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    Modeling and Simulation Methods for MDOF Structures and Rotating Machinery With Impact Dampers

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 002::page 436
    Author:
    J. M. McElhaney
    ,
    A. Kascak
    ,
    A. Palazzolo
    DOI: 10.1115/1.2815594
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Previously published work on applied impact damping typically relates to SDOF models or simple MDOF models such as the classical cantilever beam. Structural models often require an extremely large number of DOF with mode shapes that are generally very complex. Dynamics simulation of these typically becomes both complicated and time consuming. The nonlinear behavior of impact dampers further complicates such simulation in that standard linear solutions are not possible. The primary objective in this research extends previous work by applying impact dampers to MDOF structures that are modeled with general three-dimensional “beam” finite elements. Modal-based models of the MDOF systems and efficient impact damper tracking algorithms were also developed that significantly reduced CPU time for simulation. Significant among the objectives was obtaining an impact damper design for the MDOF casing structure of the Space Shuttle Main Engine (SSME), High-Pressure Oxygen Turbo-Pump (HPOTP), subject to pump rotor shaft unbalance. Impact damper performance is based on suppression of vibration at casing critical frequencies for rotor speed ranges, at rotor full speed, and very high unbalance to simulate a defect such as losing an impeller blade fragment or a cracked bearing [6]. Simulations show significant reductions in vibration at the casing critical frequencies and very high unbalance levels while little or no improvement was observed off resonance. Additionally, the previous work with an experimental rotor bearing system (RBS) and impact damper was modeled using the developed modal-based methods. Simulation of the resulting model response shows remarkable agreement with the experimental. Finally, both the RBS and the HPOTP were modeled and simulated as unstable systems with attached impact dampers. The simulations predict that the impact damper is an excellent stabilizing mechanism for a range of instability driver values. Simulation of the models in this research with the developed modal based algorithms were accomplished with excellent efficiency, and accurate results.
    keyword(s): Machinery , Simulation , Dampers , Modeling , Rotors , Vibration , Pumps , Engineering simulation , Algorithms , Bearings , Frequency , Oxygen , Shapes , Mechanisms , Impellers , High pressure (Physics) , Cantilever beams , Engines , Resonance , Dynamics (Mechanics) , Finite element analysis , Damping , Design AND Blades ,
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      Modeling and Simulation Methods for MDOF Structures and Rotating Machinery With Impact Dampers

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    http://yetl.yabesh.ir/yetl1/handle/yetl/118703
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. M. McElhaney
    contributor authorA. Kascak
    contributor authorA. Palazzolo
    date accessioned2017-05-08T23:53:29Z
    date available2017-05-08T23:53:29Z
    date copyrightApril, 1997
    date issued1997
    identifier issn1528-8919
    identifier otherJETPEZ-26764#436_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118703
    description abstractPreviously published work on applied impact damping typically relates to SDOF models or simple MDOF models such as the classical cantilever beam. Structural models often require an extremely large number of DOF with mode shapes that are generally very complex. Dynamics simulation of these typically becomes both complicated and time consuming. The nonlinear behavior of impact dampers further complicates such simulation in that standard linear solutions are not possible. The primary objective in this research extends previous work by applying impact dampers to MDOF structures that are modeled with general three-dimensional “beam” finite elements. Modal-based models of the MDOF systems and efficient impact damper tracking algorithms were also developed that significantly reduced CPU time for simulation. Significant among the objectives was obtaining an impact damper design for the MDOF casing structure of the Space Shuttle Main Engine (SSME), High-Pressure Oxygen Turbo-Pump (HPOTP), subject to pump rotor shaft unbalance. Impact damper performance is based on suppression of vibration at casing critical frequencies for rotor speed ranges, at rotor full speed, and very high unbalance to simulate a defect such as losing an impeller blade fragment or a cracked bearing [6]. Simulations show significant reductions in vibration at the casing critical frequencies and very high unbalance levels while little or no improvement was observed off resonance. Additionally, the previous work with an experimental rotor bearing system (RBS) and impact damper was modeled using the developed modal-based methods. Simulation of the resulting model response shows remarkable agreement with the experimental. Finally, both the RBS and the HPOTP were modeled and simulated as unstable systems with attached impact dampers. The simulations predict that the impact damper is an excellent stabilizing mechanism for a range of instability driver values. Simulation of the models in this research with the developed modal based algorithms were accomplished with excellent efficiency, and accurate results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleModeling and Simulation Methods for MDOF Structures and Rotating Machinery With Impact Dampers
    typeJournal Paper
    journal volume119
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2815594
    journal fristpage436
    journal lastpage446
    identifier eissn0742-4795
    keywordsMachinery
    keywordsSimulation
    keywordsDampers
    keywordsModeling
    keywordsRotors
    keywordsVibration
    keywordsPumps
    keywordsEngineering simulation
    keywordsAlgorithms
    keywordsBearings
    keywordsFrequency
    keywordsOxygen
    keywordsShapes
    keywordsMechanisms
    keywordsImpellers
    keywordsHigh pressure (Physics)
    keywordsCantilever beams
    keywordsEngines
    keywordsResonance
    keywordsDynamics (Mechanics)
    keywordsFinite element analysis
    keywordsDamping
    keywordsDesign AND Blades
    treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 002
    contenttypeFulltext
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