Kunwoo Kim, Seo-Yoon Ryu, C. Cheong, Seongjin Seo, Cheolmin Jang, Hanshin Seol
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引用次数: 0
摘要
在本研究中,通过在现有的叶轮上设计分流叶片,降低了高速无绳吸尘器风扇电机单元的噪声。首先,利用计算流体动力学技术对非定常不可压缩雷诺-平均纳维-斯托克斯(RANS)方程进行数值求解,研究了风机-电机单元特别是叶轮内部的流场。以预测流场结果为输入,求解Ffowcs williams - hawkins (FW-H)积分方程,预测叶轮辐射的气动噪声。通过与实测声压谱的比较,验证了数值方法的有效性。对预测流场的进一步分析表明,叶轮叶片之间形成了强涡。由于涡流会引起流场损失并成为气动噪声源,因此在现有叶轮上设计补充分流叶片来抑制识别出的涡流。选取分离器的长度和位置作为设计因素,采用田口法数值分析了各设计因素对气动噪声的影响。根据实验结果,确定了最小辐射噪声条件下分路器的最佳位置和长度。最终选择的设计比现有的设计具有更低的噪声。
Aerodynamic noise reduction of fan motor unit of cordless vacuum cleaner by optimal designing of splitter blades for impeller
: In this study, noise radiated from a high-speed fan-motor unit for a cordless vacuum cleaner is reduced by designing splitter blades on the existing impeller. First of all, in order to investigate the flow field through a fan-motor unit, especially impeller, the unsteady incompressible Reynolds-Averaged Navier-Stokes (RANS) equations are numerically solved by using computational fluid dynamic technique. With predicted flow field results as input, the Ffowcs Williams-Hawkings (FW-H) integral equation is solved to predict aerodynamic noise radiated from the impeller. The validity of the numerical methods is confirmed by comparing the predicted sound pressure spectrum with the measured one. Further analysis of the predicted flow field shows that the strong vortex is formed between the impeller blades. As the vortex induces the loss of the flow field and acts as an aerodynamic noise source, supplementary splitter blades are designed to the existing impeller to suppress the identified vortex. The length and position of splitter are selected as design factors and the effect of each design factor on aerodynamic noise is numerically analyzed by using the Taguchi method. From this results, the optimum location and length of splitter for minimum radiated noise is determined. The finally selected design shows lower noise than the existing one.