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Transverse fuel jet in turbulent cross-flow: influence of fuel composition on near field flame stabilization

机译:湍流交叉流动中的横向燃料喷射:燃料组合物对近场火焰稳定的影响

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Compressible three-dimensional direct numerical simulations (DNS) of transverse fuel jet in turbulent boundary layer cross-flow of air (JICF) are performed to gain fundamental insight into the influence of fuel composition on the near field flame stabilization characteristics. A transverse jet of synthesis gas fuel, diluted by 30% nitrogen by volume, at 420 K is injected from a circular nozzle of 1 mm diameter with a bulk velocity of 250 m/s into a turbulent cross-flow of air at 750 K and free stream velocity of 55 m/s, representing nominal conditions of the premixer section of stationary gas-turbines. The aim is to develop an understanding of those mechanisms that are critical to flame stabilization in this configuration and aid the design of gas turbine burners that are fuel-flexible and intrinsically flashback-safe. The DNS incorporates detailed chemical kinetics and mixture-averaged transport properties. A chemical mechanism involving 12 species and 29 reaction steps is considered and three fuel fuel compositions with varying ratios of H_2:CO mole fractions are investigated: 1:0 (pure H_2), 1:0.06 (H_2 rich) and 1:1 (H_2 lean). The laminar flame speeds for the three mixtures at nominal conditions (stoichiometric mixture, unburnt temperature of 420 K) are in the ratio 1:0.93:0.49 respectively. In spite of the large difference in the laminar propagation speeds the flame stabilizes on average at roughly the same location in all three cases: 1 mm downstream of the nozzle center in the stream wise direction and 4 mm downstream in the wall-normal direction. This location corresponds to a region of low velocity magnitudes and near stoichiometric mixtures. The dilatational influence of the flame on the turbulent flow field is likely the same in the three cases since the density ratios for the three mixtures are roughly equal to 4.5. Significant differential diffusion effects are observed with the elemental mixture fraction of hydrogen being much larger than carbon in the vicinity of the flame anchoring region. This suggests that the influence of adding CO in the fuel stream is negated somewhat by differential diffusion which continually provides an excess of H_2 to the flame compared to CO, relative to the fuel stream.
机译:在空气(JICF)的紊流边界层横流横向燃料射流的可压缩三维直接数值模拟(DNS)被执行,以获得基本洞察燃料组合物在近场火焰稳定特性的影响。合成气燃料的横向射流,由30%的氮气稀释的体积,在420 K从直径为1mm的具有250μm的整体速度的圆形喷嘴喷射/ s的进入空气中的750 K A湍流横流和55米/秒自由流速度,代表固定式燃气涡轮机的预混合区的标称条件。的目的是开发那些对火焰稳定临界在这种配置和辅助燃气涡轮燃烧器是燃料的柔性本质和回火安全的设计机制的理解。的DNS结合详述化学动力学和混合物平均传输性质。涉及12种和29个的反应步骤的化学机制被认为与具有不同H_2的比率三个燃料的燃料组合物:CO摩尔分数进行了研究:1:0(纯H_2),1:0.06(H_2丰富)和1:1(H_2倾斜)。层流火焰速度在标称条件下的三种混合物(化学计量的混合物,420的K未燃烧温度)处于比为1:0.93:0.49分别。尽管在层传播的大的差异的速度平均火焰稳定在大致在所有三种情况下相同的位置:在流方向上喷嘴中心的下游1mm,并且在壁法线方向下游为4mm。此位置对应于低速大小和接近化学计量的混合物的区域。在紊流场火焰的疏密的影响很可能在三种情况下,同样由于用于三种混合物的密度比大致等于4.5。显著差扩散效应与氢比在火焰锚定区域的附近碳大得多的元素混合物级分中观察。这表明,在燃料流中添加CO的影响是由相对于燃料流差动扩散相比CO其连续提供过量的H_2到火焰,有些否定。

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