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Performance optimization of a Two-Stroke supercharged diesel engine for aircraft propulsion

机译:用于飞机推进的二冲程增压柴油发动机的性能优化

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In Two-Stroke engines, the cylinder filling efficiency is antithetical to the cylinder scavenging efficiency; moreover, both of them are influenced by geometric and thermodynamic parameters characterizing the design and operation of both the engine and the related supercharging system. Aim of this work is to provide several guidelines about the definition of design and operation parameters for a Two-Stroke two banks Uniflow diesel engine, supercharged with two sequential turbochargers and an aftercooler per bank, with the goal of either increasing the engine brake power at take-off or decreasing the engine fuel consumption in cruise conditions. The engine has been modeled with a 0D/1D modeling approach. Then, the model capability in describing the effect of several parameters on engine performance has been assessed comparing the results of 3D simulations with those of 0D/1D model. The validated 0D/1D model has been used to simulate the engine behavior varying several design and operation engine parameters (exhaust valves opening and closing angles and maximum valve lift, scavenging ports opening angle, distance between bottom edge of the scavenging ports and bottom dead center, area of the single scavenging port and number of ports, engine volumetric compression ratio, low and high pressure compressor pressure ratios, air/fuel ratio) on a wide range of possible values. The parameters most influencing the engine performance are then recognized and their effect on engine thermodynamic behavior is discussed. Finally, the system configurations leading to best engine power at sea level and lowest fuel consumption in cruise conditions- respectively +42% and -7% with respect to baseline-have been determined implementing a multicriteria optimization procedure. (C) 2016 Elsevier Ltd. All rights reserved.
机译:在二冲程发动机中,汽缸填充效率与汽缸扫气效率相反。此外,它们都受到表征发动机和相关增压系统的设计和运行的几何和热力学参数的影响。这项工作的目的是为两冲程两列Uniflow柴油发动机的设计和运行参数的定义提供一些指导,该柴油发动机用两个顺序涡轮增压器和每列后冷器进行增压,目的是提高发动机的制动功率。在巡航条件下起飞或减少发动机油耗。该引擎已使用0D / 1D建模方法进行了建模。然后,通过比较3D仿真结果和0D / 1D模型的结果,评估了描述几个参数对发动机性能的影响的模型能力。经过验证的0D / 1D模型已用于模拟发动机行为,该发动机行为会改变一些设计和运行中的发动机参数(排气门的打开和关闭角度以及最大气门升程,扫气口打开角度,扫气口底边缘与下止点之间的距离) ,单个扫气口的面积和端口数,发动机容积压缩比,低压和高压压缩机的压力比,空燃比)在可能的范围内。然后识别最影响发动机性能的参数,并讨论它们对发动机热力学行为的影响。最后,已经确定了实现多标准优化程序的系统配置,该系统配置可在海平面上获得最佳发动机功率,并在巡航条件下实现最低燃油消耗(相对于基准分别为+ 42%和-7%)。 (C)2016 Elsevier Ltd.保留所有权利。

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