首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part C. Journal of mechanical engineering science >A novel pulse-adaption flow control method for a turbocharger turbine: Elastically restrained guide vane
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A novel pulse-adaption flow control method for a turbocharger turbine: Elastically restrained guide vane

机译:用于涡轮增压器涡轮机的新型脉冲适配流量控制方法:弹性限制导向叶片

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摘要

A turbocharger is a key enabler for energy conservation in an internal combustion engine. The turbine in a turbocharger is fed by highly pulsating gas flow due to the reciprocating engine, resulting in significant deterioration of the turbocharger performance. To solve this problem, a novel pulse-optimized regulation mechanism named 'elastically restrained guide vane' for a novel variable geometry turbocharger is proposed in this paper. The new mechanism regulates the instantaneous flow angle at turbine inlet due to guide vane's self-adaptive rotation under interactions of the elastic force by elastically restrained guide vane and the aerodynamic force from flowing gas, which is different from the traditional variable geometry turbocharger that is achieved by an active control system (e.g. actuator). To investigate the effectiveness of the novel method, a double-passage computational fluid dynamics model is built in ANSYS CFX software combined with a fluid-structure interaction method. The results demonstrate that the pulse-adaptive regulation method can effectively adjust the nozzle opening according to the different pulsating pressures at turbine inlet. Subsequently, based on the calibrated models, the numerical simulation concentrates on the potential gain in turbine eventual power output and the exhaust energy recover as well as the corresponding effects on efficiency as a result of operating the turbocharger in its elastically restrained guide vane mode compared to its operation as a conventional variable geometry turbocharger.
机译:涡轮增压器是内燃机中节能的关键推动因子。涡轮增压器中的涡轮机由由于往复发动机引起的高度脉动气流供给,导致涡轮增压器性能显着恶化。为了解决这个问题,本文提出了一种新的脉冲优化的调节机构,名为“可弹性限制导向叶片”的新型可变几何涡轮增压器。由于通过弹性束缚的导向叶片和流动气体的空气动力力,引导叶片的自适应旋转引导叶片的自适应旋转的引导叶片的自适应旋转的瞬时流动角度调节了涡轮机入口处的瞬时流动角。通过主动控制系统(例如,执行器)。为了研究新方法的有效性,在ANSYS CFX软件中建立了双通道计算流体动力学模型与流体结构相互作用方法建立。结果表明,脉冲自适应调节方法可以根据涡轮机入口处的不同脉动压力有效地调节喷嘴开口。随后,基于校准模型,数值模拟集中在涡轮机最终功率输出和排气能量恢复的潜在增益上,以及由于在其弹性受限制的导向叶片模式下操作涡轮增压器而对效率的相应效果。其作为传统变量几何涡轮增压器的操作。

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