Multi-point Optimization of Recirculation Flow Type Casing Treatment in Centrifugal Compressors

被引:0
作者
Min Thaw Tun
Daisaku Sakaguchi
机构
[1] NagasakiUniversity
关键词
Centrifugal Compressor; Casing Treatment; Multi-point Optimization; Turbocharger;
D O I
暂无
中图分类号
TH452 [离心式];
学科分类号
080704 ;
摘要
High-pressure ratio and wide operating range are highly required for a turbocharger in diesel engines.A recirculation flow type casing treatment is effective for flow range enhancement of centrifugal compressors.Two ring grooves on a suction pipe and a shroud casing wall are connected by means of an annular passage and stable recirculation flow is formed at small flow rates from the downstream groove toward the upstream groove through the annular bypass.The shape of baseline recirculation flow type casing is modified and optimized by using a multi-point optimization code with a metamodel assisted evolutionary algorithm embedding a commercial CFD code CFX from ANSYS.The numerical optimization results give the optimized design of casing with improving adiabatic efficiency in wide operating flow rate range.Sensitivity analysis of design parameters as a function of efficiency has been performed.It is found that the optimized casing design provides optimized recirculation flow rate,in which an increment of entropy rise is minimized at grooves and passages of the rotating impeller.
引用
收藏
页码:231 / 241
页数:11
相关论文
共 9 条
[1]  
Suppression of Unstable Flow at Small Flow Rates in a Centrifugal Blower by Controlling Tip Leakage Flow and Reverse Flow. M.Ishida,T.Surana,H.Ueki,D.Sakaguchi. ASME Journal of Turbomachines . 2005
[2]   Numerical study on the range enhancement of a centrifugal compressor with a ring groove system [J].
Park, Chi-Yong ;
Choi, Young-Seok ;
Lee, Kyoung-Yong ;
Yoon, Joon-Yong .
JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2012, 26 (05) :1371-1378
[3]  
Effect of Recirculation Device With Counter Swirl Vane on Performance of High Pressure Ratio Centrifugal Compressor. Tamaki,Hideaki. Journal of Turbomachinery . 2012
[4]  
Map Width Enhancement Technique for a Turbocharger Compressor. Subenuka S,Stephen S,Julian E. Transaction of the ASME,Journal of Turbomachinery . 2013
[5]  
Improvement in the performance of a high pressure ratio turbocharger centrifugal compressor by blade bowing and self-recirculation casing treatment. Xinqian Zheng,Chuanjie Lan. The Journal of Automatic Chemistry . 2013
[6]  
Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control—Part n. Xinqian Zheng,et al. Transaction of the ASME,Journal of Turbomachinery . 2011
[7]  
Effect of Guide Vane in Ring Groove Arrangement for a Small Turbocharger. Sakaguchi D,Nagoshi K,Tanimuar M,Ishida M,Ueki H. Proceedings of the 10- (th)Asian Internal Conference on Fluid Machinery (AICFM10) . 2009
[8]  
Application of Map Width Enhancement Devices to Turbocharger Compressor Stages. FISHER,F. B. SAE Paper,No.880794 . 1988
[9]  
Stability Improvement of High-Pressure-Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control—Part I. Xinqian Zheng et al. Transaction of the ASME,Journal of Turbomachinery . 2011