An Experimental Investigation on the Dynamic Response Variability of a Turbine Blade With Midspan Dampers

Author:

Ferhatoglu Erhan1,Botto Daniele1,Zucca Stefano1

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Politecnico di Torino , Italy Corso Duca degli Abruzzi 24, Torino 10129, Italy

Abstract

Abstract This paper addresses two main subjects. First, a novel test setup is described to experimentally study the nonlinear dynamic behavior of a turbine blade coupled with two midspan dampers (MSDs). To this end, a representative turbine blade and midspan friction dampers are originally designed, and they are assembled to a special test rig which has been previously developed at Politecnico di Torino. Second, the variability of the dynamic response is intensively investigated with a purposely defined loading/unloading strategy. To better understand the inherent kinematics of the blade–damper interaction, contact forces are measured through the novel design of the experimental campaign. It is shown that multiple responses, which are obtained in different tests while keeping all user-controlled inputs nominally same, are due to nonunique contact forces that provide different static force equilibria on the damper. This outcome is further supported by the qualitative illustration of hysteresis cycles. This study contributes to the understanding of the response repeatability linked to the nonuniqueness of friction forces.

Publisher

ASME International

Subject

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

Reference22 articles.

1. High Cycle Fatigue in Aircraft Gas Turbines—An Industry Prospective;Int. J. Fract.,1996

2. Flutter and Resonant Vibration Characteristics of Engine Blades;ASME J. Eng. Gas Turbines Power,1997

3. Asymmetrical Underplatform Dampers in Gas Turbine Bladings: Theory and Application,2004

4. Forced Response Prediction of Constrained and Unconstrained Structures Coupled Through Frictional Contacts;ASME J. Eng. Gas Turbines Power,2009

5. Forced Response Analysis of Integrally Bladed Disks With Friction Ring Dampers;J. Vib. Acoust.,2010

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