A transverse shaft crack in a rotor is usually modeled as a local change in shaft stiffness. This local stiffness change is not constant and varies as a result of a so-called breathing mechanism, explained with periodical opening and closing of crack faces under the load of external forces applied to the rotor. The rotor with a periodically varied stiffness can be modeled as a parametrically excited linear system. In the presence of a parametric excitation, the vibrations of the system can be amplified or damped at specific excitation frequencies. Usually, the frequencies at which the vibrations are amplified are important, since they can affect stability of the system. However, the increased damping at specific frequencies is a significant feature of a parametrically excited system that can have some potentially useful applications. One of such applications can be an early detection of a shaft crack. This paper presents results of numerical analysis of the influence of Rayleigh's damping and gyroscopic effects on the increase in damping in a parametrically excited rotor with a cracked shaft. It is shown that the increase in damping in a parametrically excited system is rather a rare phenomenon that can be observed only at properly selected values of the excitation frequency and Rayleigh's damping. Furthermore, gyroscopic effects influence the exact values of antiresonance frequencies at which the phenomenon appears.
Skip Nav Destination
Article navigation
January 2017
Research-Article
Parametrically Induced Damping in a Cracked Rotor
Zbigniew Kulesza,
Zbigniew Kulesza
Faculty of Mechanical Engineering,
Bialystok University of Technology,
Bialystok 15-351, Poland
e-mail: z.kulesza@pb.edu.pl
Bialystok University of Technology,
Bialystok 15-351, Poland
e-mail: z.kulesza@pb.edu.pl
Search for other works by this author on:
Jerzy T. Sawicki
Jerzy T. Sawicki
Fellow ASME
Center for Rotating Machinery Dynamics and
Control (RoMaDyC),
Washkewicz College of Engineering,
Cleveland State University,
Cleveland, OH 44115-2214
e-mail: j.sawicki@csuohio.edu
Center for Rotating Machinery Dynamics and
Control (RoMaDyC),
Washkewicz College of Engineering,
Cleveland State University,
Cleveland, OH 44115-2214
e-mail: j.sawicki@csuohio.edu
Search for other works by this author on:
Zbigniew Kulesza
Faculty of Mechanical Engineering,
Bialystok University of Technology,
Bialystok 15-351, Poland
e-mail: z.kulesza@pb.edu.pl
Bialystok University of Technology,
Bialystok 15-351, Poland
e-mail: z.kulesza@pb.edu.pl
Jerzy T. Sawicki
Fellow ASME
Center for Rotating Machinery Dynamics and
Control (RoMaDyC),
Washkewicz College of Engineering,
Cleveland State University,
Cleveland, OH 44115-2214
e-mail: j.sawicki@csuohio.edu
Center for Rotating Machinery Dynamics and
Control (RoMaDyC),
Washkewicz College of Engineering,
Cleveland State University,
Cleveland, OH 44115-2214
e-mail: j.sawicki@csuohio.edu
Contributed by the Structures and Dynamics Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received June 21, 2016; final manuscript received June 22, 2016; published online August 16, 2016. Editor: David Wisler.
J. Eng. Gas Turbines Power. Jan 2017, 139(1): 012505 (8 pages)
Published Online: August 16, 2016
Article history
Received:
June 21, 2016
Revised:
June 22, 2016
Citation
Kulesza, Z., and Sawicki, J. T. (August 16, 2016). "Parametrically Induced Damping in a Cracked Rotor." ASME. J. Eng. Gas Turbines Power. January 2017; 139(1): 012505. https://doi.org/10.1115/1.4034197
Download citation file:
Get Email Alerts
Cited By
Shape Optimization of an Industrial Aeroengine Combustor to reduce Thermoacoustic Instability
J. Eng. Gas Turbines Power
Dynamic Response of A Pivot-Mounted Squeeze Film Damper: Measurements and Predictions
J. Eng. Gas Turbines Power
Review of The Impact Of Hydrogen-Containing Fuels On Gas Turbine Hot-Section Materials
J. Eng. Gas Turbines Power
Effects of Lattice Orientation Angle On Tpms-Based Transpiration Cooling
J. Eng. Gas Turbines Power
Related Articles
Transient Analysis of Gas-Expanded Lubrication and Rotordynamic Performance in a Centrifugal Compressor
J. Eng. Gas Turbines Power (April,2016)
Improving the Stability of Labyrinth Gas Seals
J. Eng. Gas Turbines Power (April,2001)
Dynamics of Slant Cracked Rotor for a Steam Turbine Generator System
J. Eng. Gas Turbines Power (June,2017)
Rotordynamic Energy Expressions for General Anisotropic Finite Element Systems
J. Eng. Gas Turbines Power (February,2018)
Related Proceedings Papers
Related Chapters
Fundamentals of Structural Dynamics
Flow Induced Vibration of Power and Process Plant Components: A Practical Workbook
Summary and Conclusions
Bearing Dynamic Coefficients in Rotordynamics: Computation Methods and Practical Applications
Unbalance
Fundamentals of Rotating Machinery Diagnostics