Flow Fields in an Axial Flow Compressor During Four Quadrant Operation

Abstract

It has been shown in previous investigations that when all combinations of both positive and negative direction of rotation and flow direction are allowed in operating a multistage axial flow compressor, the operating point may be in any of the four quadrants of the pressure rise versus flow characteristic. The present paper is the first discussion of the flow field of all possible modes of operation of an axial flow compressor. During the present study interstage time dependent hot film velocity measurements and five hole pneumatic probe measurements were combined with steady and time dependent CFD solutions to investigate the flow fields in the threestage axial compressor. Results are presented in terms of meanline velocity triangles, mean stream surface plots, midspan radial velocity contours right through the compressor, rotordownstream radial distributions of axial and tangential velocity, statordownstream axial velocity contours and midspan entropy contours through the compressor. Main flow features are pointed out and discussed. The study was instigated in an effort to understand possible accident scenarios in a threeshaft closed cycle nuclear powered helium gas turbine.