A Systematic Approach to Estimate the Impact of the Aerodynamic Force Induced by Rotating Stall in a Vaneless Diffuser on the Rotordynamic Behavior of Centrifugal Compressors

One of the main challenges of the present industrial research on centrifugal compressors is the need of extending the left margin of the operating range of the machines. As a result, interest is being paid in accurately evaluating the amplitude of the pressure fluctuations caused by rotating stall, which usually occurs prior to surge. The related aerodynamic force acting on the rotor can produce subsynchronous vibrations, which can prevent the machine to further operate, in case their amplitude is too high. These vibrations are often contained thanks to the stiffness of the oil journals.Centrifugal compressors design is, however, going towards alternative journal solutions having lower stiffness levels (e.g. Active Magnetic Bearings or Squeeze Film Dampers), which hence will be more sensitive to this kind of excitation: consequently, a more accurate estimation of the expected forces in presence of dynamic external forces like those connected to an aerodynamically unstable condition is needed to predict the vibration level and the compressor operability in similar conditions.Within this scenario, experimental tests were carried out on an industrial impeller operating at high peripheral Mach number. The dedicated test rig was equipped with several dynamic pressure probes that were inserted in the gas flow path; moreover, the rotor vibrations were constantly monitored with typical vibration probes located near the journal bearings.The pressure field induced by the rotating stall in the vaneless diffuser was reconstructed by means of an ensemble average approach, defining the amplitude and frequency of the external force acting on the impeller. The calculated force value was then included in the rotordynamic model of the test rig: the predicted vibrations on the bearings were compared with the measurements, showing satisfactory agreement.Finally, the prospects of the proposed approach are discussed by investigating the response of a real machine in high-pressure functioning when different choices of journal bearings are made.© 2013 ASME

[1]  A. N. Abdelhamid Effects of Vaneiess Diffuser Geometry on Flow Instability in Centrifugal Compression Systems , 1981 .

[2]  B. Perlman,et al.  A phase-locking technique for estimating the ensemble average of time-series data , 1977 .

[3]  Rinpei Kawashita,et al.  Prediction of Subsynchronous Rotor Vibration Amplitude Caused by Rotating Stall , 2008 .

[4]  Giovanni Ferrara,et al.  Rotating Stall in Centrifugal Compressor Vaneless Diffuser: Experimental Analysis of Geometrical Parameters Influence on Phenomenon Evolution , 2004 .

[5]  W. Jansen Rotating Stall in a Radial Vaneless Diffuser , 1964 .

[6]  James M. Sorokes,et al.  A Review of Aerodynamically Induced Forces Acting on Centrifugal Compressors, and Resulting Vibration Characteristics of Rotors , 2000 .

[7]  Thomas Alban,et al.  Rotordynamic Evaluation of Full Scale Rotor on Tilting Pad Bearings With Integral Squeeze Film Dampers , 2012 .

[8]  H. Ohashi,et al.  Rotordynamic Fluid Force Moments on an Open-type Centrifugal Compressor Impeller in Precessing Motion , 2001 .

[9]  博美 小林,et al.  遠心圧縮機の旋回失速に関する研究 : 第2報, 羽根なしディフューザ入口形状の影響 , 1990 .

[10]  博美 小林,et al.  遠心圧縮機の旋回失速に関する研究 : 第1報, 羽根なしディフューザ流路幅の影響 , 1988 .

[11]  Boaz Porat,et al.  Digital Processing of Random Signals: Theory and Methods , 2008 .

[12]  Alvin W. Drake,et al.  Fundamentals of Applied Probability Theory , 1967 .

[13]  Leonardo Ishimoto,et al.  Early Detection Of Rotating Stall Phenomenon In Centrifugal Compressors By Means Of ASME PTC 10 Type 2 Test , 2012 .

[14]  Giovanni Ferrara,et al.  Experimental Investigation and Characterization of the Rotating Stall in a High Pressure Centrifugal Compressor: Part I — Influence of Diffuser Geometry on Stall Inception , 2002 .

[15]  J. C. Wachel,et al.  NONSYNCHRONOUS FORCED VIBRATION IN CENTRIFUGAL COMPRESSORS , 1983 .

[16]  Giacomo Bruno Azzurro Persico,et al.  Unsteady Flow Field Measurements In An Industrial Centrifugal Compressor , 2010 .