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Modeling the Evolution of Fuel and Lubricant Interactions on the Liner in Internal Combustion Engines

机译:基于内燃机衬里燃料和润滑剂相互作用的塑造模拟

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In internal combustion engines, a portion of liquid fuel spray may directly land on the liner and mix with oil (lubricant), forming a fuel-oil film (~10μm) that is much thicker than the original oil film (~0.1μm). When the piston retracts in the compression stroke, the fuel-oil mixture may have not been fully vaporized and can be scraped by the top ring into the 1st land crevice and eventually enter the combustion chamber in the format of droplets. Studies have shown that this mechanism is possibly a leading cause for low-speed pre-ignition (LSPI) as the droplets contain oil that has a much lower self-ignition temperature than pure fuel. In this interest, this work aims to study the oil-fuel interactions on the liner during an engine cycle, addressing molecular diffusion (in the liquid film) and vaporization (at the liquid-gas interface) to quantify the amount of fuel and oil that are subject to scraping by the top ring, thereby exploring their implications on LSPI and friction. An analytical model is developed by coupling multi-component heat and mass transfer using an implicit, adaptive-time and fixed-space numerical scheme. The results of this model suggest that a substantial fraction of the fuel-oil mixture still remains on the liner when the piston retracts if the initial fuel film thickness is on the order of 20 μm; this fuel-oil mixing also results in a local oil dilution that can lead to a significant increase in the ring-liner contact force.
机译:在内燃机中,液体燃料喷雾的一部分可以直接落在衬里上并与油(润滑剂)混合,形成比原始油膜(约0.1μm)更厚的燃料 - 油膜(〜10μm)。当活塞在压缩冲程中缩回时,燃料油混合物可能尚未完全蒸发,并且可以通过顶部环刮到第一陆地缝隙中,并最终以液滴的形式进入燃烧室。研究表明,由于液滴含有比纯燃料更低的自燃温度的油,这种机制可能是低速预点火(LSPI)的主要原因。在这种兴趣中,这项工作旨在在发动机循环期间研究衬里上的油燃料相互作用,寻址分子扩散(在液体膜中)和蒸发(在液体气体界面)中,以量化燃料和油的量受顶环的刮擦,从而探讨了对LSPI和摩擦的影响。通过使用隐式,自适应时间和固定空间数值方案耦合多分量热量和质量传递来开发分析模型。该模型的结果表明,如果初始燃料膜厚度约为20μm,则当活塞缩回时,在衬里仍然保持在衬里上的大部分仍然保持在衬里上;这种燃料油混合也导致局部油稀释,这可以导致环衬圆接触力显着增加。

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