Similarity and cascade flow characteristics of a highly loaded helium compressor

Abstract Helium compressor is a major component of the Power Conversion Unit (PCU) used in a High Temperature Gas Cooled Reactor (HTGR). Because the high cost of closed cycle test and leakage problem of helium gas, air could be used as working fluid instead of helium in compressor performance tests. However, the properties of Helium are largely different from those of air, e.g. the adiabatic exponent of Helium is 1.6, while the adiabatic exponent itself is a criterion of similarity between the two compressors. The characteristics of compressor will be different due to the effect of the adiabatic exponent of working fluid, especially for highly loaded compressor working at higher inlet Mach number. In this paper, a theoretical study on the similarity between air compressor and a highly loaded helium compressor is carried out and the deviation of similarity is analyzed. Numerical simulations are then used to confirm the theoretical analysis. The results indicate that the similarity deviation could not be neglected for highly loaded compressor cascade, which means the experience and experimental results of those conventional air compressor cannot be applied directly to the design of highly loaded helium compressor. The flow characteristics of a highly loaded helium compressor at different Reynolds numbers, attack angles, Mach numbers and cascade geometries are then investigated.

[1]  S. A. Sjolander,et al.  Effect of the specific heat ratio on the aerodynamic performance of turbomachinery , 2005 .

[2]  Jenny Persson,et al.  Power Conversion System (PCS) Options for Generation IV Nuclear Plant , 2009 .

[3]  Steven Deutsch,et al.  The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 1—A Unique Experimental Facility , 1987 .

[4]  A. I. van Heek ACACIA: A Small Scale Nuclear Power Plant With Cogeneration Capabilities , 2002 .

[5]  Kazuhiko Kunitomi,et al.  Aerodynamic Design, Model Test, and CFD Analysis for a Multistage Axial Helium Compressor , 2008 .

[6]  Mohamed S. El-Genk,et al.  Axial flow, multi-stage turbine and compressor models , 2010 .

[7]  Robert Dobson PBMR Technology Development Projects at Stellenbosch University, South Africa , 2008 .

[8]  Yang Xu,et al.  Technical design and principle test of active magnetic bearings for the turbine compressor of HTR-10GT , 2012 .

[9]  Isao Minatsuki,et al.  Improvement in the Design of Helium Turbine for the HTGR-GT Power Plant , 2001 .

[10]  Suyuan Yu,et al.  HTGR PROJECTS IN CHINA , 2007 .

[11]  Qun Zheng,et al.  Off-design performance research of an axial helium compressor for HTGR-10 power conversion unit , 2010 .

[12]  Reiner Kuhr,et al.  PBMR Desalination Options: An Economic Study , 2008 .

[13]  Qun Zheng,et al.  Highly loaded aerodynamic design and three dimensional performance enhancement of a HTGR helium compressor , 2012 .

[14]  S. E. Belov,et al.  Development of the GT-MHR Turbo Machine , 2009 .

[15]  Fabrice Bentivoglio,et al.  Validation of the Cathare2 Code Against Oberhausen II Data , 2008 .

[16]  Peigang Yan,et al.  Numerical investigation of influence of rotor/stator interaction on blade boundary layer flow in a low speed compressor , 2011 .

[17]  W. Nitsche,et al.  Wall Shear Stress Measurements on a Highly Loaded Compressor Cascade , 2013 .

[18]  Limin Xu,et al.  Optimization Design for a New Cascade of Helium Compressor With Enhanced Pressure Ratio , 2010 .

[19]  N Csic,et al.  A Study of Similarity Problems Concerning the Working Media Helium and Air in an Axial-flow Compressor , 2008 .

[20]  Mohamed S. El-Genk,et al.  On the Performance of Very High Temperature Reactor Plants With Direct and Indirect Closed Brayton Cycles , 2010 .

[21]  Fabrice Bentivoglio,et al.  Study of nitrogen injection to enhance forced convection for gas fast reactors , 2011 .