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HYDRODYNAMIC SUPPRESSION OF SOOT FORMATION IN LAMINAR COFLOWING JET DIFFUSION FLAMES

机译:层状CoFlowing射流扩散火焰中烟灰形成的流体动力学抑制

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Effects of flow (hydrodynamic) properties on limiting conditions for soot-free laminar non-premixed hydrocarbon/air flames (called laminar soot-point conditions) were studied, emphasizing non-buoyant laminar coflowing jet diffusion flames. Effects of air/fuel-stream velocity ratios were of particular interest; therefore, the experiments were carried out at reduced pressures to minimize effects of flow acceleration due to the intrusion of buoyancy. Test conditions included reactant temperatures of 300 K; ambient pressures of 3.7-49.8 kPa; methane-, acetylene-, ethylene-, propane-, and methane-fueled flames burning in coflowing air with fuel-port diameters of 1.7, 3.2, and 6.4 mm; fuel jet Reynolds numbers of 18-121; air coflow velocities of 0-6 m/s; and air/fuel-stream velocity ratios of 0.003-70. Measurements included laminar soot-point flame lengths, laminar soot-point fuel flow rates, and laminar liftoff conditions. The measurements show that laminar soot-point flame lengths and fuel flow rates can be increased, broadening the range of fuel flow rates where the flames remain soot free, by increasing air/fuel-stream velocity ratios. The mechanism of this effect involves the magnitude and direction of flow velocities relative to the flame sheet where increased air/fuel-stream velocity ratios cause progressive reduction of flame residence times in the fuel-rich soot-formation region. The range of soot-free conditions is limited by both liftoff, particularly at low pressures, and the intrusion of effects of buoyancy on effective air/fuel-stream velocity ratios, particularly at high pressures. Effective correlations of laminar soot- and smoke-point flame lengths were also found in terms of a corrected fuel flow rate parameter, based on simplified analysis of laminar jet diffusion flame structure. The results show that laminar smoke-point flame lengths in coflowing air environments are roughly twice as long as soot-free (blue) flames under comparable conditions due to the presence of luminous soot particles under fuel-lean conditions when smoke-point conditions are approached. This is very similar to earlier findings concerning differences between laminar smoke- and soot-point flame lengths in still environments.
机译:研究了流动(流体动​​力学)性能对无苏波层的无预混合烃/空气火焰(称为层状烟灰点状况)的限制条件的影响,强调了非浮标层状CoFlowing射流扩散火焰。空气/燃料流速度比的影响特别感兴趣;因此,在减少压力下进行实验,以最小化由于浮力的侵入引起的流动加速的影响。试验条件包括300 k的反应物温度; 3.7-49.8 KPA的环境压力;在CoFlowing空气中燃烧的甲烷,乙炔,乙烯,丙烷和甲烷燃料火焰,燃料端口直径为1.7,3.2和6.4mm;燃料喷射雷诺数为18-121;空气coflow速度为0-6米/秒;和空气/燃料流速度比0.003-70。测量包括层压烟灰点火焰长度,层状烟点燃料流速和层流升空条件。测量结果表明,通过增加空气/燃料流速度比,可以增加层状烟灰点火焰长度和燃料流速,扩大火焰自由保持烟雾的燃料流速范围。这种效果的机制涉及相对于火焰片的流速的大小和方向,其中增加的空气/燃料流速度比率导致富含燃料烟灰形成区域中的火焰停留时间的逐渐降低。无烟灰条件的范围受到升降机的限制,特别是在低压下,浮力对有效空气/燃料流速比率的影响,特别是在高压下。基于层流射流扩散火焰结构的简化分析,还以校正的燃料流速参数发现了层状烟灰和烟雾点火焰长度的有效相关性。结果表明,由于在接近烟点条件下的燃料稀释条件下的烟雾稀释条件下,CoFlowing空气环境中的层状烟点火焰长度大致两倍。 。这与仍然存在静止环境中的层流烟雾和烟尘烟雾长度之间的差异非常相似。

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