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Flow reactor autoignition studies of iso-octane at high pressures and low-to-intermediate temperatures.

机译:高压和中低温度下异辛烷的流式反应器自燃研究。

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摘要

The trend in internal combustion engine and aviation gas turbine design is moving increasingly toward a computational approach, requiring well-validated chemical kinetics models. Autoignition delay measurements are among the key set of validation data used by chemical kinetics modelers. Autoignition is an ignition event that occurs when the mixture reaches conditions of temperature, pressure, and equivalence ratio such that the rate of chain branching exceeds the rate of chain termination. In this case there is no external ignition source, such as a spark or initiating flame. Iso-octane, the compound studied in this work, is one of the fuels used to establish the octane rating for gasoline. Recently it has become of further interest as a component in fuel mixtures referred to as surrogate fuel mixtures such as JP-8. These surrogate fuel mixtures consist of only a few compounds that behave chemically in a manner similar to a practical fuel.;Studies of autoignition of iso-octane were conducted in a high-pressure flow reactor. A novel methodology was employed in which the minimum equivalence ratio required for ignition was established for specific conditions of pressure, temperature, and residence time. Liquid iso-octane was spray injected into the products of a hydrogen/oxygen/argon preburner, and the resulting vaporized mixture was then rapidly mixed with air in the high-pressure flow reactor. Autoignition delay times were obtained at pressures of 15, 17.5, 20, and 22.5 atm, for a temperature range of 640-850 K. Residence times of approximately 70, 100, 125, 155, and 175 ms were investigated over equivalence ratios ranging from 0.25 to 0.8.;Very few previous iso-octane ignition delay studies have investigated the conditions included in the present study. However, the current experiments have some overlapping pressure and temperature conditions (15 atm and 650-850 K) with rapid compression machine experiments. The rapid compression machine results are all for stoichiometric mixtures, whereas the current results are for equivalence ratios ranging from 0.37-0.8. The results from this work are useful for model validation as they are consistent with trends from previous studies and extend into a range of pressures, temperatures, and equivalence ratios not previously investigated.;The onset of autoignition for all pressures occurred at approximately 640K. Trends in the results showed that as temperature increased, the threshold equivalence ratio decreased. As temperature increased further into the negative temperature coefficient (NTC) region, the threshold equivalence ratio increased with increasing temperature. The NTC behavior started at temperatures of approximately 700-725K and ended at approximately 775K. At temperatures above 775K, the threshold equivalence ratio again decreased with increasing temperature. Pressure also had a strong effect on ignition delay. For all conditions, as pressure increased the threshold equivalence ratio decreased.;Results were compared with two chemical kinetics models. Good agreement was shown with a model from Lawrence Livermore National Laboratory (LLNL) for the conditions studied in this work. The main discrepancy between the experimental and modeling results was the overprediction of the threshold equivalence ratio in the NTC region at the shorter ignition delay times. For example, at the residence time of 70 ms, a pressure of 15 atm, and temperature of 775 K, the threshold equivalence ratios found experimentally and by the model were 0.75 and 0.95, respectively. At the longest residence time of 175 ms at the same conditions of pressure (15 atm) and temperature (775 K), the threshold equivalence ratios found experimentally and by the model were much closer at 0.44 and 0.47, respectively. The second model from Chemical Reaction Engineering and Chemical Kinetics (CRECK) gave similar results as the experiment for the temperature at the onset of autoignition, but showed no presence of the NTC region that was observed experimentally and predicted by the LLNL model. Neither the LLNL nor CRECK model predicted autoignition below temperatures of 650 K.;The LLNL model was used to identify key reactions controlling ignition through reaction pathway and temperature sensitivity analyses for the conditions of this study. The results showed the importance of the location of H-atom abstraction from the iso-octane molecule in determining how reactions proceeded. H-atom abstraction from the tertiary site on iso-octane served to slow overall reactivity, while abstraction from the primary and secondary locations increased overall reactivity.
机译:内燃机和航空燃气轮机设计的趋势正日益趋向于一种计算方法,需要一种经过充分验证的化学动力学模型。自燃延迟测量是化学动力学建模人员使用的关键验证数据集之一。自燃是一种点火事件,当混合物达到温度,压力和当量比的条件,从而使链支化速率超过链终止速率时发生。在这种情况下,没有外部点火源,例如火花或起火火焰。异辛烷是这项工作中研究的化合物,是用于确定汽油辛烷值的燃料之一。近来,作为燃料混合物中被称为替代燃料混合物(例如JP-8)的组分,它引起了进一步的关注。这些替代燃料混合物仅由一些化学性质类似于实际燃料的化合物组成。异辛烷的自燃研究是在高压流动反应器中进行的。采用了一种新颖的方法,其中针对压力,温度和停留时间的特定条件确定了点火所需的最小当量比。将液态异辛烷喷雾注入氢气/氧气/氩气预燃烧器的产物中,然后在高压流动反应器中将生成的汽化混合物与空气快速混合。在640-850 K的温度范围内,自燃延迟时间是在15、17.5、20和22.5 atm的压力下获得的。在当量比范围为0.25至0.8 。;很少有以前的异辛烷点火延迟研究对本研究中包含的条件进行了研究。但是,当前的实验在快速压缩机实验中存在一些重叠的压力和温度条件(15个大气压和650-850 K)。快速压缩机的结果全部针对化学计量混合物,而当前结果针对的当量比范围为0.37-0.8。这项工作的结果与先前研究的趋势相一致,并扩展到先前未研究的压力,温度和当量比范围内,因此对于模型验证很有用;所有压力的自燃开始发生在大约640K。结果趋势表明,随着温度升高,阈值当量比降低。随着温度进一步升高到负温度系数(NTC)区域,阈值当量比随温度升高而增加。 NTC行为始于大约700-725K的温度,结束于大约775K的温度。在高于775K的温度下,阈值当量比再次随温度升高而降低。压力对点火延迟也有很大的影响。在所有条件下,随着压力的增加,当量当量比减小;将结果与两个化学动力学模型进行比较。劳伦斯·利弗莫尔国家实验室(LLNL)的模型对这项工作中研究的条件显示出良好的一致性。实验结果与模型结果之间的主要差异是在较短的点火延迟时间下,NTC区域中的阈值当量比的过高预测。例如,在70 ms的停留时间,15 atm的压力和775 K的温度下,通过实验和模型发现的阈值当量比分别为0.75和0.95。在相同的压力(15个大气压)和温度(775 K)的条件下,最长停留时间为175 ms,通过实验和模型发现的阈值当量比分别接近0.44和0.47。来自化学反应工程和化学动力学(CRECK)的第二个模型给出了与自燃开始时的温度相似的结果,但没有显示通过LLNL模型进行实验观察和预测的NTC区域的存在。 LLNL和CRECK模型均未预测温度低于650 K时的自燃。LLNL模型用于确定通过本研究条件的反应途径和温度敏感性分析来控制点火的关键反应。结果表明,从异辛烷分子中提取H原子的位置对于确定反应的进行方式非常重要。从异辛烷上的叔位提取H原子可减慢总反应性,而从主要和次要位置提取H原子可提高总反应性。

著录项

  • 作者单位

    The Pennsylvania State University.;

  • 授予单位 The Pennsylvania State University.;
  • 学科 Mechanical engineering.
  • 学位 Ph.D.
  • 年度 2012
  • 页码 227 p.
  • 总页数 227
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:43:55

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