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

    Source: Journal of Vibration and Acoustics:;1991:;volume( 113 ):;issue: 002::page 167
    Author:
    A. B. Palazzolo
    ,
    A. F. Kascak
    ,
    J. Montague
    ,
    R. R. Lin
    ,
    R. M. Alexander
    DOI: 10.1115/1.2930165
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: 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.
    keyword(s): Vibration control , Actuators , Machinery , Control systems , Reliability , Stability , Rotors , Turbines , Jet engines AND Piezoelectric actuators ,
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      Test and Theory for Piezoelectric Actuator-Active Vibration Control of Rotating Machinery

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109509
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    • Journal of Vibration and Acoustics

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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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