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Combustion Recession after End of Injection in Diesel Sprays

机译:柴油喷雾剂喷射结束后的燃烧衰退

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This work contributes to the understanding of physical mechanisms that control flashback, or more appropriately combustion recession, in diesel sprays. A large dataset, comprising many fuels, injection pressures, ambient temperatures, ambient oxygen concentrations, ambient densities, and nozzle diameters is used to explore experimental trends for the behavior of combustion recession. Then, a reduced-order model, capable of modeling non-reacting and reacting conditions, is used to help interpret the experimental trends. Finally, the reduced-order model is used to predict how a controlled ramp-down rate-of-injection can enhance the likelihood of combustion recession for conditions that would not normally exhibit combustion recession. In general, fuel, ambient conditions, and the end-of-injection transient determine the success or failure of combustion recession. The likelihood of combustion recession increases for higher ambient temperatures and oxygen concentrations, as well as for higher reactivity fuels. The likelihood of combustion recession was further linked to the characteristics of end-of-injection entrainment. A simple equation, linking equivalence ratio at the lift-off length, φ(LOL), with a dimensionless parameter related to the end-of-injection entrainment wave, was found to well predict the propensity for combustion recession of dodecane sprays over a wide range of experimental data and 1-D model predictions. Our results suggest that this relationship is φ(LOL) ~ D_(eff)/(αU_(eff))~(0.474), where D_(eff) is the effective orifice diameter, α is the end-of-injection ramp-down duration, and U_(eff) is the effective injection velocity.
机译:这项工作有助于理解控制柴油喷雾中回火或更合适的燃烧后退的物理机制。包含许多燃料,喷射压力,环境温度,环境氧气浓度,环境密度和喷嘴直径的大型数据集用于探索燃烧衰退行为的实验趋势。然后,使用能够建模非反应和反应条件的降阶模型来帮助解释实验趋势。最后,降阶模型用于预测在正常情况下不会表现出燃烧后退的情况下,受控的下降斜率喷射可以如何提高燃烧后退的可能性。通常,燃料,环境条件和喷射结束瞬态决定燃烧衰退的成败。对于较高的环境温度和氧气浓度以及较高的反应性燃料,燃烧后退的可能性增加。燃烧后退的可能性还与喷射结束夹带的特征有关。发现了一个简单的方程式,该方程将提升长度处的当量比φ(LOL)与与喷射结束夹带波有关的无量纲参数联系起来,可以很好地预测十二烷喷雾在大范围内燃烧后退的可能性。实验数据和一维模型预测的范围。我们的结果表明该关系为φ(LOL)〜D_(eff)/(αU_(eff))〜(0.474),其中D_(eff)是有效孔口直径,α是注入结束时的斜降持续时间,U_(eff)是有效注射速度。

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