空间不均匀流场诱发螺旋桨振动的实验研究

Experimental study on flow-induced vibration of propeller blades under non-uniform inflow

  • 摘要:
      目的  为获得空间不均匀流场诱发的螺旋桨振动随其固有频率的变化关系,进行实验研究。
      方法  实验获得两种几何外形相同而材料不同的七叶大侧斜螺旋桨在不同工况下的动应变。实验中的空间非均匀流场由螺旋桨上游400 mm处布置的4阶或6阶尾流窗产生。在尾流窗下游100 mm处布置激光多普勒测试系统,测得流场的轴向速度分布。利用贴在桨叶不同位置的应变片测试系统测得桨叶振动应变。
      结果  获得了桨叶振动随螺旋桨转速与尾流窗变化的规律,在均匀来流条件、4阶和6阶不均匀来流条件下,动应变频谱的最大峰值分别出现在轴频、4倍轴频和6倍轴频处。明确了非均匀流场激励下桨叶固有模态对其振动响应的影响,当6倍轴频激励力的频率与塑料桨的固有频率一致时发生共振,桨叶振动的幅度最大。
      结论  本研究表明设计人员设计螺旋桨时,除关注其水动力性能外,应考虑其固有频率的影响。

     

    Abstract:
      Objectives  This article presents an experimental study of the flow-induced vibration of propeller blades under periodic inflow, and the dependence of the response on its modes.
      Methods  Two seven-bladed highly skewed model propellers of identical proportions but different material are operated in four-cycle and six-cycle inflows to produce a blade vibratory strain response. Two kinds of wire mesh wake screens located 400 mm upstream of the propeller plane are used to generate the four-cycle and six-cycle inflows. A laser Doppler velocimetry system located 100 mm downstream of the wake screen plane is used to measure the axial velocity distributions produced by the wake screens. Strain gauges are attached to the propeller blades at different positions. The data from the strain gauges quantifies the excitation frequencies induced by the wake screens. It is shown that the response will reach peak axial propeller frequency, four times axial propeller frequency and six times axial propeller frequency under uniform inflow, four-cycle inflow and six-cycle inflow respectively.
      Results  The effect of resonance on the vibratory strain response is revealed. When six times axial propeller frequency induced by six-cycle inflow coincides with the natural frequency of a flexible propeller, the response of the propeller is at its greatest.
      Conclusions  This research reveals that when designing a propeller, it is not sufficient to only focus on its hydrodynamic properties; the effects of the modes of the propeller should also be considered.

     

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