期刊文献+

串列叶片式前向离心风机气动与噪声特性的优化研究 被引量:10

Aerodynamics Optimization and Noise Characteristic for Forward-Swept Centrifugal Fan with Tandem Blades
下载PDF
导出
摘要 对采用串列叶片的某前向离心风机内部三维非定常流动进行了数值计算,重点研究了串列叶片不同叶片相对长度和不同叶片相对周向位置两个参数对风机气动性能及气动噪声的影响。通过响应面方法对数值结果进行二次回归拟合,得到两个参数与风机效率和A声级间的函数关系,并进行了优化分析。数值结果表明:两个参数对串列叶片式前向离心风机效率和A声级均有较大影响,合理的串列叶片设计能够在保持气动性能基本不变的情况下降低风机的气动噪声。将可靠的CFD数值技术与响应面方法结合起来用于指导离心风机的改进及试验设计是可行的,本文的研究结果可为串列式离心风机在节能与降噪的总体设计方面提供参考。 A numerical optimization for aerodynamic performance and aerodynamic noise of a forward-swept centrifugal fan with tandem blades is carried out.Three-dimensional unsteady viscous flows are investigated for the whole impeller-volute configuration.The influences of relative length and circumferential position of tandem-blade on the aerodynamic performance and aerodynamic noise of the centrifugal fan,are discussed.And the response surface methodology(RSM)with full factorial designs is used to obtain an approximated efficiency and A-weighted sound pressure level in terms of the two parameters.The analysis shows that the two parameters significantly affect the efficiency and A-weighted sound pressure level of the tandem-blade centrifugal fan.Reasonable tandem-blade designs can lower the aerodynamic noise remaining the aerodynamic performance.The feasible method of reliable CFD technique combined with RSM can be effectively applied to the improvement and experiment design of centrifugal fans.
机构地区 西安交通大学
出处 《应用力学学报》 CAS CSCD 北大核心 2009年第1期40-44,共5页 Chinese Journal of Applied Mechanics
关键词 串列叶片 气动性能 气动噪声 前向离心风机 响应面方法 tandem-blade,aerodynamic performance,aerodynamic noise,forward-swept centrifugal fan,response surface methodology
  • 相关文献

参考文献9

  • 1Neise W. Review of noise reduction methods for centrifugal fans [J]. Journal of Engineering for Industry, 1982, 104(5) : 381-399.
  • 2Neise W. Noise reduction in centrifugal fans: A literature survey[J]. Journal of Sound and Vibration, 1976, 45: 375-403.
  • 3黄东涛,边晓东,唐旭东,卢钰.长短叶片开缝技术在离心风机设计中的应用[J].清华大学学报(自然科学版),1999,39(4):6-9. 被引量:30
  • 4王宝潼,张楚华,席光,刘帆.串列叶片式离心叶轮内流场的数值研究[J].西安交通大学学报,2007,41(11):1275-1278. 被引量:11
  • 5Liu Qiuhong, Qi Datong, Mao Yijun. Numerical calculation of centrifugal fan noise [J]. Proceedings of the Institution of Mechanical Engineers, Part C-Journal of Mechanical Engineering Science, 2006, 220(8) : 1167-1178.
  • 6毛义军,祁大同,刘秋洪.基于非定常流场的离心风机气动噪声分析[J].西安交通大学学报,2005,39(9):989-993. 被引量:61
  • 7Liu Qiuhong, Qi Datong, Tang Hongtao. Computation of aerodynamic noise of centrifugal fan using LES approach, acoustic analogy and vortex sound theory [J]. Proceedings of the Institution of Mechanical Engineers, Part C-Journal of Mechanical Engineering Science, 2007, 221(11) : 1321-1332.
  • 8Han S Y, Maeng J S, Yoo D H. Shape optimization of cutoff in a multiblade fan/scroll system using response surface methodology [J]. Numerical Heat Transfer, Part B, 2003, 43 (1) ; 87-98.
  • 9Kim K Y, Seo S J. Application of numerical optimization technlque to design of forward-curved blades centrifugal fan [J]. Numerical Heat Transfer, Part B, 2006, 49(1): 152-158.

二级参考文献17

  • 1居鸿宾,沈孟育.计算气动声学的问题、方法与进展[J].力学与实践,1995,17(5):1-10. 被引量:15
  • 2唐旭东.具有开缝叶片或长短叶片的离心风机叶轮通道湍流场数值模拟及实验研究[学士学位论文].北京:清华大学工程力学系,1996..
  • 3边晓东.离心风机叶轮通道三维数值模拟初探[学士学位论文].北京:清华大学工程力学系,1995..
  • 4唐旭东,学位论文,1996年
  • 5边晓东,学位论文,1995年
  • 6Jeon W H, Lee D J. An analysis of the flow and aerodynamic acoustic sources of a centrifugal impeller [J].Journal of Sound and Vibration, 1999, 222 (3):505-511.
  • 7Jeon W H, Lee D J. A numerical study on the flow and sound field of centrifugal impeller near a wedge[J]. Journal of Sound and Vibration, 2003,266(4):785-804.
  • 8Miche R. Broad band fan noise prediction using singleairfoil theory[A]. Fan Noise 2nd International Symposinm, Senlis, France, 2003.
  • 9Bache G. Impeller tandem blade study with grid embedding for local grid refinement[C] // Proceedings of the Tenth Workshop for Computational Fluid Dynamics Applications in Rocket Propulsion: Part1. Sacramento, USA: NASA Conference Publication, 1992: 259-288.
  • 10Josuhn-Kadner B. Flow field and performance of a centrifugal compressor rotor with tandem blades of adjustable geometry, ASME Paper 94-GT-13 [R]. New York: ASME Publication, 1994.

共引文献95

同被引文献103

引证文献10

二级引证文献54

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