期刊文献+

6kW静音型柴油发电机组排风通道风阻仿真研究

Numerical Simulation on the Air Resistance of Exhaust Channel in 6 kW Silent Canopy Diesel Generator Set
在线阅读 下载PDF
导出
摘要 为了研究6 kW静音型柴油发电机组排风通道结构对空气流动阻力的影响,通过计算流体力学方法(CFD)分析排风通道内流体模型的压力场和流场分布,研究了排风通道内风阻的影响因素。通过改变阻风板、消声器相对位置和排风出口形状、尺寸,对比风阻变化及流体流速变化。结果表明移动阻风板,扩大排风通道体积及移动消声器相对阻风板的距离可以减小风阻,同时增大排风出口处U型挡板宽度可以减小风阻,当不考虑排风出口处吸音海绵表面粗糙度时其厚度对风阻影响不大。为排风通道结构设计和优化提供理论依据。 In order to study the impacts on the air resistance which from the structural parameters of exhaust chan- nel in 6 kW silent canopy diesel generator set, the pressure field and flow field of the exhaust channel are analyzed with the help of the Computational fluid dynamics (CFD) method to study the factors which affect the air resist- ance. By changing the location of the wind resistance board or the muffler, the size of exhaust export shape, air flu- id model in the exhaust channel is numerically simulated and the results of air resistance and flow field are com- pared. The results show that air resistance can be reduced by moving the wind resistance board to expand the ex- haust channel's volume, adjusting the location of muffler, increasing the distance between intakes and the U- shaped baffle can reduce air resistance; when the surface roughness of the sound-absorbing sponge isn't consid- ered ; changing the thickness has little effect on air resistance. sign and parameter optimization of exhaust channel. And it provides the theoretical basis for structure de-
出处 《机械科学与技术》 CSCD 北大核心 2013年第7期1006-1012,共7页 Mechanical Science and Technology for Aerospace Engineering
关键词 阻力 计算流体力学 模型 优化 computer simulation optimization flow fields air resistance computational fluid dynamics model exhaust channel silent canopy diesel generator
  • 相关文献

参考文献8

  • 1Yuan Y,Jackson A,Nelson M.CFD Simulation of Flow andHeat Transfer in Airways[R].SAE Technical Paper,2001-01-1712.
  • 2Halici F,Taymaz I,Gunduz M.The effect of the number of tuberows on heat,mass and momentum transfer in flat-plate finnedtube heat exchanges[J].Energy,2001,26(11):963~972.
  • 3Kim M H,Bullard C W.Air-side thermal hydraulic performanceof multi-louvered fin aluminum heat exchangers[J].Interna-tional Journal of Refrigeration,2002,25(3):390~400.
  • 4刘蕾,王永军,闵荣,吴建中.基于响应面法的梯形直肋散热板优化设计[J].机械科学与技术,2011,30(7):1168-1170. 被引量:7
  • 5Tai C,Cheng C,Liao C.A Practical and Simplified AirflowSimulation to Assess Underhood Cooling Performence[R].SAE Technical Paper,2007-01-1402.
  • 6张毅,俞小莉,陆国栋,夏立峰,蒋平灶.间距对散热器模块匹配性能影响的试验研究[J].内燃机工程,2006,27(5):46-49. 被引量:11
  • 7Allen D A,Lasecki M P.Thermal Management Evollutionand Controlled Coolant Flow[R].SAE Technical Paper,2001:SAE,2001-01-1732.
  • 8姚仲鹏,王新国.车辆冷却传热[M].北京:北京大学出版社,2011.

二级参考文献26

  • 1陆国栋,俞小莉,张毅,李迎.装载机冷却组优化匹配的试验研究[J].内燃机工程,2005,26(4):47-49. 被引量:15
  • 2Harris T A. Roiling Bearing Amdysis [M]. Wiley, 1966.
  • 3Cooper D H. Hertzian contact-stress deformation coefficients[J]. ASME Journal of Applied Mechanics, 1956,36:296 - 603.
  • 4Roark R J, Young W C. Formulas for Stress and Strain[M]. McGaw-Hill, 5th Ed. , 1975, 516 -518.
  • 5Brewe D E, Hamrock B J. Simplified solution for elliptical-con- tact deformation between two elastic solids [ J ]. ASME Journal of Triboiogy, 1977,99:485 -487.
  • 6Hanm~k B J, Brewe D E. Simplified solution for stresses and deformations [ J ]. ASME Journal of Lubrication Technology, 1983,105:171 -177.
  • 7Greenwood J A. Formulas for moderately elliptical Hertzian con- tacts [ J ]. ASME Journal of Tribology, 1985,107:501 - 504.
  • 8Greenwood J A. Analysis of elliptical Herzian contacts[J]. Tri- boiogy International, 1997,30 ( 3 ) :235 - 237.
  • 9Markho P H. Highly accurate formulas for rapid calculation of the key geometrical parameters of elliptic Hertzian contacts [ J ]. ASME Journal of Triboiogy, 1987,109:640-647.
  • 10Dyson A, Evans H P, Snidle R F. A simple, accurate method for calculation of stresses and deformations in elliptical Herzian contacts [ J ]. Journal of Mechanical Engineering and Sci- ence, 1992,206:139 - 141.

共引文献16

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