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Soot in diesel fuel jets: effects of ambient temperature, ambient density, and injection pressure

机译:柴油喷气发动机中的烟尘:环境温度,环境密度和喷射压力的影响

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Measurements of soot distributions in fuel jets injected into high-temperature, high-pressure diesel-like operating conditions were made in an optically accessible constant-volume combustion vessel. A laser-extinction technique was used to make quantitative measurements of path-length-averaged soot volume fraction. Flame luminosity and planar laser-induced incandescence imaging were used to visualize the sooting region of the fuel jet. Flame lift-off lengths were also measured and used in the interpretation and analysis of the soot measurements. Fuel was injected with a common-rail diesel fuel injector equipped with a single 100-μm-diameter orifice. The fuel used was #2 diesel fuel. The matrix of experimental conditions included ambient gas temperatures from 850 to 1300 K, ambient gas densities from 7.3 to 30.0 kg/m~3, and injection pressures from 43 to 184 MPa. The results show that peak soot level in a fuel jet increases with increasing ambient gas temperature, with the increase scaling linearly with temperature. However, near the tip of the flame, the soot levels decrease with increasing ambient temperature, indicating significantly higher soot oxidation rates in the flame-tip region at higher temperatures. The results also show that the peak soot level in a fuel jet increases with increasing ambient gas density and decreasing injection pressure. The increase with increasing ambient density is nonlinear with respect to density. The increase with decreasing injection pressure is linear with decreasing injection velocity (or the square root of the pressure drop across the injector orifice). Overall, the trends observed in diesel fuel jet soot closely correlate with the cross-sectional average equivalence ratio at the lift-off length, with soot levels decreasing as the equivalence ratio decreases (i.e., as more air entrainment and mixing of fuel and air occur upstream of the lift-off length). Published by Elsevier Inc. on behalf of The Combustion Institute.
机译:在光学上可访问的恒定容积燃烧容器中,对注入高温,高压柴油状工作条件的喷油嘴中的油烟分布进行了测量。使用激光消光技术对光程平均烟灰体积分数进行定量测量。火焰发光度和平面激光诱导的白炽成像用于可视化燃料喷射的烟the区域。还测量了火焰剥离长度,并将其用于烟尘测量的解释和分析。使用配备有单个100-μm直径孔的共轨柴油喷油器喷射燃油。使用的燃料是2号柴油。实验条件的矩阵包括:环境气体温度为850至1300 K,环境气体密度为7.3至30.0 kg / m〜3,注入压力为43至184 MPa。结果表明,燃料射流中的烟灰峰值水平随环境气体温度的升高而增加,且随温度的升高呈线性比例变化。但是,在火焰尖端附近,烟灰水平随环境温度升高而降低,这表明在较高温度下,火焰尖端区域的烟灰氧化速率明显更高。结果还表明,随着环境气体密度的增加和喷射压力的降低,燃料喷射中的烟灰峰值水平增加。随着环境密度的增加,这种增加相对于密度是非线性的。随着注射压力的降低,该增加与注射速度的降低(或整个注射孔的压降的平方根)成线性关系。总体而言,在喷射长度上,柴油机喷气烟尘中观察到的趋势与横截面平均当量比密切相关,当当量比减小时,烟灰含量降低(即,随着更多的空气夹带和燃料与空气的混合发生)提升长度的上游)。由Elsevier Inc.代表燃烧研究所出版。

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