A novel test rig to investigate under-platform damper dynamics

Abstract In the field of turbomachinery, vibration amplitude is often reduced by dissipating the kinetic energy of the blades with devices that utilize dry friction. Under-platform dampers, for example, are often placed in the underside of two consecutive turbine blades. Dampers are kept in contact with the under-platform of the respective blades by means of the centrifugal force. If the damper is well designed, vibration of blades instigate a relative motion between the under-platform and the damper. A friction force, that is a non-conservative force, arises in the contact and partly dissipates the vibration energy. Several contact models are available in the literature to simulate the contact between the damper and the under-platform. However, the actual dynamics of the blade-damper interaction have not fully understood yet. Several test rigs have been previously developed to experimentally investigate the performance of under-platform dampers. The majority of these experimental setups aim to evaluate the overall damper efficiency in terms of reduction in response amplitude of the blade for a given exciting force that simulates the aerodynamic loads. Unfortunately, the experimental data acquired on the blade dynamics do not provide enough information to understand the damper dynamics. Therefore, the uncertainty on the damper behavior remains a big issue. In this work, a novel experimental test rig has been developed to extensively investigate the damper dynamic behavior. A single replaceable blade is clamped in the rig with a specific clamping device. With this device the blade root is pressed against a groove machined in the test rig. The pushing force is controllable and measurable, to better simulate the actual centrifugal load acting on the blade. Two dampers, one on each side of the blade, are in contact with the blade under-platforms and with platforms on force measuring supports. These supports have been specifically designed to measure the contact forces on the damper. The contact forces on the blade are computed by post processing the measured forces and assuming the static equilibrium of the damper. The damper kinematics is rebuilt by using the relative displacement, measured with a differential laser, between the damper and the blade under-platform. This article describes the main concepts behind this new approach and explains the design and working of this novel test rig. Moreover, the influence of the damper contact forces on the dynamic behavior of the blade is discussed in the result section.

[1]  Muzio Gola,et al.  Measurement of Contact Parameters of Flat on Flat Contact Surfaces at High Temperature , 2012 .

[2]  J. Szwedowicz,et al.  Estimation of Contact Stiffness and its Role in the Design of a Friction Damper , 2001 .

[3]  Walter Sextro,et al.  Optimization of Interblade Friction Damper Design , 2000 .

[4]  Muzio Gola,et al.  Design of a new test rig to evaluate under-platform damper performance - ESDA2010-24268 , 2010 .

[5]  Chia-Hsiang Menq,et al.  The influence of microslip on vibratory response, Part II: A comparison with experimental results , 1986 .

[6]  Teresa Maria Berruti,et al.  A test rig for the investigation of the dynamic response of a bladed disk with underplatform dampers , 2010 .

[7]  Stefano Zucca,et al.  Range of variability in the dynamics of semi-cylindrical friction dampers for turbine blades. , 2008 .

[8]  Christoph W. Schwingshackl,et al.  Measured and estimated friction interface parameters in a nonlinear dynamic analysis , 2012 .

[9]  Stefano Zucca,et al.  The effect of underplatform dampers on the forced response of bladed disks by a coupled static/dynamic harmonic balance method , 2011 .

[10]  Christoph W. Schwingshackl,et al.  Validation of test rig measurements and prediction tools for friction interface modelling , 2010 .

[11]  J. Barbera,et al.  Contact mechanics , 1999 .

[12]  Muzio Gola,et al.  Design of a high-precision, flat-on-flat fretting test apparatus with high temperature capability , 2013 .

[13]  Teresa Maria Berruti,et al.  Investigation on the Dynamic Response of Blades With Asymmetric Under Platform Dampers , 2015 .

[14]  Muzio Gola,et al.  Measurement of the Scatter of Underplatform Damper Hysteresis Cycle: Experimental Approach , 2012 .

[15]  Raymond D. Mindlin,et al.  Compliance of elastic bodies in contact , 1949 .

[16]  Tsuyoshi Murata,et al.  {m , 1934, ACML.

[17]  Muzio Gola,et al.  Test Rig for Wear and Contact Parameters Extraction for Flat-on-Flat Contact Surfaces , 2011 .

[18]  D. J. Ewins,et al.  Measuring the Performance of Underplatform Dampers for Turbine Blades by Rotating Laser Doppler Vibrometer , 2012 .

[19]  Chiara Gastaldi,et al.  Pre Optimization of Asymmetrical Underplatform Dampers , 2016 .

[20]  David J. Ewins,et al.  Underplatform Dampers for Turbine Blades: Theoretical Modeling, Analysis, and Comparison With Experimental Data , 2001 .

[21]  Walter Sextro,et al.  Improved Reliability of Bladed Disks due to Friction Dampers , 1997 .

[22]  J. Szwedowicz,et al.  Numerical and Experimental Damping Assessment of a Thin-Walled Friction Damper in the Rotating Setup With High Pressure Turbine Blades , 2006 .

[23]  Christoph W. Schwingshackl,et al.  Modelling the nonlinear behaviour of an underplatform damper test rig for turbine applications , 2017 .

[24]  Christian Maria Firrone,et al.  Measurement of the kinematics of two underplatform dampers with different geometry and comparison with numerical simulation , 2009 .

[25]  Chiara Gastaldi,et al.  Understanding Complexities in Underplatform Damper Mechanics , 2014 .

[26]  Ning An,et al.  Forced Response Prediction of Constrained and Unconstrained Structures Coupled Through Frictional Contacts , 2009 .

[27]  Chia-Hsiang Menq,et al.  Characterization of Contact Kinematics and Application to the Design of Wedge Dampers in Turbomachinery Blading: Part 2—Prediction of Forced Response and Experimental Verification , 1998 .

[28]  David J. Ewins,et al.  Underplatform Dampers for Turbine Blades: Theoretical Modelling, Analysis and Comparison With Experimental Data , 1999 .

[29]  J. Griffin Friction Damping of Resonant Stresses in Gas Turbine Engine Airfoils , 1980 .

[30]  D. J. Ewins,et al.  Experimental and Numerical Investigation of Rotating Bladed Disk Forced Response Using Underplatform Friction Dampers , 2008 .

[31]  Muzio Gola,et al.  Measurement of Tangential Contact Hysteresis During Microslip , 2004 .

[32]  Muzio Gola,et al.  A direct experimental-numerical method for investigations of a laboratory under-platform damper behavior , 2014 .