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Two-stage turbocharging for the downsizing of SI V-engines

机译:两级涡轮增压,用于缩小SI V型发动机的尺寸

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摘要

One of the most critical challenges for the specific power increase of turbocharged SI engines is the low end torque, limited by two aspects. First, the big size of the compressor necessary to deliver the maximum airflow does not allow high boost pressures at low speed, due to the surge line proximity. Second, the flame front velocity may become slower than the end gas auto-ignition rate, thus increasing the risk of knocking. This study is based on a current SI GDI V8 turbocharged engine, modeled by means of CFD tools, both 1d and 3d. The goal of the activity is to lower by 20% the displacement, without reducing brake torque, all over the engine speed range. It was decided to adopt a smaller bore, keeping stroke constant. Obviously, the combustion chamber, the valves and the intakeexhaust ports have been re-designed, as well as the whole intake and exhaust system. Instead of the two turbochargers, one for each bank of cylinders, a triple-turbocharger layout has been considered. The development of the engine has been carried out by means of 1D engine cycle simulations, using predictive knock models, calibrated with the support of both experiments and CFD-3d simulations. A few operating conditions for the final configuration have been also analyzed by means of a 3-d CFD tool. The paper presents the results of this activity, and describes in details the guidelines followed for the development of the engine.
机译:涡轮增压SI发动机的特定功率增加最关键的挑战之一是低端扭矩,受两个方面的限制。首先,由于喘振管线的接近性,提供最大气流所需的大尺寸压缩机不允许在低速下产生较高的增压压力。其次,火焰前移速度可能会比最终气体的自燃速率慢,从而增加了爆震的风险。这项研究基于当前的SI GDI V8涡轮增压发动机,并通过Cd工具(1d和3d)建模。该活动的目标是在整个发动机转速范围内将排量降低20%,而不降低制动扭矩。决定采用较小的孔,以保持行程恒定。显然,燃烧室,气门和进气口以及整个进气和排气系统都经过了重新设计。代替两个涡轮增压器(每排气缸一个),已经考虑了三涡轮增压器布局。发动机的开发已经通过一维发动机循环模拟进行,使用了预测性爆震模型,并在实验和CFD-3d模拟的支持下进行了校准。最终配置的一些操作条件也已通过3-d CFD工具进行了分析。本文介绍了该活动的结果,并详细描述了开发引擎所遵循的准则。

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