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    Optimum Design of Squeeze Film Dampers Supporting Multiple-Mode Rotors

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 004::page 992
    Author:
    A. El-Shafei
    ,
    R. Y. K. Yakoub
    DOI: 10.1115/1.1479338
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper a study of the optimum design of squeeze film dampers for multimode rotors is presented. The optimum design program obtains the best possible damper parameters for a given rotor to satisfy the minimization requirements for the objective function. The objectives are to minimize the amplitude response of the rotor at the critical speed, minimize the force transmitted to the support at the operating speed, or maximize the power dissipated by the damper. A combination of these objectives can also be used, with weighting factors to weigh the importance of each of these objectives. These are the possible objectives for the design of squeeze film dampers for aircraft engine applications. The basis of the optimum design program is an extremely fast algorithm which is able to quickly calculate the unbalance response of a rotor, for circular centered orbits of the journal in the damper. A commercial routine is used for the optimization, and is based on a complex direct search technique. The variation of the optimum clearance, length, and retainer spring stiffness are plotted against various rotor parameters. Recommendations for the design of squeeze film dampers are made. Applications to an aircraft engine illustrate the power of the developed algorithm.
    keyword(s): Dampers , Design , Rotors , Clearances (Engineering) AND Force ,
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      Optimum Design of Squeeze Film Dampers Supporting Multiple-Mode Rotors

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/126718
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. El-Shafei
    contributor authorR. Y. K. Yakoub
    date accessioned2017-05-09T00:07:23Z
    date available2017-05-09T00:07:23Z
    date copyrightOctober, 2002
    date issued2002
    identifier issn1528-8919
    identifier otherJETPEZ-26816#992_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126718
    description abstractIn this paper a study of the optimum design of squeeze film dampers for multimode rotors is presented. The optimum design program obtains the best possible damper parameters for a given rotor to satisfy the minimization requirements for the objective function. The objectives are to minimize the amplitude response of the rotor at the critical speed, minimize the force transmitted to the support at the operating speed, or maximize the power dissipated by the damper. A combination of these objectives can also be used, with weighting factors to weigh the importance of each of these objectives. These are the possible objectives for the design of squeeze film dampers for aircraft engine applications. The basis of the optimum design program is an extremely fast algorithm which is able to quickly calculate the unbalance response of a rotor, for circular centered orbits of the journal in the damper. A commercial routine is used for the optimization, and is based on a complex direct search technique. The variation of the optimum clearance, length, and retainer spring stiffness are plotted against various rotor parameters. Recommendations for the design of squeeze film dampers are made. Applications to an aircraft engine illustrate the power of the developed algorithm.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptimum Design of Squeeze Film Dampers Supporting Multiple-Mode Rotors
    typeJournal Paper
    journal volume124
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1479338
    journal fristpage992
    journal lastpage1002
    identifier eissn0742-4795
    keywordsDampers
    keywordsDesign
    keywordsRotors
    keywordsClearances (Engineering) AND Force
    treeJournal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 004
    contenttypeFulltext
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