ROTATING STALL BEHAVIOR IN A DIFFUSER OF MIXED FLOW PUMP AND ITS SUPPRESSION

被引:0
|
作者
Miyabe, Masahiro
Furukawa, Akinori
Maeda, Hideaki
Umeki, Isamu
机构
关键词
Rotating Stall; Mixed Flow Pump; Vaned Diffuser; CFD; PIV; Instability;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The relationship between pump characteristic instability and internal flow was investigated on a mixed flow pump with specific speed omega s = 1.72 (dimensionless) or 700 (m(3)/min, m. min(-1)) by using a commercial CFD code and a dynamic PIV (DPIV) measurement. As a result, it was clarified that the diffuser rotating stalls causes the positive slope of a head-flow characteristic and the back-flow at hub-side of the vaned diffuser plays an important role on the onset of the diffuser rotating stall. The complex behaviors of diffuser rotating stall were visualized by the DPIV measurements and CFD simulation. Moreover, the internal flow was investigated in detail and the inception of characteristic instability was presumed as follows: At the partial flow rate, low energy fluids are accumulated in the corner between the hub surface and the suction surface of the diffuser vane. As the flow rate is further decreased, the low energy fluids region at the corner axi-symmetrically expands along the hub and become unstable due to adverse pressure gradient. Then, strong backflow occurs and impinges against passage flow from the impeller at the inlet of the vaned diffuser. In addition, the backflow blocks the passage flow from impeller and the inlet flow angle at the leading edge of adjacent diffuser vane is reduced. Therefore, flow separation occurs near the inlet of suction surface of the vaned diffuser, and a strong vortex is generated there. After that, the vortex develops and becomes a stall core. Based on above considerations, pump design parameter studies were numerically carried out and diffuser rotating stall was suppressed and pump characteristic instability was controlled by enlarging the inlet diameter of diffuser hub.
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收藏
页码:1147 / 1152
页数:6
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