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Dual-fuel Combustion of Hydrocarbon Fuel Droplets in Lean, Premixed Methane/Oxidizer Mixtures in a Rapid Compression Machine

机译:快速压缩机中稀薄的预混合甲烷/氧化剂混合物中的碳氢化合物燃料滴的双燃料燃烧

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摘要

The combustion of two fuels with disparate reactivity (dual-fuel) has been shown to be an effective method for increasing fuel efficiency and reducing both fuel costs and pollutant formation in internal combustion engines. Due to recent decreases in the price of natural gas, the incentive has grown to operate engines in dual-fuel mode, where some amount of diesel is substituted with natural gas. Since natural gas is expected to remain less expensive on a per-unit-energy basis than diesel fuel for the foreseeable future, it will continue to be economically advantageous to maximize the substitution percentage of natural gas in dual-fuel engines. However, at higher natural gas substitution percentages, uncontrolled fast combustion (i.e. engine knock) can occur, which limits the load of the engine and can shorten the lifetime of engine components. Emission of unburned methane has also been shown to increase with increasing natural gas substitution percentage. Previous detailed computational engine modeling at CSU with reduced chemical kinetics and simplified spray models has captured these effects but little data are available to validate chemistry and spray models at engine-relevant conditions. In this study, a rapid compression machine (RCM) was used as a platform to provide a high-temperature/high-pressure environment to better understand the thermodynamic, transport and chemical kinetic phenomena of dual-fuel combustion. The RCM was modified to perform evaporation and combustion experiments on single n-alkane fuel droplets in gaseous inert, O2/inert and O2/CH4/inert environments. Droplet evaporation experiments were performed on C5 to C12 n-alkane droplets in inert gas to measure droplet evaporation rates at near supercritical and supercritical conditions (18 bar < P < 35 bar;;iii.;450 K < T < 850 K). The Dual-fuel droplet evaporation and combustion experiments were studied using pressure data and images collected a Schlieren optical system. In the combustion experiments, ignition delay of heptane/O2/inert was quantified at elevated pressure and temperature (27 bar < P < 38 bar; 844 K < T < 1251 K). In addition, the process of dual-fuel combustion was captured, showing two distinct ignition events.
机译:两种具有不同反应性的燃料(双重燃料)的燃烧已被证明是提高燃料效率,减少内燃机中燃料成本和污染物形成的有效方法。由于最近天然气价格的下降,人们越来越有动机以双燃料模式运行发动机,在这种模式下,一定数量的柴油被天然气替代。由于在可预见的将来,按单位能量计算的天然气价格预计仍将低于柴油,因此在双燃料发动机中最大化天然气的替代百分比在经济上仍将是有利的。然而,在较高的天然气替代百分比下,会发生不受控制的快速燃烧(即发动机爆震),这限制了发动机的负荷并缩短了发动机组件的寿命。还显示出未燃烧甲烷的排放随着天然气替代百分比的增加而增加。以前在CSU进行的详细的发动机模型计算,降低的化学动力学和简化的喷雾模型已经捕获了这些影响,但是很少有数据可用于验证与发动机相关的条件下的化学模型和喷雾模型。在这项研究中,快速压缩机(RCM)被用作提供高温/高压环境的平台,以更好地理解双燃料燃烧的热力学,运输和化学动力学现象。修改了RCM,以在气态惰性,O2 /惰性和O2 / CH4 /惰性环境中对单个正构烷烃燃料滴进行蒸发和燃烧实验。在惰性气体中的C5至C12正构烷烃液滴上进行液滴蒸发实验,以测量接近超临界和超临界条件(18 bar

著录项

  • 作者

    Gould, Colin M.;

  • 作者单位

    Colorado State University.;

  • 授予单位 Colorado State University.;
  • 学科 Energy.;Mechanical engineering.
  • 学位 M.S.
  • 年度 2018
  • 页码 144 p.
  • 总页数 144
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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