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A NUMERICAL STUDY OF THE BLADE PASSING FREQUENCY NOISE OF A CENTRIFUGAL FAN

机译:离心风扇叶片通过频率噪声的数值研究

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Tonal noise constitutes the major part of the overall fan noise, especially the blade passing frequency (BPF) noise which is generally the most dominant component. This paper studies the BPF tonal noise of a centrifugal fan, including the blade noise, casing aerodynamic noise, and casing structural noise caused by the flow-induced casing vibration. Firstly, generation mechanism and propagation process of fan noise were discussed and the measured spectra of fan noise and casing vibration were presented. Secondly, a fully 3-D transient simulation of the internal flow field of the centrifugal fan was carried out by the computational fluid dynamics (CFD) approach. The results revealed that the flow interactions between the impeller and the volute casing caused periodic pressure fluctuations on the solid walls of the impeller and casing. This pressure fluctuation induces aerodynamic noise radiation as dipole sources, as well as structural vibration as force excitations. Thirdly, using the acoustic analogy theory, the aeroacoustic dipole sources on the casing and blade surface were extracted. The BPF casing and blade aerodynamic sound radiation were solved by the boundary element method (BEM) taking into account the scattering effect of the casing structure. Finally, the casing structural noise was studied. The casing forced vibration and sound radiation under the excitation of BPF pressure fluctuation were calculated by finite element method (FEM) and BEM, respectively. The result indicates that at the studied flow rate, the sound power levels of the casing aerodynamic noise, blade aerodynamic noise and casing structural noise are 103 dB, 91 dB and 79 dB with the reference sound power of 1×10~(-12) W, respectively.
机译:音调噪声构成了整个风扇噪声的主要部分,尤其是叶片通过频率(BPF)噪声,该噪声通常是最主要的成分。本文研究了离心风机的BPF音调噪声,包括叶片噪声,机壳空气动力学噪声和由流动引起的机壳振动引起的机壳结构噪声。首先讨论了风扇噪声的产生机理和传播过程,给出了风扇噪声和壳体振动的实测光谱。其次,通过计算流体动力学(CFD)方法对离心风机的内部流场进行了全3D瞬态仿真。结果表明,叶轮和蜗壳之间的流动相互作用在叶轮和壳体的坚固壁上引起周期性的压力波动。这种压力波动会引起空气动力学噪声辐射(如偶极子源),以及结构振动(如力激励)。第三,利用声学类比理论,提取了壳体和叶片表面的空气声偶极子声源。考虑到壳体结构的散射效应,通过边界元法(BEM)解决了BPF壳体和叶片空气动力声辐射的问题。最后,对套管结构噪声进行了研究。利用有限元法和边界元法分别计算了BPF压力波动激励下的套管强迫振动和声辐射。结果表明,在所研究的流速下,壳体空气动力噪声,叶片空气动力噪声和壳体结构噪声的声功率级分别为103 dB,91 dB和79 dB,参考声功率为1×10〜(-12)。 W,分别。

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