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    Transient Vibration of High-Speed, Lightweight Rotors Due to Sudden Imbalance

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003::page 480
    Author:
    M. Sakata
    ,
    H. Ohnabe
    ,
    T. Aiba
    DOI: 10.1115/1.3227440
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the field of rotor dynamics, increased attention is being given to the transient response analysis of the rotor, since the effects of impact loading and vibrations of the rotor arising from blade loss can be studied by a time transient solution of the rotor system. As recent trends in rotating machinery have been directed towards lightweight, high-speed flexible rotors, the effect of flexibility on transient response analysis is becoming of increasing importance. In the present paper, a transient vibration analysis is carried out on a flexible-disk/flexible-shaft system or rigid-disk flexible-shaft system subjected to a sudden imbalance that is assumed to represent the effect of blade loss. To solve the basic equation governing a rotating flexible disk the Galerkin’s method is used, and the equation of motion of the rotor system is numerically solved by employing the Runge-Kutta-Gill’s method. Experiments were conducted on a model rotor having a blade loss simulator; the shaft vibrations were also measured. The validity of the anaytical results was demonstrated by comparison with the experimental results.
    keyword(s): Rotors , Vibration , Disks , Blades , Transients (Dynamics) , Equations of motion , Rotordynamics , Plasticity , Machinery , Equations AND Vibration analysis ,
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      Transient Vibration of High-Speed, Lightweight Rotors Due to Sudden Imbalance

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/97055
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. Sakata
    contributor authorH. Ohnabe
    contributor authorT. Aiba
    date accessioned2017-05-08T23:15:26Z
    date available2017-05-08T23:15:26Z
    date copyrightJuly, 1983
    date issued1983
    identifier issn1528-8919
    identifier otherJETPEZ-26783#480_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97055
    description abstractIn the field of rotor dynamics, increased attention is being given to the transient response analysis of the rotor, since the effects of impact loading and vibrations of the rotor arising from blade loss can be studied by a time transient solution of the rotor system. As recent trends in rotating machinery have been directed towards lightweight, high-speed flexible rotors, the effect of flexibility on transient response analysis is becoming of increasing importance. In the present paper, a transient vibration analysis is carried out on a flexible-disk/flexible-shaft system or rigid-disk flexible-shaft system subjected to a sudden imbalance that is assumed to represent the effect of blade loss. To solve the basic equation governing a rotating flexible disk the Galerkin’s method is used, and the equation of motion of the rotor system is numerically solved by employing the Runge-Kutta-Gill’s method. Experiments were conducted on a model rotor having a blade loss simulator; the shaft vibrations were also measured. The validity of the anaytical results was demonstrated by comparison with the experimental results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTransient Vibration of High-Speed, Lightweight Rotors Due to Sudden Imbalance
    typeJournal Paper
    journal volume105
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227440
    journal fristpage480
    journal lastpage486
    identifier eissn0742-4795
    keywordsRotors
    keywordsVibration
    keywordsDisks
    keywordsBlades
    keywordsTransients (Dynamics)
    keywordsEquations of motion
    keywordsRotordynamics
    keywordsPlasticity
    keywordsMachinery
    keywordsEquations AND Vibration analysis
    treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003
    contenttypeFulltext
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