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OPTIMIZED GLOBAL MECHANISMS FOR CFD ANALYSIS OF SWIRL-STABILIZED SYNGAS BURNER FOR GAS TURBINES

机译:优化燃气轮机旋流稳定合成气燃烧器CFD分析的全局机制

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A 3-step global reaction mechanism for a methane-air mixture is optimized against a detailed reference mechanism for perfectly stirred reactor (PSR) calculations. The global mechanism consists of three reactions corresponding to the fuel oxidation into CO and H_2O, and the CO - CO_2 equilibrium reaction. To ensure good agreement for rich conditions, correction functions that are dependent on the local equivalence ratio are introduced into the global mechanism. In a comparison of the optimized 3-step global reaction mechanism with the reference detailed reaction mechanism, GRI Mech 3.0, the results show that the gas temperature and emissions are reasonably well predicted for lean and rich conditions. The optimized 3-step global reaction scheme is adapted in the Computational Fluid Dynamics (CFD) analysis of a swirl-stabilized syngas burner, designed by Siemens Industrial Turbomachinery (SIT syngas burner) for gas turbines. The burner consists of a main premixed flame, a partially premixed pilot flame and a confined rich premixed lean flame which produces radicals that support both the pilot and the main flame. The CFD results are compared with experimental results obtained in an atmospheric version of the burner test rig at Lund University. Both steady-state Reynolds Averaged Navier Stokes (RANS) and hybrid Unsteady RANS/Large Eddy Simulation (URANS/LES) results were computed. The CFD results with the 3-step global reaction mechanism show good agreement with the experimental data on gas analysis and flame visualization, while the Westbrook Dryer 2-step (WD2) [2] and Meredith et al. [3] 3-step global reaction mechanisms failed in their predictions of the CO emissions downstream in the burner.
机译:针对完全搅拌反应器(PSR)计算的详细参考机制,优化了甲烷 - 空气混合物的3步全局反应机理。全局机制由对应于燃料氧化的三种反应组成CO和H_2O,以及CO-CO_2平衡反应。为确保富裕条件良好的协议,将依赖于本地等效率的校正功能引入全球机制。在优化的3步骤全局反应机理与参考详细反应机制,GRI MECH 3.0的比较中,结果表明,对贫民和富裕的条件相当良好地预测气体温度和排放。优化的3步全局反应方案适用于由西门子工业涡轮机(SIT合成气燃烧器)设计的旋流稳定的合成气燃烧器的计算流体动力学(CFD)分析。燃烧器由主要预混合的火焰,部分预混的飞行员和狭窄的富含预混贫火焰组成,产生支持飞行员和主火焰的自由基。将CFD结果与在隆德大学的燃烧器试验站的大气版本中获得的实验结果进行了比较。计算稳态雷诺平均均计算了Navier Stokes(RAN)和混合不稳定的RAN /大涡模拟(URAN / LES)结果。 CFD结果采用3步全局反应机制与天然气分析和火焰可视化的实验数据表现出良好的一致性,而威斯布鲁克干燥器2步(WD2)[2]和Meredith等。 [3] 3步骤全球反应机制在燃烧器下游的共同排放的预测中失败。

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