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Effects of Blade Counts and Clocking on the Unsteady Profile Pressure Distribution in an Axial-Radial Combined Compressor

[+] Author Affiliations
Ben Zhao, Ce Yang, Liangjun Hu, Dazhong Lao

Beijing Institute of Technology, Beijing, China

Paper No. GT2013-94251, pp. V06CT42A007; 14 pages
doi:10.1115/GT2013-94251
From:
  • ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
  • Volume 6C: Turbomachinery
  • San Antonio, Texas, USA, June 3–7, 2013
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-5524-9
  • Copyright © 2013 by ASME

abstract

A new hypothesis is presented for the superimposed effects of the blade pressure distribution in a multistage compressor. The effects of the unsteady pressure fluctuations on the blade surface are separated into three groups. The influences of the upstream or downstream rotors can be obtained by numerical simulation for the R/S or S/R configuration; the data produced by all the influences can be obtained from the R/S/R configuration. The effects of the blade counts and clocking on the superimposed effects, acting on the profile pressure distribution, are studied using a special data analysis method that had been previously developed by the authors. The results indicate that the blade counts of the upstream and downstream rotors determine the periods of the unsteady pressure fluctuations on the stator surface. The clocking moving blade rows modulate the relative superimposed phases and interactions between two rotors such that the unsteady pressure fluctuates with different amplitudes on the surface of the stator blade.

Copyright © 2013 by ASME

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