Friction dampers are often used in turbine design to attenuate blade vibration to acceptable levels so as to prolong blades’ service life. A wedge damper, also called a self-centering, blade-to-blade damper, can provide more design flexibility to meet various needs in different operating conditions when compared with conventional platform dampers. However, direct coupling of the two inclined friction interfaces of the wedge damper often leads to very complex contact kinematics. In Part I of this two-part paper, a dual-interface friction force model is proposed to investigate the coupling contact kinematics. The key issue of the model formulation is to derive analytical criteria for the stick-slip transitions that can be used to precisely simulate the complex stick-slip motion and, thus, the induced friction force as well. When considering cyclic loading, the induced periodic friction forces can be obtained to determine the effective stiffness and damping of the interfaces over a cycle of motion. In Part II of this paper, the estimated stiffness and damping are then incorporated with the harmonic balance method to predict the forced response of a blade constrained by wedge dampers.
Skip Nav Destination
Article navigation
April 1998
Research Papers
Characterization of Contact Kinematics and Application to the Design of Wedge Dampers in Turbomachinery Blading: Part 1—Stick-Slip Contact Kinematics
B. D. Yang,
B. D. Yang
Department of Mechanical Engineering, The Ohio State University, Columbus, OH 43210
Search for other works by this author on:
C. H. Menq
C. H. Menq
Department of Mechanical Engineering, The Ohio State University, Columbus, OH 43210
Search for other works by this author on:
B. D. Yang
Department of Mechanical Engineering, The Ohio State University, Columbus, OH 43210
C. H. Menq
Department of Mechanical Engineering, The Ohio State University, Columbus, OH 43210
J. Eng. Gas Turbines Power. Apr 1998, 120(2): 410-417 (8 pages)
Published Online: April 1, 1998
Article history
Received:
July 1, 1997
Online:
November 19, 2007
Citation
Yang, B. D., and Menq, C. H. (April 1, 1998). "Characterization of Contact Kinematics and Application to the Design of Wedge Dampers in Turbomachinery Blading: Part 1—Stick-Slip Contact Kinematics." ASME. J. Eng. Gas Turbines Power. April 1998; 120(2): 410–417. https://doi.org/10.1115/1.2818138
Download citation file:
Get Email Alerts
Characterization of Knocking Pressure Data From Two Closely Spaced Transducers: Effect of Transducer Mounting
J. Eng. Gas Turbines Power (September 2025)
Comparison of a Full-Scale and a 1:10 Scale Low-Speed Two-Stroke Marine Engine Using Computational Fluid Dynamics
J. Eng. Gas Turbines Power (September 2025)
An Adjustable Elastic Support Structure for Vibration Suppression of Rotating Machinery
J. Eng. Gas Turbines Power (September 2025)
Related Articles
Characterization of Contact Kinematics and Application to the Design of Wedge Dampers in Turbomachinery Blading: Part 2—Prediction of Forced Response and Experimental Verification
J. Eng. Gas Turbines Power (April,1998)
Effects of Contact Interface Parameters on Vibration of Turbine Bladed Disks With Underplatform Dampers
J. Eng. Gas Turbines Power (March,2012)
Convergence Behaviors of Reduced-Order Models For Frictional
Contacts
J. Vib. Acoust (August,2005)
Forced Response Prediction of Constrained and Unconstrained Structures Coupled Through Frictional Contacts
J. Eng. Gas Turbines Power (March,2009)
Related Proceedings Papers
Related Chapters
Materials
Design and Application of the Worm Gear
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Summary
Heat Transfer & Hydraulic Resistance at Supercritical Pressures in Power Engineering Applications