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The combustion properties of 2,6,10-trimethyl dodecane and a chemical functional group analysis

机译:2,6,10-三甲基十二烷的燃烧特性及化学官能团分析

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摘要

The global combustion characteristics of 2,6,10-trimethyl dodecane (trimethyl dodecane), a synthetic fuel candidate species, have been experimentally investigated by measuring extinction limits for strained laminar diffusion flames at 1 atm and reflected shock ignition delays at 20 atm. The Derived Cetane Number (DCN) of trimethyl dodecane, (59.1) and Hydrogen/Carbon (H/C) ratio (2.133) are very close to the DCN and H/C ratio of a previously studied synthetic aviation fuel, S-8 POSF 4734 (S-8) and its surrogate mixture composed of n-dodecane/iso-octane (58.9 and 2.19, respectively). Identical high temperature global kinetic reactivities are observed in all experiments involving the aforementioned compounds. However, at temperatures below ~870 K, the S-8 surrogate mixture has ignition delay times approximately a factor of two faster. A chemical functional group analysis identifies that the methylene (CH_2) to methyl (CH_3) ratio globally correlates the low temperature alkylperoxy radical reactivity for these large paraffinic fuels. This result is further supported experimentally, by comparing observations using a surrogate fuel mixture of n-hexadecane (n-cetane) and 2,2,4,4,6,8,8-heptamethyl nonane (iso-cetane) that shares the same methylene-to-methyl ratio as trimethyl dodecane, in addition to the same DCN and H/C ratio. Measurements of both diffusion flame extinction and reflected shock ignition delays show that the n-cetane/iso-cetane model fuel has very similar combustion behavior to trimethyl dodecane at all conditions studied. A kinetic modeling analysis on the model fuel suggests the formation of alkylhydr-operoxy radicals (QOOH) to be strongly influenced by the absence or presence of the methyl and methylene functional groups in the fuel chemical structure. The experimental observations and analyses suggest that paraffinic based fuels having high DCN values may be more appropriately emulated by further including the CH_2 to CH_3 ratio as an additional combustion property target, as DCN alone fails to fully distinguish the relative reaction characteristics of low temperature kinetic phenomena.
机译:通过测量1 atm处的应变层流扩散火焰的消光极限并在20 atm处反射冲击点火延迟,已通过实验研究了合成燃料候选物质2,6,10-三甲基十二烷(三甲基十二烷)的整体燃烧特性。三甲基十二烷的十六烷值(DCN)(59.1)和氢/碳(H / C)比(2.133)非常接近先前研究的合成航空燃料S-8 POSF的DCN和H / C比。 4734(S-8)及其替代混合物,由正十二烷/异辛烷组成(分别为58.9和2.19)。在涉及上述化合物的所有实验中观察到相同的高温全局动力学反应性。但是,在低于870 K的温度下,S-8替代混合物的点火延迟时间大约快两倍。化学官能团分析确定,亚甲基(CH_2)与甲基(CH_3)的比例总体上与这些大链烷烃燃料的低温烷基过氧自由基反应性相关。通过比较使用正十六烷(n-十六烷)和2,2,4,4,6,8,8-庚甲基壬烷(异十六烷)的替代燃料混合物的观察值,该结果在实验上得到了进一步的支持。除了相同的DCN和H / C比率外,亚甲基与甲基的比率与三甲基十二烷的比率相同。扩散火焰消光和反射冲击点火延迟的测量表明,在所有研究条件下,正十六烷/异十六烷模型燃料的燃烧行为都与三甲基十二烷非常相似。对模型燃料的动力学建模分析表明,烷基氢过氧自由基(QOOH)的形成将受到燃料化学结构中是否存在甲基和亚甲基官能团的强烈影响。实验观察和分析表明,通过进一步包括CH_2与CH_3之比作为附加燃烧性能目标,可以更适当地模拟具有高DCN值的石蜡基燃料,因为仅DCN不能完全区分低温动力学现象的相对反应特性。 。

著录项

  • 来源
    《Combustion and Flame》 |2014年第3期|826-834|共9页
  • 作者单位

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA;

    Department of Chemical and Environmental Sciences, University of Limerick, Ireland;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA;

    Department of Mechanical Engineering, California State University Fullerton, Fullerton, CA, USA;

    Department of Mechanical, Aerospace, and Nuclear Engineering, Rensselaer Polytechnic Institute, Troy, NY, USA;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA;

    Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA;

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

    Alternative diesel fuel; Trimethyl dodecane; Farnesane; Surrogate fuel; Combustion properties;

    机译:替代柴油;三甲基十二烷;法呢烷;替代燃料;燃烧特性;
  • 入库时间 2022-08-18 00:11:28

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