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Development of a two-part n-heptane oxidation mechanism for two stage combustion process in internal combustion engines

机译:用于内燃机两段燃烧过程的两部分正庚烷氧化机理的开发

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This paper presents an attempt to build a very reduced kinetics mechanism of n-heptane to simulate the two stage ignition process in terms of ignition delay time and in-cylinder pressure profiles over the whole range of engine operations. Starting from the previous 26 reactions and 25 species mechanism, two reduced schemes have been developed, one with 18 reactions and 19 species and the other with 13 reactions and 14 species. The reduction step shows that when the reactions describing the first stage are reduced as in the 18-step model, the accuracy is poor. The second 13-step model, where the reaction path describing the low temperature period has been kept, is more reliable when the window of engine operations is restricted. From this reduction step, a two-part reaction mechanism linked with a temperature criterion has been developed, while maintaining a wide range of engine operating conditions. This mechanism includes a low temperature reaction group and a high temperature reaction group, linked with a transition temperature correlation. Ignition delay times calculated with the two-part model are compared to those from the detailed mechanism. In addition, the comparison of the Indicated Mean Effective Pressure (IMEP) with the results of the previous 26-step mechanism has been done. The results obtained with the present model are in good agreement with the 26-step one. Moreover, this model has a very short computational time and thus could be used in CFD simulations as well as single zone or multi-zone engine models, and also model-based design. (C) 2017 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:本文提出了一种尝试建立正庚烷动力学机制的简化方法,以模拟整个发动机操作范围内的点火延迟时间和缸内压力曲线来模拟两阶段点火过程。从先前的26种反应和25种物种机制出发,已经开发出两种简化方案,一种具有18种反应和19种物种,另一种具有13种反应和14种物种。还原步骤表明,当像18步模型中那样还原描述第一阶段的反应时,准确性很差。当限制了发动机运行的窗口时,第二个13步模型(其中保留了描述低温时段的反应路径)更加可靠。通过该还原步骤,已经开发了与温度标准相关联的两部分反应机理,同时保持广泛的发动机工况。该机理包括与转变温度相关性关联的低温反应基团和高温反应基团。将由两部分模型计算的点火延迟时间与详细机制中的点火延迟时间进行比较。此外,已将指示平均有效压力(IMEP)与先前的26步机构的结果进行了比较。使用本模型获得的结果与26步模型非常吻合。此外,该模型的计算时间非常短,因此可用于CFD仿真以及单区域或多区域引擎模型以及基于模型的设计中。 (C)2017燃烧研究所。由Elsevier Inc.出版。保留所有权利。

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