期刊文献+

延长叶轮盘、盖尺寸对离心压缩机模型级性能影响研究(英文)

Effect of Impeller Extended Hub and Shroud on Centrifugal Compressor Stage Performance
下载PDF
导出
摘要 CFD method was employed to analyze the effect of the wall extension of hub and shroud at the impeller outlet(rotating diffuser)in a centrifugal compressor model stage with a large mass flow coefficient.The effect of clearance leakage was considered.Results show that the extended hub and shroud increases the head coefficient and ploytropic efficiency for the centrifugal compressor stage,and the extension length is longer,the head coefficient and ploytropic efficiency is higher.When extension length is under 4.44%impeller outlet diameter(R2),the increase rate of head coefficient and polytropic efficiency is rapid.When the extension length is beyond 4.44%R2,the rate is slowed down.The uniformity at the diffuser inlet is to be improved,the total pressure loss of stationary parts decreases,and then the performance of stage is improved.The total pressure loss of stationary parts starts to reduce with the increase of mass flow coefficient when the extension length exceeds 5.56%R2 and mass flow coefficientis beyond the design value of 0.1957. CFD method was employed to analyze the effect of the wall extension of hub and shroud at the impeller outlet(rotating diffuser)in a centrifugal compressor model stage with a large mass flow coefficient. The effect of clearance leakage was considered. Results show that the extended hub and shroud increases the head coefficient and ploytropic efficiency for the centrifugal compressor stage, and the extension length is longer, the head coefficient and ploytropic efficiency is higher. When extension length is under 4.44% impeller outlet diameter(R2), the increase rate of head coefficient and polytropic efficiency is rapid. When the extension length is beyond 4.44% R2, the rate is slowed down. The uniformity at the diffuser inlet is to be improved, the total pressure loss of stationary parts decreases, and then the performance of stage is improved.The total pressure loss of stationary parts starts to reduce with the increase of mass flow coefficient when the extension length exceeds 5.56% R2 and mass flow coefficientis beyond the design value of 0.1957.
作者 刘艳 赵鹏飞 刘啸 王杨 石海 Yan Liu;Peng-fei Zhao;Xiao Liu;Yang Wang;Hai Shi
出处 《风机技术》 2019年第5期28-34,共7页 Chinese Journal of Turbomachinery
基金 NSFC-liaoning Joint Fund U1808214
关键词 Shrouded CENTRIFUGAL COMPRESSOR Numerical Simulation CLEARANCE LEAKAGE LEAKAGE COEFFICIENT Large MASS Flow COEFFICIENT Shrouded Centrifugal Compressor Numerical Simulation Clearance Leakage Leakage Coefficient Large Mass Flow Coefficient
  • 相关文献

参考文献2

二级参考文献29

  • 1康顺,刘强,祁明旭.一个高压比离心叶轮的CFD结果确认[J].工程热物理学报,2005,26(3):400-404. 被引量:37
  • 2彭森,杨策,马朝臣.离心压气机叶尖间隙泄漏流动数值研究[J].工程热物理学报,2005,26(6):935-937. 被引量:15
  • 3杜建一,汤华,赵晓路,徐建中.叶顶间隙对离心压气机性能影响的研究[J].工程热物理学报,2006,27(4):583-585. 被引量:24
  • 4HIRANO T, GUO Zenglin, KIRK R G. Application of computational fluid dynamics analysis for rotating machinery--part Ⅱ : labyrinth seal analysis[C]//2003 International Joint Power Generation Conference. Norcross, GA, USA: ASME IGTI, 2003:661-667.
  • 5DAVID L, RHODE J, WAYNE J. Measured flow oscillations and instabilities in labyrinth seal cavities [J]. AIAA Journal of Propulsion and Power, 2002, 18 (6) :1267-1272.
  • 6GAMAL A J M, VANCE J M. Labyrinth seal leakage tests: tooth profile, tooth thickness, and eccentricity effects[J]. ASME Journal of Engineering for Gas Turbines and Power, 2008, 130(1):012510.
  • 7VAKILI A D, MEGANATHAN A J, MICHAUD M, et al. An experimental and numerical study of labyrinth seal flow [C] // Proceedings of ASME Turbo Expo. New York, USA: ASME, 2005:1121-1128.
  • 8MISCHO B, RIBI B. Influence of labyrinth seal leakage on centrifugal compressor performance[C] // Proceedings of ASME Turbo Expo. New York, USA: ASME, 2009 : 1283-1293.
  • 9WANG Zhiheng, XU Liqun, XI Gang. Numerical investigation on the labyrinth seal leakage for a low flow coefficient centrifugal compressor[C]//Proceedings of ASME Turbo Expo: Power for Land, Sea and Air. New York, USA: ASME, 2010:23096.
  • 10刘瑞韬.离心压缩机内部三维复杂流动的数值模拟及PIV实验研究[D].西安:西安交通大学,2005.

共引文献22

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