In the second part of this paper, the application of the proposed dual-interface model to the prediction of the forced response of a blade constrained by wedge dampers will be presented. When considering cyclic loading, the induced friction forces and contact normal loads are combined so as to determine the effective stiffness and damping of the friction interfaces over a cycle of motion. The harmonic balance method is then used to impose the approximate stiffness and damping of the friction interfaces to a linear structure model of the blade. This approach results in a set of nonlinear algebraic equations that can be solved to yield the forced response of the blade excited by harmonic external forces. The predicted forced response can then be used to optimize a given damper design, namely to determine the dynamic weight at which the maximum reduction of resonant response is obtained. In order to illustrate the capacity of the proposed method and to examine its accuracy, the forced response of a test beam is examined. The prediction is also compared with the results of lab tests to validate the proposed dual-interface friction force model.
Skip Nav Destination
ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition
June 2–5, 1997
Orlando, Florida, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7871-2
PROCEEDINGS PAPER
Characterization of Contact Kinematics and Application to the Design of Wedge Dampers in Turbomachinery Blading: Part II — Prediction of Forced Response and Experimental Verification Free
B. D. Yang,
B. D. Yang
The Ohio State University, Columbus, OH
Search for other works by this author on:
C. H. Menq
C. H. Menq
The Ohio State University, Columbus, OH
Search for other works by this author on:
B. D. Yang
The Ohio State University, Columbus, OH
C. H. Menq
The Ohio State University, Columbus, OH
Paper No:
97-GT-020, V004T14A008; 8 pages
Published Online:
December 24, 2014
Citation
Yang, BD, & Menq, CH. "Characterization of Contact Kinematics and Application to the Design of Wedge Dampers in Turbomachinery Blading: Part II — Prediction of Forced Response and Experimental Verification." Proceedings of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award. Orlando, Florida, USA. June 2–5, 1997. V004T14A008. ASME. https://doi.org/10.1115/97-GT-020
Download citation file:
352
Views
Related Proceedings Papers
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)
Characterization of Contact Kinematics and Application to the Design of Wedge Dampers in Turbomachinery Blading: Part 1—Stick-Slip Contact Kinematics
J. Eng. Gas Turbines Power (April,1998)
Forced Response Prediction of Constrained and Unconstrained Structures Coupled Through Frictional Contacts
J. Eng. Gas Turbines Power (March,2009)
Related Chapters
Supporting Systems/Foundations
Handbook on Stiffness & Damping in Mechanical Design
Fatigue Analysis in the Connecting Rod of MF285 Tractor by Finite Element Method
International Conference on Advanced Computer Theory and Engineering, 4th (ICACTE 2011)
Common Compliant Platforms
Offshore Compliant Platforms: Analysis, Design, and Experimental Studies