首页> 外文期刊>JSME International Journal. Series B, Fluids and Thermal Engineering >Investigation of an Axial Fan -Blade Stress and Vibration Due to Aerodynamic Pressure Field and Centrifugal Effects
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Investigation of an Axial Fan -Blade Stress and Vibration Due to Aerodynamic Pressure Field and Centrifugal Effects

机译:气动压力场和离心作用引起的轴流扇叶片应力和振动的研究

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摘要

A 1.829 m (6 ft) diameter industrial large flow-rate axial fan operated at 1 770 rpm was studied experimentally in laboratory conditions. The flow characteristics on the fan blade surfaces were investigated by measuring the pressure distributions on the blade suction and pressure surfaces and the results were discussed by comparing with analytical formulations and CFD. Flow visualizations were also performed to validate the flow characteristics near the blade surface and it was demonstrated that the flow characteristics near the fan blade surface were dominated by the centrifugal force of the fan rotation which resulted in strong three-dimensional flows. The time-dependent pressure measurement showed that the pressure oscillations on the fan blade were significantly dominated by vortex shedding from the fan blades. It was further demonstrated that the pressure distributions during the fan start-up were highly unsteady, and the main frequency variation of the static pressure was much smaller than the fan rotational frequency. The time-dependent pressure measurement when the fan operated at a constant speed showed that the magnitude of the blade pressure variation with time and the main variation frequency was much smaller than the fan rotational frequency. The pressure variations that were related to the vortex shedding were slightly smaller than the fan rotational frequency. The strain gages were used to measure the blade stress and the results were compared with FEA results.
机译:在实验室条件下,通过实验研究了直径为1.829 m(6 ft)的工业大流量轴流风扇,其工作速度为1 770 rpm。通过测量叶片吸力和压力表面的压力分布来研究风扇叶片表面的流动特性,并与分析公式和CFD进行比较,讨论了结果。还进行了流动可视化以验证叶片表面附近的流动特性,并证明了风扇叶片表面附近的流动特性受风扇旋转的离心力所支配,从而产生了强劲的三维流动。随时间变化的压力测量结果表明,风扇叶片上的压力振荡主要由风扇叶片上的涡旋脱落所主导。进一步证明,风扇启动过程中的压力分布非常不稳定,并且静压的主频率变化远小于风扇旋转频率。风扇以恒定速度运行时随时间变化的压力测量结果表明,叶片压力随时间变化的幅度和主变化频率远小于风扇旋转频率。与涡流脱落有关的压力变化略小于风扇旋转频率。应变计用于测量叶片应力,并将结果与​​FEA结果进行比较。

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