侧气道旋转发动机低压直喷燃油-空气混合过程

O. Taskiran
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引用次数: 2

摘要

分层被认为是一个突出的技术,以改善火花点火发动机的性能,特别是在部分负荷。旋转发动机虽然具有高比功率,但其油耗和HC排放较高。出于这个原因,在旋转发动机的直接喷射方法已经研究,因为他们被引入市场。本文采用CFD技术对某侧气道旋转发动机的早期直喷进行了研究。研究的目的是获得低压直注法在混合气形成过程中的潜力。采用马自达Renesis发动机的几何模型进行建模研究,该模型是马自达Renesis发动机为研究活动而改装成单转子发动机的。燃油从当前的油孔位置直接注入燃烧室,该位置比Renesis发动机的任何其他位置具有更少的几何约束。对发动机典型的零件负荷工作点2000rpm进行了仿真。在数值计算中,湍流模型采用RNG k-e模型;采用Taylor类比破碎(TAB)模型对喷雾破碎进行建模。研究了火花塞周围存在丰富混合气的可能性的进气流型和燃油滴分布。结果表明,侧气道发动机的旋涡运动抑制了燃油喷雾在燃烧室中部的积聚。燃油液滴被进口空气的离心力驱动到进口壁面的反侧。由于转子的扫掠运动,这种影响随着旋涡流的减少而减少。观察到,在压缩行程的中后期,腔室内的主流转变为翻滚流。
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Fuel-air mixing process of low pressure direct injection in a side ported rotary engine
Stratification is seen as a prominent technique for improving the performance of spark ignition engines especially at part loads. Though rotary engines have high specific power, they suffer high fuel consumption and HC emission. For this reason, direct injection methods in rotary engines have been investigated since they were introduced to the market. In this study, early direct injection in a side ported rotary engine was investigated by using CFD techniques. The aim of the study is to obtain the potential of low pressure direct injection method on mixture formation process. Geometrical model of Mazda Renesis engine that were modified as a single rotor engine for research activities was used in the modeling studies. Fuel was injected directly to the chamber from present oil hole location that has less geometrical constraints than any other location of the Renesis engine. Simulations were done for 2000 rpm which is a typical part load operation point of the engine. In numerical calculations, RNG k-e model was used as the turbulence model; spray breakup was modeled by the Taylor Analogy Breakup (TAB) model. Flow pattern of intake air and fuel droplet distributions were investigated for a possibility of having rich mixture around spark plugs. The results showed that swirl-like motion of the side ported engine inhibits fuel spray to accumulate in the middle of the combustion chamber. Fuel droplets were driven to the counter side of the inlet wall by centrifugal force of the inlet air. This effect reduced as the swirl flow diminishes due to sweeping motion of the rotor. It is observed that the main flow in the chamber is converted to the tumble-like flow at middle and last part of the compression stroke.
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