Experimental and Numerical Investigation of Rotating Bladed Disk Forced Response Using Underplatform Friction Dampers

Author:

Sever Ibrahim A.1,Petrov Evgeny P.2,Ewins David J.2

Affiliation:

1. Rolls-Royce plc, P.O. Box 31, Derby DE24 8BJ UK

2. Department of Mechanical Engineering, Imperial College London, London SW7 2AZ, UK

Abstract

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.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference22 articles.

1. Experimental Evaluation of Damping in a Bladed Disk Model;Jaiswal;J. Sound Vib.

2. Modal Test Experience With a Jet Engine Fan Model;Hollkamp;J. Sound Vib.

3. Hollkamp, J. J., and Gordon, R. W., 1998, “An Experimental Investigation of Non-Uniform Damping in Bladed Disks,” Paper No. IAA-98–3747.

4. A Test Rig for Frictionally Damped Bladed Segments;Berruti

5. Underplatform Damper Performance With Turbine Blades;Berruti

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