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Experimental investigation of the effect of cavitation on the rotordynamic forces on a whirling centrifugal pump impeller.

机译:空化对旋转离心泵叶轮转子动力的影响的实验研究。

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摘要

The interaction of a rotating impeller and the working fluid introduce forces on the rotor. These fluid-induced forces can cause self-excited whirl, where the rotor moves away from and whirls along a trajectory eccentric to its undeflected position. When designing a turbomachine, particularly one which is to operate at high speed, it is important to be able to predict the fluid-induced forces, both steady and unsteady, acting on the various components of the machine. The fluid-induced rotordynamic forces acting upon the impeller and therefore on the bearings was investigated for a centrifugal impeller in a spiral volute in the presence of cavitation.; An experiment in forced vibration was made to study the fluid-induced rotordynamic force on an impeller whirling around its machine axis of rotation in water. The whirl trajectory of the rotor is prescribed to be a circular orbit of a fixed radius. A dynamometer mounted behind the rotor and rotating with it measures the force on the impeller. The force measured is a combination of a steady radial force due to volute asymmetries and an unsteady force due to the eccentric motion of the rotor. These measurements have been carried out over a full range of whirl/impeller speed ratios at different flow coefficients for various turbomachines. A destabilizing force was observed over a region of positive whirl ratio. Cavitation corresponding to a three percent head loss did not have a significant effect upon this destabilizing force. However, a lesser degree of cavitation at the design point for the impeller-volute combination tested increased this destabilizing force for a particular set of whirl ratios.
机译:旋转的叶轮和工作流体的相互作用将力施加到转子上。这些由流体引起的力会引起自激涡旋,在此转子从偏心轨迹移开并沿着偏心轨迹回旋至未偏转位置。在设计涡轮机时,特别是设计一种高速运转的涡轮机时,重要的是要能够预测作用在机器各个部件上的,由流体引起的稳态和非稳态力。对于存在气蚀现象的螺旋蜗壳中的离心式叶轮,研究了作用在叶轮上并因此作用在轴承上的流体诱导的转子动力。进行了强迫振动实验,研究了绕叶轮在水中旋转的叶轮上由流体引起的转子动力。转子的旋涡轨迹规定为具有固定半径的圆形轨道。测功机安装在转子后面并随其旋转,以测量叶轮上的力。测得的力是由于蜗壳不对称引起的稳定径向力与由于转子的偏心运动引起的不稳定力的组合。这些测量是在各种涡轮机的不同流量系数下,在整个旋涡/叶轮速度比范围内进行的。在正涡动比的区域观察到去稳定力。相应于3%的水头损失的气蚀对该稳定力没有显着影响。但是,对于一组特定的涡流比,在测试的叶轮-蜗壳组合设计点上出现的气穴程度较小,从而增加了这种不稳定力。

著录项

  • 作者

    Franz, Ronald John.;

  • 作者单位

    California Institute of Technology.;

  • 授予单位 California Institute of Technology.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1989
  • 页码 178 p.
  • 总页数 178
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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