基于子午粘性流动分析的跨声速离心压气机叶轮二次流抑制反设计方法

Sasuga Ito, Shinji Okada, Y. Kawakami, Kaito Manabe, M. Furukawa, Kazutoyo Yamada
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引用次数: 1

摘要

跨声速离心式压气机叶轮内的二次流影响其气动性能。在开式叶轮中,由于二次流和叶尖泄漏流相互干扰,会在靠近尾缘叶尖侧的吸力面聚集低能流体,在叶轮周围会产生复杂的流动现象。因此,设计人员在设计压气机叶轮时必须考虑二次流的影响,以避免压气机叶轮气动性能下降。本文提出了一种抑制离心压气机叶轮二次流的新设计理念,以改善其气动性能。本文采用基于子午粘性流动计算的二维反求方法,对跨声速离心压气机叶轮进行了重新设计。在上述计算过程中引入了一种设计理念。根据设计理念,通过弯曲涡丝控制叶片载荷分布的峰值位置,在与吸力面二次流径向相反的方向上产生叶片束缚涡诱导速度。为了研究设计理念的影响,本文进行了三维Reynolds平均Navier-Stokes模拟,采用临界点理论对涡核进行可视化,并采用无量纲螺旋度着色。在常规跨声速离心压气机叶轮中,确定了二次流涡,并对其中一个二次流涡进行了分解。与传统叶轮相比,重新设计的叶轮没有观察到二次流涡的破裂,并且抑制了低能流体的积累。该叶轮的总压比和绝热效率均高于常规叶轮,并成功抑制了二次流。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Suppression of Secondary Flows in a Transonic Centrifugal Compressor Impeller Using an Inverse Design Method Based on Meridional Viscous Flow Analysis
Secondary flows in transonic centrifugal compressor impellers affect their aerodynamic performance. In open-type impellers, low energy fluids can accumulate on the suction surfaces near the trailing edge tip side since the secondary flows and tip leakage flows interfere each other and complex flow phenomena can be generated around the impellers. Therefore, designers must consider the effect of secondary flows to avoid the aerodynamic performance degradation while designing compressor impellers. In this paper, a novel design concept about suppression of secondary flows in centrifugal compressor impellers to improve their aerodynamic performance. A transonic centrifugal compressor impeller was redesigned with the present design concept by a two-dimensional inverse method based on a meridional viscous flow calculation in this study. A design concept was introduced in above calculation process. As the design concept, by bending vortex filaments with controlling peak positions of the blade loading distributions, induced velocity due to bound vortices at the blades was generated in radial opposite direction of the secondary flows on the suction surface. Due to investigate the effect of the design concept in this paper, three-dimensional Reynolds Averaged Navier-Stokes simulations were carried out, and the vortex cores were visualized by a critical point theory and colored by non-dimensional helicity. In the conventional transonic centrifugal compressor impeller, the secondary flow vortices were confirmed and one of the vortices was broken down. In the redesigned impeller, the breakdown of the secondary flow vortices was not observed and the accumulation of the low energy fluids was suppressed compared with the conventional impeller. The total pressure ratio and adiabatic efficiency of the redesign impeller were higher than that of the conventional impeller, and the secondary flows were successfully suppressed in this research.
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