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    The Influence of a Variable Normal Load on the Forced Vibration of a Frictionally Damped Structure

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002::page 300
    Author:
    C.-H. Menq
    ,
    J. H. Griffin
    ,
    J. Bielak
    DOI: 10.1115/1.3239903
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An approximate procedure is developed for calculating the steady-state response of frictionally damped structures for which the normal load across the friction interface consists of a constant force and a force that varies linearly with the vibratory displacement. Such situations occur quite frequently in practice, as, for example; in the case of shrouded fan blades or in certain types of turbine-blade friction dampers. Depending on the magnitudes of the constant and the variable normal loads, the friction element will either stick, slip, or lift off at various intervals during a cycle of oscillation. The various possibilities are considered in the present study. Results from the approximate method are compared with “long-time” solutions obtained from a conventional transient analysis of the problem in order to assess the accuracy of the proposed procedure. As an application, the new method is then used to study the influence of the dynamic coupling on the optimization of the friction force in turbine blade dampers. Results show that the optimum friction force and the maximum amplitude of the response increase with dynamic coupling.
    keyword(s): Stress , Vibration , Friction , Force , Turbine blades , Dampers , Optimization , Blades , Cycles , Displacement , Steady state , Transient analysis AND Oscillations ,
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      The Influence of a Variable Normal Load on the Forced Vibration of a Frictionally Damped Structure

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/101126
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorC.-H. Menq
    contributor authorJ. H. Griffin
    contributor authorJ. Bielak
    date accessioned2017-05-08T23:22:27Z
    date available2017-05-08T23:22:27Z
    date copyrightApril, 1986
    date issued1986
    identifier issn1528-8919
    identifier otherJETPEZ-26634#300_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101126
    description abstractAn approximate procedure is developed for calculating the steady-state response of frictionally damped structures for which the normal load across the friction interface consists of a constant force and a force that varies linearly with the vibratory displacement. Such situations occur quite frequently in practice, as, for example; in the case of shrouded fan blades or in certain types of turbine-blade friction dampers. Depending on the magnitudes of the constant and the variable normal loads, the friction element will either stick, slip, or lift off at various intervals during a cycle of oscillation. The various possibilities are considered in the present study. Results from the approximate method are compared with “long-time” solutions obtained from a conventional transient analysis of the problem in order to assess the accuracy of the proposed procedure. As an application, the new method is then used to study the influence of the dynamic coupling on the optimization of the friction force in turbine blade dampers. Results show that the optimum friction force and the maximum amplitude of the response increase with dynamic coupling.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Influence of a Variable Normal Load on the Forced Vibration of a Frictionally Damped Structure
    typeJournal Paper
    journal volume108
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239903
    journal fristpage300
    journal lastpage305
    identifier eissn0742-4795
    keywordsStress
    keywordsVibration
    keywordsFriction
    keywordsForce
    keywordsTurbine blades
    keywordsDampers
    keywordsOptimization
    keywordsBlades
    keywordsCycles
    keywordsDisplacement
    keywordsSteady state
    keywordsTransient analysis AND Oscillations
    treeJournal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002
    contenttypeFulltext
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