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Experimental characterization of jet fuels under engine relevant conditions - Part 2: Insights on optimization approach for surrogate formulation

机译:发动机相关条件下喷气燃料的实验特性-第2部分:替代配方优化方法的见解

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摘要

Computational combustion modeling is an essential complementary tool to engine experiments and the combination of computational fluid dynamics and detailed chemical kinetics provides the promise for optimizing engine performance. However, predicting the effects of chemical and physical properties of fuels on engine performance is a great challenge since transportation fuels are composed of several hundreds to thousands of chemical species. Surrogates are simpler representations of real fuels and are comprised of selected species of known concentrations that exhibit combustion characteristics similar to those of the real fuels. In this paper, drawing from our previous work on surrogate formulations, we investigate the effects of surrogate components on the autoignition characteristics of conventional and alternative jet fuels, using a combination of experimental and modeling approaches. As target fuels, we analyzed a conventional jet fuel (Jet-A) and two alternative jet fuels (coal-derived IPK, natural-gas-derived S8). Experimental data on the properties of surrogate mixtures, such as liquid density and threshold sooting index, their combustion behaviors, together with those from their corresponding target real fuels are compared and analyzed using predictions obtained from the surrogate model. Results from a modified CFR engine show that the ignition reactivity of Jet-A and Sasol IPK surrogates are stronger than their target fuels, while the S8 surrogate displayed an ignition behavior very similar to the target S8. Results from a constant volume spray combustion chamber provided reasonable agreements between the surrogates and their target jet fuels in terms of physical and chemical ignition delay times and apparent heat release trends, with the S8 surrogate showing the best agreement. In addition, surrogate mixtures that were modified from the original Jet-A and IPK surrogates to achieve a better agreement with CFR experiments performed poorly when tested in a spray chamber. These results imply that the agreement between the behaviors of surrogates and real fuels in one device or in one condition does not guarantee similarity in other devices or in other conditions. This study also highlights the need for improvements in the current surrogate formulation methodologies to provide a more universal emulation of the autoignition behaviors of target transportation fuels.
机译:计算燃烧模型是发动机实验必不可少的补充工具,计算流体动力学和详细的化学动力学的结合为优化发动机性能提供了希望。但是,预测燃料的化学和物理性质对发动机性能的影响是一个巨大的挑战,因为运输燃料是由数百到数千种化学物质组成的。替代物是真实燃料的简单表示,由已知浓度的选定物质组成,这些物质表现出与真实燃料相似的燃烧特性。在本文中,从我们先前关于替代物配方的工作中汲取了经验,我们结合实验和建模方法,研究了替代物成分对常规和代用喷气燃料自燃特性的影响。作为目标燃料,我们分析了传统的喷气燃料(Jet-A)和两种替代的喷气燃料(煤衍生的IPK,天然气衍生的S8)。使用替代模型获得的预测结果,对替代混合物特性的实验数据进行了比较和分析,这些替代数据包括液体密度和阈值烟ing指数,其燃烧行为以及来自其相应目标真实燃料的燃烧行为。改进的CFR发动机的结果表明,Jet-A和Sasol IPK替代物的点火反应性强于其目标燃料,而S8替代物的点火行为与目标S8非常相似。在物理和化学点火延迟时间以及明显的放热趋势方面,恒定体积喷雾燃烧室的结果提供了代用品与其目标喷气燃料之间的合理协议,其中S8代用品显示出最佳协议。另外,从原始Jet-A和IPK改性而来的替代混合物与在雾化室中进行测试时表现差的CFR实验取得了更好的一致性。这些结果表明,一种设备或一种条件下替代燃料和实际燃料的行为之间的一致性不能保证其他设备或其他条件下的相似性。这项研究还强调需要改进当前的替代配方方法,以提供对目标运输燃料自燃行为的更通用仿真。

著录项

  • 来源
    《Fuel》 |2019年第1期|1405-1416|共12页
  • 作者单位

    Univ Michigan, Dept Chem Engn, 2300 Hayward St, Ann Arbor, MI 48109 USA;

    Hongik Univ, Dept Mech & Syst Design Engn, 94 Wausan Ro, Seoul 04066, South Korea;

    Penn State Univ, Dept Energy & Mineral Engn, EMS Energy Inst, University Pk, PA 16802 USA;

    Univ Michigan, Dept Mech Engn, 2350 Hayward St, Ann Arbor, MI 48109 USA;

    Univ Michigan, Dept Chem Engn, 2300 Hayward St, Ann Arbor, MI 48109 USA|Univ Michigan, Dept Mech Engn, 2350 Hayward St, Ann Arbor, MI 48109 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Surrogate; Autoignition; Kinetic mechanisms; TSI; Motored engine; Constant volume spray chamber;

    机译:替代;自燃;动力学机制;TSI;机动发动机;恒定容积喷雾室;

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