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Understanding the Effect of Inhomogeneous Mixing on Knocking Characteristics of Iso-Octane by Using Rapid Compression Machine

机译:了解快速压缩机通过快速压缩机突然混合对异辛烷爆震特性的影响

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As fuel injection strategies in spark-ignition (SI) engines have been diversified, inhomogeneous mixing of the fuel-air mixture can occur to varying extents during mixture preparation. In this study, we analyzed the effect of inhomogeneous mixing on the knocking characteristics of iso-octane and air mixture under a standardized fuel testing condition for research octane number (RON), based on ASTM D2699. For this purpose, we assumed that both lean spots and rich spots existed in unburned gas during compression stroke and flame propagation and calculated the thermodynamic state of the spots by using an in-house multi-zone, zero-dimensional SI engine model. Then, the ignition delay was measured over the derived thermodynamic profiles by using rapid compression machine (RCM), and we calculated ξ, the ratio of sound speed to auto-ignition propagation speed, based on Zel’dovich and Bradley’s ξ - ε theory to estimate knock intensity. As a result, we discovered that lean spots would have higher reactivity than stoichiometric mixture (ξ > 0), while rich spots would not (ξ < 0); thus, knocking has more tendency to be initiated from a lean spot. For further analysis, ξ was divided into two terms, ξT for temperature gradient and ξ_Φ for equivalence ratio gradient, and each term was evaluated separately. At a lean spot, ξ_T is generally positive because temperature is higher than that of stoichiometric mixture due to smaller fuel charge cooling and higher specific heat ratio of the mixture. On the other hand, ξ_Φ is negative but rapidly converges to zero as flame propagates; thus, ξ is determined dominantly by ξ_T. In addition, ξ from various spot radii and steepness of gradient were compared to analyze the effect of spot structure on knock intensity. As a result, we found that a steeper gradient of equivalence ratio leads to a weaker knock intensity, while the effect of radius change is negligible.
机译:如在火花点火燃料喷射策略(SI)发动机已经多样化,燃料 - 空气混合物的不均匀混合可以发生到混合物制备过程中不同程度。在这项研究中,我们分析了不均匀混合对异辛烷和空气混合物的爆燃特性的影响的标准化测试燃料条件研究法辛烷值(RON)下,根据ASTM D2699。为此,我们假设两个瘦点和丰富的点压缩行程和火焰传播过程中未燃烧的气体存在,通过使用一个内部的多区域,零维SI发动机模型计算出的点的热力学状态。然后,点火延迟经衍生热力学谱通过使用快速压缩机(RCM)测量,并且我们计算ξ,声速的至自动点火传播速度之比,基于泽尔多维奇和布拉德利的ξ - ε理论估计爆震强度。其结果是,我们发现,贫斑点将具有比化学计量的混合物(ξ> 0)更高的反应性,同时富含斑点不会(ξ<0);因此,敲必须从瘦点开始更倾向。进行进一步的分析,ξ被分成两个方面,对ξT温度梯度和ξ_Φ为当量比梯度,并且每个术语分别进行评估。在贫点,ξ_T通常是正的,因为温度低于化学计量的混合物的更高由于较小的燃料进气冷却,并将该混合物的更高的比热比。在另一方面,ξ_Φ是负但迅速收敛到零作为火焰传播;因此,ξ是由ξ_T支配性地决定。另外,来自各种点的半径和梯度的陡度ξ进行比较,以分析点结构对爆震强度的效果。其结果是,我们发现,当量比引线的较陡的梯度,以较弱的爆震强度,而半径变化的影响是微不足道的。

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