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Unsteady performance of a mixed-flow turbine with nozzled twin-entry volute confronted by pulsating incoming flow

机译:带有双入口蜗壳蜗壳的混流式涡轮机的不稳定性能受到输入流的脉动

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Turbine with twin-entry volute has advantage of utilising energy from pulsatile exhaust gas and improving low-speed torque of an internal combustion engine. This paper investigates unsteady performance of a mixed flow turbine with nozzled twin-entry volute confronted by pulsatile incoming flow. The turbine performance at pulsating conditions with different Strouhal numbers (St) is studied via experimentally validated numerical method. Results show that the unsteadiness of turbine performance is enhanced as Strouhal number increases. In particular, the cycle-average efficiency at St = 0.522 is about 3.4% higher than that of quasi-steady condition (St = 0). Instantaneous loss breakdown of the turbine shows that the entropy generation rate of turbine components reduces evidently at pulsating conditions as Strouhal number increases, especially for the nozzle. Specifically, the cycle-averaged reduction of the loss in the nozzle is 37.3% at St = 0.522 compared with that of St = 0. The flow analysis shows that secondary flow which contributes to the majority of loss in the nozzle, including flow separation, horseshoe vortex, and reversed flow near the leading edge, are notably alleviated as Strouhal number increases. The alleviation of the flow structures are resulted from two reasons: one is that the flow distortion at the nozzle inlet is evidently depressed by the pulsating conditions, the other is that the inertia of the low momentum flow in the nozzle damps flow evolution at pulsating incoming flow. Consequently, the loss is reduced and the turbine performance is benefited by the pulsating inflows. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:具有双进气蜗壳的涡轮具有利用来自脉动废气的能量并改善内燃机的低速扭矩的优点。本文研究了带有双入口蜗壳的混流式涡轮机的不稳定性能,该涡轮机面对有脉动的进入流。通过实验验证的数值方法研究了在不同斯特劳哈尔数(St)的脉动条件下的涡轮性能。结果表明,随着Strouhal数的增加,涡轮机性能的不稳定加剧。特别是,St = 0.522时的循环平均效率比准稳态条件(St = 0)高约3.4%。涡轮机的瞬时损耗破坏表明,随着斯特劳哈尔数的增加,尤其是对于喷嘴,涡轮机组件的熵产生率在脉动条件下明显降低。具体而言,与St = 0相比,在St = 0.522时,喷嘴的损失平均减少了37.3%。流量分析表明,次级流量占喷嘴损失的大部分,包括流量分离,随着Strouhal数的增加,马蹄涡和前缘附近的逆流得到明显缓解。减少流动结构的原因有两个:一是由于脉动条件明显降低了喷嘴入口处的流动畸变,二是喷嘴中低动量流的惯性抑制了脉动进入时的流动演化。流。因此,损失减少了,脉动流使涡轮机性能受益。 (C)2019 Elsevier Masson SAS。版权所有。

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