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Evaporation and Autoignition Studies of Liquid n-Alkane Droplets in Lean, High Pressure Methane/Air Mixtures in a Rapid Compression Machine

机译:快速压缩机中稀液N-烷烃液滴液态N-烷烃液滴的蒸发和自燃研究

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The combustion of two fuels with disparate reactivity (e.g. natural gas/diesel) in conventional diesel engines has been demonstrated as a means to increase fuel efficiency, reduce fuel costs and reduce pollutant formation compared to standard diesel operation. To maximize the economic benefits, it is desirable to maximize the natural gas substitution rate. However, the natural gas substation rate is constrained by onset of uncontrolled fast combustion (i.e. engine knock) and/or incomplete combustion, which results in high unburned hydrocarbon emissions. Previous detailed computational engine modeling with reduced chemical kinetics and simplified spray models have captured these effects but little data are available to validate chemistry and spray models at these engine-like 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, O_2/inert and O_2/CH_4/inert environments. Droplet evaporation experiments were performed on C_5 to C_(12) n-alkane droplets in inert gas to measure droplet evaporation rates at near supercritical and supercritical conditions (18 bar < P < 35 bar; 450 K < T < 850 K). Droplet ignition experiments were conducted to measure ignition delay as a function of temperature, pressure and ambient CH_4 concentration.
机译:在传统的柴油发动机中具有不同反应性的两个燃料(例如天然气/柴油)的燃烧已经证明了提高燃料效率,降低燃料成本并与标准柴油操作相比降低燃料成本的手段。为了最大限度地提高经济效益,希望最大化天然气替代率。然而,天然气变电站率受到不受控制的快速燃烧(即发动机爆震)和/或不完全燃烧的发生限制,这导致高碳酸烃排放。以前的详细的计算发动机,具有减少的化学动力学和简化的喷雾模型已经捕获了这些效果,但是可以在这些发动机状条件下验证化学和喷涂模型的几乎没有数据。在这项研究中,快速压缩机(RCM)用作提供高温/高压环境的平台,以更好地了解双燃料燃烧的热力学,运输和化学动力学现象。修饰RCM以对气态惰性,O_2 /惰性和O_2 / CH_4 /惰性环境中的单一N-烷烃燃料液滴进行蒸发和燃烧实验。在惰性气体中对C_5至C_(12)N-烷烃液滴进行液滴蒸发实验,在近临界和超临界条件下测量液滴蒸发速率(18AR

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