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    Impact Excitation Tests to Determine the Influence Coefficients for Balancing Lightly Damped Rotors

    Source: Journal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 004::page 600
    Author:
    J. Tonnesen
    ,
    J. W. Lund
    DOI: 10.1115/1.3240177
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments have been conducted to evaluate a supplementary method for balancing lightly damped rotors. The rotor, while running, is excited by an impact generator, and the response is measured at the bearings by transducers for displacement, force, and acceleration. An FFT analyzer is employed to obtain the frequency-dependent transfer functions from which the corresponding influence coefficients can be calculated. The results are compared with the values obtained from the conventional trial weight method, and they are also used in a successful balancing of the rotor.
    keyword(s): Rotors , Transducers , Displacement , Generators , Weight (Mass) , Force , Transfer functions AND Bearings ,
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      Impact Excitation Tests to Determine the Influence Coefficients for Balancing Lightly Damped Rotors

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/103820
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. Tonnesen
    contributor authorJ. W. Lund
    date accessioned2017-05-08T23:27:03Z
    date available2017-05-08T23:27:03Z
    date copyrightOctober, 1988
    date issued1988
    identifier issn1528-8919
    identifier otherJETPEZ-26660#600_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103820
    description abstractExperiments have been conducted to evaluate a supplementary method for balancing lightly damped rotors. The rotor, while running, is excited by an impact generator, and the response is measured at the bearings by transducers for displacement, force, and acceleration. An FFT analyzer is employed to obtain the frequency-dependent transfer functions from which the corresponding influence coefficients can be calculated. The results are compared with the values obtained from the conventional trial weight method, and they are also used in a successful balancing of the rotor.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleImpact Excitation Tests to Determine the Influence Coefficients for Balancing Lightly Damped Rotors
    typeJournal Paper
    journal volume110
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3240177
    journal fristpage600
    journal lastpage604
    identifier eissn0742-4795
    keywordsRotors
    keywordsTransducers
    keywordsDisplacement
    keywordsGenerators
    keywordsWeight (Mass)
    keywordsForce
    keywordsTransfer functions AND Bearings
    treeJournal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 004
    contenttypeFulltext
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