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    Nonlinear Analysis of Rotor-Bearing Systems Using Component Mode Synthesis

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003::page 606
    Author:
    H. D. Nelson
    ,
    W. L. Meacham
    ,
    D. P. Fleming
    ,
    A. F. Kascak
    DOI: 10.1115/1.3227460
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The method of component mode synthesis is developed to determine the forced response of nonlinear, multishaft, rotor-bearing systems. The formulation allows for simulation of system response due to blade loss, distributed unbalance, base shock, maneuver loads, and specified fixed frame forces. The motion of each rotating component of the system is described by superposing constraint modes associated with boundary coordinates and constrained precessional modes associated with internal coordinates. The precessional modes are truncated for each component and the reduced component equations are assembled with the nonlinear supports and interconnections to form a set of nonlinear system equations of reduced order. These equations are then numerically integrated to obtain the system response. A computer program, which is presently restricted to single shaft systems has been written and results are presented for transient system response associated with blade loss dynamics, with squeeze film dampers, and with interference rubs.
    keyword(s): Bearings , Rotors , Equations , Blades , Computer software , Dampers , Nonlinear systems , Dynamics (Mechanics) , Force , Motion , Simulation , Stress , Structural frames AND Shock (Mechanics) ,
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      Nonlinear Analysis of Rotor-Bearing Systems Using Component Mode Synthesis

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/97074
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorH. D. Nelson
    contributor authorW. L. Meacham
    contributor authorD. P. Fleming
    contributor authorA. F. Kascak
    date accessioned2017-05-08T23:15:28Z
    date available2017-05-08T23:15:28Z
    date copyrightJuly, 1983
    date issued1983
    identifier issn1528-8919
    identifier otherJETPEZ-26783#606_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97074
    description abstractThe method of component mode synthesis is developed to determine the forced response of nonlinear, multishaft, rotor-bearing systems. The formulation allows for simulation of system response due to blade loss, distributed unbalance, base shock, maneuver loads, and specified fixed frame forces. The motion of each rotating component of the system is described by superposing constraint modes associated with boundary coordinates and constrained precessional modes associated with internal coordinates. The precessional modes are truncated for each component and the reduced component equations are assembled with the nonlinear supports and interconnections to form a set of nonlinear system equations of reduced order. These equations are then numerically integrated to obtain the system response. A computer program, which is presently restricted to single shaft systems has been written and results are presented for transient system response associated with blade loss dynamics, with squeeze film dampers, and with interference rubs.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNonlinear Analysis of Rotor-Bearing Systems Using Component Mode Synthesis
    typeJournal Paper
    journal volume105
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227460
    journal fristpage606
    journal lastpage614
    identifier eissn0742-4795
    keywordsBearings
    keywordsRotors
    keywordsEquations
    keywordsBlades
    keywordsComputer software
    keywordsDampers
    keywordsNonlinear systems
    keywordsDynamics (Mechanics)
    keywordsForce
    keywordsMotion
    keywordsSimulation
    keywordsStress
    keywordsStructural frames AND Shock (Mechanics)
    treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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