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PIV investigation of the flow induced by a passive surge control method in a radial compressor

机译:被动式喘振控制方法在径向压缩机中引起的流动的PIV研究

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Due to recent emission regulations, the use of turbochargers for force induction of internal combustion engines has increased. Actually, the trend in diesel engines is to downsize the engine by use of turbochargers that operate at higher pressure ratios. Unfortunately, increasing the impeller rotational speed of turbocharger radial compressors tends to reduce their range of operation, which is limited at low mass flow rate by the occurrence of surge. In order to extend the operability of turbochargers, compressor housings can be equipped with a passive surge control device such as a “ported shroud.” This specific casing treatment has been demonstrated to enhance the surge margin with minor negative impact on the compressor efficiency. However, the actual working mechanisms of the system remain not well understood. Hence, in order to optimize the design of the ported shroud, it is crucial to identify the dynamic flow changes induced by the implementation of the device to control instabilities. From the full dynamic survey of the compressor performance characteristics obtained with and without ported shroud, specific points of operation were selected to carry out planar flow visualization. At normal working, both standard and stereoscopic particle imaging velocimetry (PIV) measurements were performed to evaluate instantaneous and mean velocity flow fields at the inlet of the compressor. At incipient and full surge, phase-locked PIV measurements were added. As a result, satisfying characterization of the compressor instabilities was provided at different operational speeds. Combining transient pressure data and PIV measurements, the time evolution of the complex flow patterns occurring at surge was reconstructed and a better insight into the bypass mechanism was achieved.
机译:由于最近的排放法规,增加了将涡轮增压器用于内燃机的力感应。实际上,柴油发动机的趋势是通过使用在较高压力比下运行的涡轮增压器来减小发动机的尺寸。不幸的是,增加涡轮增压器径向压缩机的叶轮转速趋于减小其工作范围,这在低质量流量下受到喘振的限制。为了扩展涡轮增压器的可操作性,压缩机壳体可以配备无源喘振控制装置,例如“端口罩”。事实证明,这种特殊的套管处理方法可提高喘振裕度,并对压缩机效率产生较小的负面影响。但是,该系统的实际工作机制仍然没有很好地理解。因此,为了优化带孔罩的设计,至关重要的是识别由装置的实施引起的动态流量变化以控制不稳定性。从对带或不带端口护罩的压缩机性能特性进行的全面动态调查中,选择了特定的操作点以进行平面流可视化。在正常工作时,执行标准和立体粒子成像测速(PIV)测量,以评估压缩机入口处的瞬时和平均速度流场。在初始和完全浪涌时,添加了锁相PIV测量。结果,在不同的运行速度下提供了令人满意的压缩机不稳定性特征。结合瞬态压力数据和PIV测量,重构了在喘振时出现的复杂流型的时间演化,并更好地了解了旁路机制。

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