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A direct comparison of unsteady influence of turbine with twin-entry and single-entry scroll on performance of internal combustion engine

机译:涡轮机与孪晶和单入口滚动对内燃机性能的直接比较

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摘要

Radial turbine with twin-entry scroll becomes prevailing recently due to its potential for energy recovery of internal combustion engine, especially at low speed condition. However, few quantitative comparisons of the impacts between this configuration and the conventional single-entry turbine have been performed on engine performance. This paper investigates unsteady influence of twin-entry and single-entry scroll on turbocharged engine performance via an in-house developed code 'SPEED-Engine' coupled with the geometry-based model of twin-entry turbine. Firstly, one-dimensional performance model of turbocharged diesel engine is established. Next, engine performance with two kinds of turbines is compared via the turbo-engine coupled model and confirms the 2.3% improvement of output power for the case with twin-entry. Further discussions manifest that swallowing capacity of twin-entry turbine varies with engine operational conditions, which has a similar function as a variable geometry turbine. The location of hysteresis loop is confirmed to be the reason for this phenomenon. Furthermore, a nominated throat area of twin-entry scroll is developed to compare the influence of twin-entry scroll on engine performance. Specifically, the nominated throat area is decreased by 28% at low engine speed. This investigation develops a convenient method to directly compare the effect of scroll configuration on engine performance.
机译:由于其内燃机能量回收的可能性,径向涡轮机具有较高的速度,特别是在低速条件下。然而,已经对发动机性能进行了很少的数量比较该配置与传统单入口涡轮机之间的影响。本文通过内部开发的代码“速度发动机”研究了双进入和单入口滚动对涡轮增压发动机性能的不稳定影响,与双入口涡轮机的几何形状的型号相结合。首先,建立了涡轮增压柴油发动机的一维性能模型。接下来,通过Turbo-Engine耦合模型比较具有两种涡轮机的发动机性能,并确认双进入的情况的输出功率的2.3%提高。进一步的讨论表明,双入口涡轮机的吞咽容量随发动机运行条件而变化,其具有与可变几何涡轮机相似的功能。确认滞后环的位置是这种现象的原因。此外,开发了一条双入口涡旋滚动的提名喉部区域,以比较双进入滚动对发动机性能的影响。具体地,提名的喉部区域以低发动机速度降低28%。本研究开发了一种方便的方法,可以直接比较滚动配置对发动机性能的影响。

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