首页> 外文期刊>Journal of Fluids Engineering: Transactions of the ASME >The unsteady pressure field in a high specific speed centrifugal pump impeller -- part I: influence of the volute
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The unsteady pressure field in a high specific speed centrifugal pump impeller -- part I: influence of the volute

机译:高比转速离心泵叶轮中的非定常压力场-第一部分:蜗壳的影响

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An experimental investigation is presented regarding the unsteady pressure field within a high specific speed centrifugal pump impeller (ω{sub}s=1.7) which operated in a double spiral volute. For this, twenty-five piezoresistive pressuretransducers were mounted within a single blade passage and sampled in the rotating impeller frame with a telemetry system. The influence of varying volume flux on the pressure transducers was evaluated in terms of pressure fluctuation magnitudes and phase differences. The magnitude information reveals that the pressure fluctuations from the impeller-volute interaction grew as the volume flux become further removed from the best efficiency point and as the trailing edge of the impeller blade was approached. These fluctuations reached 35% of the pump head in deep part load. The upstream influence of the volute steady pressure field dominates the unsteady pressure field within the impeller at all off design load points. Acquired signal phase informationpermits the identification of the pressure field unsteadiness within the impeller passage as fundamentally synchronized simultaneously with the volute tongue passing frequency. Special emphasis was placed on the volume flux regime where the pump andimpeller pressure discharge characteristic undergo hysteresis, as impeller inlet and outlet recirculation commence and cease. A synthesis of the rotating transducers was performed to obtain unsteady blade loading parameters. The value of the unsteady lift coefficient varies on the order of 200% for a single blade in part load operation (at 45% bep), an abrupt fluctuation occurring as the fore running blade suction side passes a volute tongue. The unsteady moment coefficient and center of pressure are alsoshown to vary significantly during the impeller-volute tongue interaction.
机译:提出了关于在双螺旋蜗壳中运行的高比转速离心泵叶轮(ω{sub} s = 1.7)中的非恒定压力场的实验研究。为此,将二十五个压阻式压力传感器安装在单个叶片通道中,并使用遥测系统在旋转的叶轮框架中进行采样。根据压力波动幅度和相位差评估了体积通量对压力传感器的影响。量值信息显示,随着体积流量从最佳效率点进一步去除以及接近叶轮叶片的后缘,叶轮与蜗壳相互作用产生的压力波动会增大。在深部分负荷下,这些波动达到了泵压头的35%。蜗壳稳态压力场的上游影响在所有非设计载荷点主导了叶轮内的非稳态压力场。所获取的信号相位信息可以识别出叶轮通道内的压力场不稳定,因为该压力场与蜗壳舌片通过频率基本同步。特别强调了体积流量状态,在此情况下,随着叶轮入口和出口再循环的开始和停止,泵和叶轮的压力排放特性会出现滞后。进行了旋转换能器的综合以获得不稳定的叶片加载参数。对于单叶片在部分负载操作(45%bep)下,非恒定升力系数的值在200%的数量级上变化,当前叶片吸力侧经过蜗壳舌时会发生突然波动。还显示了在叶轮与蜗壳舌相互作用期间,非定常力矩系数和压力中心会发生显着变化。

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