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Numerical Analysis on Effects of Inlet Bent Pipe's Position on a Centrifugal Compressor's Aerodynamic Noise

机译:入口弯管位置对离心式压缩机空气动力学噪声影响的数值分析

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The inlet connection of a centrifugal compressor is a bent pipe, and a straight pipe is installed between the bent pipe outlet and impeller inlet. The effect of different lengths of the straight pipe on the aerodynamic noise of a centrifugal compressor is numerically simulated. The result show that it's essential to value the inlet bent pipe's position in the inlet and outlet aerodynamic design. With the increase of straight pipe's length, the noise radiated from the inlet decreases. When the length is over the pipe diameter, it has little effect on the outlet noise. The increase of straight pipe's length also makes the circumferential noise decrease. The noise is distorted at approximately 90° in the rotational direction of the volute tongue. The sound power level of the compressor decreases to a constant value with the length over the pipe diameter. In the engineering application on aerodynamic noise, the straight pipe's length before impeller inlet should be longer than the pipe diameter.
机译:离心式压缩机的入口连接是弯曲管,直管安装在弯曲管道和叶轮入口之间。在数值模拟中模拟了不同长度的直管对离心式压缩机的空气动力噪声的影响。结果表明,在入口和出口空气动力学设计中重视入口弯管的位置是必要的。随着直管长度的增加,从入口辐射的噪声减小。当长度超过管道直径时,它对出口噪声影响很小。直管长度的增加也使圆周噪声减小。噪声在速度舌头的旋转方向上的大约90°处变形。压缩机的声功率水平降低到具有管道直径的长度的恒定值。在空气动力学噪声的工程应用中,叶轮入口前的直管长度应比管道长度长。

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