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    A Magnetic Damper for First-Mode Vibration Reduction in Multimass Flexible Rotors

    Source: Journal of Engineering for Gas Turbines and Power:;1990:;volume( 112 ):;issue: 004::page 463
    Author:
    M. E. F. Kasarda
    ,
    P. E. Allaire
    ,
    R. R. Humphris
    ,
    L. E. Barrett
    DOI: 10.1115/1.2906190
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Many rotating machines such as compressors, turbines, and pumps have long thin shafts with resulting vibration problems. They would benefit from additional damping near the center of the shaft. Magnetic dampers have the potential to be employed in these machines because they can operate in the working fluid environment, unlike conventional bearings. This paper describes an experimental test rig that was set up with a long thin shaft and several masses to represent a flexible shaft machine. An active magnetic damper was placed in three locations: near the midspan, near one end disk, and close to the bearing. With typical control parameter settings, the midspan location reduced the first mode vibration 82 percent, the disk location reduced it 75 percent, and the bearing location attained a 74 percent reduction. Magnetic damper stiffness and damping values used to obtain these reductions were only a few percent of the bearing stiffness and damping values. A theoretical model of both the rotor and the damper was developed and compared to the measured results. The agreement was good.
    keyword(s): Dampers , Rotors , Vibration , Bearings , Machinery , Damping , Disks , Stiffness , Pumps , Turbines , Compressors AND Fluids ,
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      A Magnetic Damper for First-Mode Vibration Reduction in Multimass Flexible Rotors

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/106862
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. E. F. Kasarda
    contributor authorP. E. Allaire
    contributor authorR. R. Humphris
    contributor authorL. E. Barrett
    date accessioned2017-05-08T23:32:32Z
    date available2017-05-08T23:32:32Z
    date copyrightOctober, 1990
    date issued1990
    identifier issn1528-8919
    identifier otherJETPEZ-26679#463_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106862
    description abstractMany rotating machines such as compressors, turbines, and pumps have long thin shafts with resulting vibration problems. They would benefit from additional damping near the center of the shaft. Magnetic dampers have the potential to be employed in these machines because they can operate in the working fluid environment, unlike conventional bearings. This paper describes an experimental test rig that was set up with a long thin shaft and several masses to represent a flexible shaft machine. An active magnetic damper was placed in three locations: near the midspan, near one end disk, and close to the bearing. With typical control parameter settings, the midspan location reduced the first mode vibration 82 percent, the disk location reduced it 75 percent, and the bearing location attained a 74 percent reduction. Magnetic damper stiffness and damping values used to obtain these reductions were only a few percent of the bearing stiffness and damping values. A theoretical model of both the rotor and the damper was developed and compared to the measured results. The agreement was good.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Magnetic Damper for First-Mode Vibration Reduction in Multimass Flexible Rotors
    typeJournal Paper
    journal volume112
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906190
    journal fristpage463
    journal lastpage469
    identifier eissn0742-4795
    keywordsDampers
    keywordsRotors
    keywordsVibration
    keywordsBearings
    keywordsMachinery
    keywordsDamping
    keywordsDisks
    keywordsStiffness
    keywordsPumps
    keywordsTurbines
    keywordsCompressors AND Fluids
    treeJournal of Engineering for Gas Turbines and Power:;1990:;volume( 112 ):;issue: 004
    contenttypeFulltext
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