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NUMERICAL SIMULATION OF SURGE IN TURBOCHARGER CENTRIFUGAL COMPRESSOR - INFLUENCES OF DOWNSTREAM PLENUM

机译:增压器离心式压缩机喘振的数值模拟-下游气室的影响。

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Surge is an important instability seriously affecting compression systems. This paper presents a numerical simulation of surge flow phenomenon inside a turbocharger centrifugal compressor with a vaneless diffuser. The compressor was discharged into a plenum and the effect of the plenum on surge behavior of the compressor system was investigated. The entire geometry of the compressor, including the impeller, vaneless diffuser, volute housing and downstream plenum, were included in the simulation. Three-dimensional Reynolds averaged compressible Navier-Stokes equations were solved with the κ-ε turbulence model using commercial software CFX and two different sizes of plenum were studied. A new plenum model is proposed which allows temporal variation of temperature inside the plenum. The numerical technique employed to set up CFD (computational fluid dynamics) with such an unstable flow system are described. The results show that when the plenum volume was nearly doubled, the dominating frequency of the system suddenly dropped from 72Hz to 23Hz. During the surge cycle, the compressor characteristic (pressure ratio v mass flow curve) showed distinct differences. With the smaller plenum, the characteristic showed random traces with little global backflow at the compressor inlet, while with the larger plenum, clear surge cycles are displayed with strong global backflow at the inlet. The flow fields of the two systems are presented as functions of time and show distinct differences. In the case of the smaller plenum, the circumferential flow field inside the impeller is non uniform, showing influences of rotating stall, while in the case of the large plenum, the circumferential uniformity returns and the flow field behaves quasi-steadily during the surge cycle. With the larger plenum, the volute flow synchronises with the inlet mass flow oscillation in time and a completed vortex break down occurs at every volute cross section, but with the smaller plenum the synchronisation disappears and vortex break down only occurs partially at the centers of some volute cross sections.
机译:喘振是严重影响压缩系统的重要不稳定因素。本文提出了带有无叶片扩压器的涡轮增压离心压缩机内部喘振现象的数值模拟。将压缩机排入增压室,并研究增压对压缩机系统喘振性能的影响。模拟中包括了压缩机的整个几何形状,包括叶轮,无叶片扩压器,蜗壳和下游增压室。使用商业软件CFX用κ-ε湍流模型求解了三维雷诺平均可压缩Navier-Stokes方程,并研究了两种不同尺寸的气室。提出了一种新的气室模型,该模型允许气室内部温度随时间变化。描述了用这种不稳定的流动系统建立CFD(计算流体动力学)的数值技术。结果表明,当气室容积几乎增加一倍时,系统的主导频率突然从72Hz下降到23Hz。在喘振周期中,压缩机特性(压力比v质量流量曲线)显示出明显的差异。气室越小,该特性将显示出随机痕迹,压缩机入口处的总体回流很小,而气室越大,则显示清晰的喘振周期,且入口处的整体回流强。这两个系统的流场作为时间的函数表示,并显示出明显的差异。在较小的气室的情况下,叶轮内部的周向流场是不均匀的,显示出旋转失速的影响,而在较大的气室的情况下,周向均匀性又恢复了,并且在喘振周期中流场表现为准稳定。在更大的气室中,蜗壳流动与入口质量流振荡及时地同步,并且在每个蜗壳横截面上都发生了完整的涡旋破坏,但是在较小的气室中,同步消失了,涡旋破坏仅部分地在某些中心发生。蜗壳横截面。

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