期刊文献+

矿用离心风机阶梯蜗舌降噪机理数值研究 被引量:4

Numerical Simulation of Noise Reduction Mechanism of Stepped Tongue on Mine Centrifugal Fan
下载PDF
导出
摘要 以某矿用离心风机为研究对象,基于三维不可压缩雷诺时均Navier-Stokes方程和Standard k-ε湍流模型对此风机进行数值模拟研究。风机气动性能试验验证了数值模拟的准确性。在噪声源分析的基础上,采用阶梯蜗舌结构降低其气动噪声辐射,并给出了此种结构的降噪机理。此降噪机理为:阶梯蜗舌结构使得风机在噪声源区域产生不同的压力脉动波形,从而形成一个相位差,抵消了噪声源区域部分压力脉动,致使阶梯蜗舌覆盖高位区域噪声源强度有所减弱。 A numerical simulation method based on the three-dimensional impressible time-average Navier-Stokes equations and Standard κ-ε turbulent flow model was used in a mine centrifugal fan. The aerodynamic performance of numerical simulation shows a good agreement with the experimental one. A stepped tongue, which based on the analyzed results of noise source, was designed to reduce the fan aerodynamic noise, giving the noise reduction mechanism of the steeped tongue. The mechanism of fan noise reduction is that the phase offset of the different segment on the tongue decrease the superposition of pressure fluctuations amplitude in the tongue region.
作者 吴让利
出处 《煤矿机械》 2017年第1期21-23,共3页 Coal Mine Machinery
关键词 离心风机 气动噪声 阶梯蜗舌降噪 centrifugal fan aerodynamic noise noise reduction of steeped tongue
  • 相关文献

参考文献1

二级参考文献18

  • 1Feshe K R,Neise W.Generation mechanisms of low-frequency centrifugal fan noise[J].American Institute of Aeronautics and Astronautics Journal,1999,37(10):1173-1179.
  • 2Velarde-Suárez S,Santolaria-Morros C,Ballesteros-Tajadura R.Experimental study on the aeroacoustic behavior of a forward-curved blades centrifugal fan[J].Journal of Fluids Engineering,1999,121(2):276-281.
  • 3Velarde-Suárez S,Ballesteros-Tajadura R,Santolaria-Morros C,et al.Unsteady flow pattern characteristics downstream of a forward-curved blades centrifugal fan[J].Journal of Fluids Engineering,2001,123(2):265-270.
  • 4Ballesteros-Tajadura R,Velarde-Suárez S,Hurtado-Cruz Juan P.Noise prediction of a centrifugal fan:numerical results and experimental validation[J].Journal of Fluids Engineering,2008,130(9):1-12.
  • 5Younsi M,Bakir F,Kouidri S,et al.Numerical and experimental study of unsteady flow in centrifugal fan[J].Journal of Power and Energy,2007,221(7):1025-1036.
  • 6Lebrun M,Favre C H.Fan-OGV unstrady Navier-Stokes computation using an adapted acoustic mesh[R].AIAA-2004-2995,2004.
  • 7Weckmueller C,Guerin S,Ashcroft G.CFD-CAA coupling apply to DLR UHBR-fan:comparison to experimental data[R].AIAA-2009-3342,2009.
  • 8Khelladi S,Kouidri S,Bakir F,et al.Predicting tonal noise from a high rotational speed centrifugal fan[J].Journal of Sound and Vibration,2008,313(1/2):113-133.
  • 9LIU Qiuhong,QI Datong,TAN Hongtao.Computation of aerodynamic noise of centrifugal fan using LES approach,acoustic analogy and vortex sound theory[J].Journal of Mechanical Engineering Science,2007,221(11):1321-1332.
  • 10Tournour M,El Hachemi Z,Alex R.Investigation of the tonal noise radiated by subsonic fans using the aero-acoustic analogy[C]//Proceeding of Fan Noise International Symposium.Senlis.France:CETIM,2003:1-8.

共引文献5

同被引文献31

引证文献4

二级引证文献30

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部