Experimental Aeroelastic Investigation of Vibrating Turbine Blade Clusters

The presented work consists of the presentation and discussion of unsteady experimental results of controlled vibration measurements for two single-blade and two cluster test cases subjected to the same subsonic flow conditions. The experiments were performed in a non-rotating annular test facility with the aim of investigating the influence of cluster vibrations on the aerodynamic damping of turbine rotor blades. Two frequently-used blade package types were selected: a two-blade-cluster in bending mode and a four-blade-cluster in torsion mode. In addition, single-blade test cases were investigated serving as reference for the cluster cases. The actuation of the 20 blades was obtained by an electromagnetic excitation system, enabling the adjustment of vibration amplitude and phase for each blade at one vibration frequency. The unsteady measurements obtained include time-synchronous unsteady blade surface pressures and blade displacements resulting in local and global aerodynamic blade damping. The comparison between single-blade and cluster test cases identified similarities with the distribution of local aerodynamic damping on the outer cluster-blades.


Editor(s):
Backman, Jari
Bois, Gérard
Leonard, Olivier
Published in:
10th European Conference on Turbomachinery, 210-221
Presented at:
ETC10 - 10th European Conference on Turbomachinery, Lappeenranta, FI, April 14-19, 2013
Year:
2013
Publisher:
Lappeenranta, FI, Lappeenranta University of Technology
ISBN:
978-952-265-385-7
Keywords:
Laboratories:


Note: The status of this file is: EPFL only


 Record created 2013-04-21, last modified 2018-01-28

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