首页> 外文会议>2003 Fall Technical Conference of the ASME Internal Combustion Engine Division; Sep 7-11, 2003; Erie, Pennsylvania >DESIGN OF A COMPRESSION PRESSURIZED AIR BLAST DIRECT INJECTION SYSTEM FOR SMALL DISPLACEMENT TWO-STROKE ENGINES
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DESIGN OF A COMPRESSION PRESSURIZED AIR BLAST DIRECT INJECTION SYSTEM FOR SMALL DISPLACEMENT TWO-STROKE ENGINES

机译:小排量二冲程发动机压缩空气直接喷射系统设计

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In two-stroke engines replacement of carburetors with direct fuel injection systems greatly reduces engine emissions and fuel consumption by eliminating fuel short-circuiting. Air-blast direct fuel injection using a dedicated air pump has been successfully applied to both two- and four-stroke engines. In this study we re-examine the design of a low cost compression pressurized direct injection system. This system uses gases extracted from the combustion chamber during the compression stroke to supply pressure for the air blast injection, thus eliminating the air pump. Gases, predominantly scavenging air, are transferred to a mixing cavity from the combustion chamber via a small (5mm diameter) solenoid poppet valve as the piston rises during the compression stroke. Proper functioning of the system requires careful optimization of the mixing cavity size and the blast valve timing to ensure adequate mixing cavity pressure and fuel atomization. To assist in the optimization of these design parameters a one-dimensional fluid dynamics model has been developed. Parameter sensitivity studies were carried out using the model to determine the optimum cavity size, blast valve timing, and fuel injection duration. These parameters were optimized over a wide range of engine speeds and throttle settings. Results show that a mixing cavity pressure of 500 kPa is attainable over the range of 1000 to 6000 rpm, from closed throttle to wide open throttle (WOT) without cavity pressurization encroaching into the ignition regime. Fuel maps and valve timings are presented and results are contrasted with the carbureted case, showing improved fuel efficiency and emissions for the direct injection system. These data will be used in the design of a physical demonstration engine.
机译:在二冲程发动机中,通过直接燃料喷射系统替代化油器,可消除燃料短路,从而大大减少了发动机排放和燃料消耗。使用专用气泵的鼓风直接燃油喷射已成功应用于二冲程和四冲程发动机。在这项研究中,我们重新检查了低成本压缩加压直接喷射系统的设计。该系统在压缩冲程期间使用从燃烧室中抽出的气体为喷射空气提供压力,从而省去了气泵。当活塞在压缩冲程中升起时,主要清除空气的气体通过一个小(直径5mm)的电磁提升阀从燃烧室转移到混合腔。系统正常运行需要仔细优化混合腔的大小和鼓风阀正时,以确保足够的混合腔压力和燃料雾化。为了帮助优化这些设计参数,已开发了一维流体动力学模型。使用该模型进行了参数敏感性研究,以确定最佳腔体尺寸,爆破阀正时和燃料喷射持续时间。这些参数已在各种发动机转速和节气门设置中进行了优化。结果表明,从密闭节气门到全开节气门(WOT),在1000至6000 rpm的转速范围内,可获得500 kPa的混合腔压力,而腔内增压不会侵入点火区。给出了燃油图和气门正时,并将结果与​​化油器进行了对比,显示了直接喷射系统的燃油效率和排放得到改善。这些数据将用于物理演示引擎的设计中。

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