着影响,在分层条件下,由于高度高,局部轮廓的长度尺度远大于均质情况与火焰有关的运动粘度当火焰经受高振幅声强迫时,分层对火焰-涡旋相互作用有显着影响,导致响应于振幅的FDF的不同演化方式(振幅和扰动对流时间)。目前的实验研究表明,故意分层h作为消除或抑制有害预混合气燃气轮机燃烧系统中有害燃烧不稳定性问题发生的潜力。

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