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contributor authorA. B. Palazzolo
contributor authorA. F. Kascak
contributor authorJ. Montague
contributor authorR. R. Lin
contributor authorR. M. Alexander
date accessioned2017-05-08T23:37:11Z
date available2017-05-08T23:37:11Z
date copyrightApril, 1991
date issued1991
identifier issn1048-9002
identifier otherJVACEK-28797#167_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109509
description abstractThe 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleTest and Theory for Piezoelectric Actuator-Active Vibration Control of Rotating Machinery
typeJournal Paper
journal volume113
journal issue2
journal titleJournal of Vibration and Acoustics
identifier doi10.1115/1.2930165
journal fristpage167
journal lastpage175
identifier eissn1528-8927
keywordsVibration control
keywordsActuators
keywordsMachinery
keywordsControl systems
keywordsReliability
keywordsStability
keywordsRotors
keywordsTurbines
keywordsJet engines AND Piezoelectric actuators
treeJournal of Vibration and Acoustics:;1991:;volume( 113 ):;issue: 002
contenttypeFulltext


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