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Research on unsteady performance of a two-stage self-priming centrifugal pump
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In order to study the unsteady performance of a two-stage self-priming centrifugal pump, the unsteady numerical calculation in a two-stage self-priming centrifugal pump was performed and energy characteristics experiments and self-priming experiments were carried out. The pressure pulsation and radial force in the pump were then analyzed. The results show that numerical calculation values are close to the experiment values. Head deviation of the pump is less than 3 %, and efficiency deviation of the pump is less than 2 percentage points. Compared with monitoring point P1, the pressure fluctuation coefficient of monitoring point P3 at the design flow rate is reduced by 61 %. Compared with monitoring point P8, the pressure fluctuation coefficient of monitoring point P5 is reduced by 70 %. The radial force on the radial guide-vane is obviously smaller than that on the volute. Under the same flow rate, radial force on the volute of second-stage pump is almost 20 times larger than that on the radial guide-van of first-stage pump.
JVE International Ltd.
Title: Research on unsteady performance of a two-stage self-priming centrifugal pump
Description:
In order to study the unsteady performance of a two-stage self-priming centrifugal pump, the unsteady numerical calculation in a two-stage self-priming centrifugal pump was performed and energy characteristics experiments and self-priming experiments were carried out.
The pressure pulsation and radial force in the pump were then analyzed.
The results show that numerical calculation values are close to the experiment values.
Head deviation of the pump is less than 3 %, and efficiency deviation of the pump is less than 2 percentage points.
Compared with monitoring point P1, the pressure fluctuation coefficient of monitoring point P3 at the design flow rate is reduced by 61 %.
Compared with monitoring point P8, the pressure fluctuation coefficient of monitoring point P5 is reduced by 70 %.
The radial force on the radial guide-vane is obviously smaller than that on the volute.
Under the same flow rate, radial force on the volute of second-stage pump is almost 20 times larger than that on the radial guide-van of first-stage pump.
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