Test and Theory for Piezoelectric Actuator-Active Vibration Control of Rotating Machinery

[+] Author and Article Information
A. B. Palazzolo, R. R. Lin, R. M. Alexander

Department of Mechanical Engineering, Texas A&M University, College Station, Texas 77843-3123

A. F. Kascak, J. Montague

ARMY-NASA Lewis Research Center, MS 23/3, Cleveland, Ohio 44135 Sverdrup Technology Inc., Middleburg Heights, Ohio 44130

J. Vib. Acoust 113(2), 167-175 (Apr 01, 1991) (9 pages) doi:10.1115/1.2930165 History: Received August 01, 1989; Revised June 01, 1990; Online June 17, 2008


The application of piezoelectric actuators for active vibration control (AVC) of rotating machinery is examined. Theory is derived and the resulting predictions are shown to agree closely with results of tests performed on the air turbine driven-overhung rotor. The test results show significant reduction in unbalance, transient, and subsynchronous responses. Results from a 30 hour endurance test support the AVC system reliability. Various aspects of the electromechanical stability of the control system are also discussed and illustrated. Finally, application of the AVC system to an actual jet engine is discussed.

Copyright © 1991 by The American Society of Mechanical Engineers
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In