In this paper, we present a methodology and results from an experimental investigation of forced vibration response for a bladed disk with fitted underplatform “cottage-roof” friction dampers, together with the corresponding numerical predictions. A carefully designed and constructed rotating test rig is used to make precise measurements, which involve only the phenomena of interest. For this purpose, the measurement rig is operated under vacuum to eliminate aerodynamic effects on the rotating blisk and noncontact excitation and measurement techniques are employed so as not to modify the bladed disk dynamics. The experimental data measured are used for validation of multiharmonic balance-based prediction tools developed at the Imperial College. Predictions are carried out both with and without taking inherent mechanical mistuning into account, which is identified from measured data. Measured and predicted response curves are compared with each other and the degree of correlation is discussed.
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e-mail: y.petrov@imperial.ac.uk
e-mail: d.ewins@imperial.ac.uk
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July 2008
Research Papers
Experimental and Numerical Investigation of Rotating Bladed Disk Forced Response Using Underplatform Friction Dampers
Evgeny P. Petrov,
Evgeny P. Petrov
Department of Mechanical Engineering,
e-mail: y.petrov@imperial.ac.uk
Imperial College London
, London SW7 2AZ, UK
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David J. Ewins
David J. Ewins
Department of Mechanical Engineering,
e-mail: d.ewins@imperial.ac.uk
Imperial College London
, London SW7 2AZ, UK
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Ibrahim A. Sever
Evgeny P. Petrov
Department of Mechanical Engineering,
Imperial College London
, London SW7 2AZ, UKe-mail: y.petrov@imperial.ac.uk
David J. Ewins
Department of Mechanical Engineering,
Imperial College London
, London SW7 2AZ, UKe-mail: d.ewins@imperial.ac.uk
J. Eng. Gas Turbines Power. Jul 2008, 130(4): 042503 (11 pages)
Published Online: April 29, 2008
Article history
Revised:
July 30, 2007
Received:
July 30, 2007
Published:
April 29, 2008
Citation
Sever, I. A., Petrov, E. P., and Ewins, D. J. (April 29, 2008). "Experimental and Numerical Investigation of Rotating Bladed Disk Forced Response Using Underplatform Friction Dampers." ASME. J. Eng. Gas Turbines Power. July 2008; 130(4): 042503. https://doi.org/10.1115/1.2903845
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