Design Optimization and Experimental Study of Tandem Impeller for Centrifugal Compressor

Although significant advances have been made in tandem-blade technology for axial compressors, few efforts were devoted to its application in centrifugal compressors. Based on detailed computational fluid dynamics simulations and sensitivity analysis, multiobjective design optimization is conducted for a tandem impeller. An optimized tandem impeller, for which the objectives are all better than those of the baseline, is fabricated and tested on a high-speed centrifugal compressor rig. The numerical results show that the baseline tandem impeller has more uniform discharge flow but lower efficiency than the corresponding splitter impeller. The geometries of the inducer blade profile and inducer–exducer gap are found to have the greatest impact on the tandem impeller efficiencies. By optimization, the tandem impeller efficiency can be increased through reduced curvature of the blade profile at the inducer hub, S-shaped blade angle distribution at the inducer tip, and increased blade angle at the exducer tip ...

[1]  J. R. Wood,et al.  Experimental performance of a 13.65-centimeter-tip-diameter tandem-bladed sweptback centrifugal compressor designed for a pressure ratio of 6 , 1977 .

[2]  Yaping Ju,et al.  Multi-Objective Optimization Design Method for Tandem Compressor Cascade at Design and Off Design Conditions , 2010 .

[3]  Hiroaki Hasegawa,et al.  Development of Highly Loaded Fan with Tandem Cascade , 2003 .

[4]  Burkhard Josuhn-Kadner Flow Field and Performance of a Centrifugal Compressor Rotor With Tandem Blades of Adjustable Geometry , 1994 .

[5]  M. V. Casey A Computational Geometry for the Blades and Internal Flow Channels of Centrifugal Compressors , 1983 .

[6]  Sanford Fleeter,et al.  High Speed Centrifugal Compressor Aeromechanics - Impeller Unsteady Aerodynamics , 2007 .

[7]  Jack L. Kerrebrock,et al.  Experimental Investigation of a High Pressure Ratio Aspirated Fan Stage , 2005 .

[8]  B. Josuhn-Kadner,et al.  Investigations on a Radial Compressor Tandem Rotor Stage with Adjustable Geometry. , 1993 .

[9]  Reza S. Abhari,et al.  Clearance Effects on the Onset of Instability in a Centrifugal Compressor , 2008 .

[10]  Y P Ju,et al.  Multi-point and multi-objective optimization design method for industrial axial compressor cascades , 2011 .

[11]  Lennart S. Hultgren,et al.  Demonstration of Separation Delay With Glow-Discharge Plasma Actuators , 2003 .

[12]  K. Bammert,et al.  Investigations of an Axial Flow Compressor with Tandem Cascades , 1980 .

[13]  Akira Nishida Investigation of flow in centrifugal impeller with tandem inducer , 1976 .

[14]  J. A. Brent Single-stage experimental evaluation of compressor blading with slots and vortex generators. Part 3 - Data and performance for stage 4 , 1970 .

[15]  J. A. Brent,et al.  Single-stage experimental evaluation of tandem-airfoil rotor and stator blading for compressors, part 8 , 1974 .

[16]  Yaping Ju,et al.  Optimization of Centrifugal Impellers for Uniform Discharge Flow and Wide Operating Range , 2012 .

[17]  Meinhard T. Schobeiri Turbomachinery Flow Physics and Dynamic Performance , 2004 .

[18]  Koji Nakagawa,et al.  An aerodynamic investigation of a centrifugal compressor for HCFC123 , 1992 .

[19]  Guang Xi,et al.  Optimization of High Speed Centrifugal Compressor for a Micro Gas Turbine Based on CFD and FEM Analysis , 2010 .

[20]  Douglas A. Roberts,et al.  Numerical Investigation of Tandem-Impeller Designs for a Gas Turbine Compressor , 2001 .

[21]  Steven R. Wellborn,et al.  Numerical Investigation of Tandem Airfoils for Subsonic Axial-Flow Compressor Blades , 2009 .