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    Optimization of Intentional Mistuning Patterns for the Reduction of the Forced Response Effects of Unintentional Mistuning: Formulation and Assessment

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001::page 131
    Author:
    B.-K. Choi
    ,
    J. Lentz
    ,
    A. J. Rivas-Guerra
    ,
    M. P. Mignolet
    DOI: 10.1115/1.1498270
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The focus of the present investigation is on the use of intentional mistuning of bladed disks to reduce their sensitivity to unintentional random mistuning. The class of intentionally mistuned disks considered here is limited, for cost reasons, to arrangements of two types of blades (A and B, say). A two-step procedure is then described to optimize the arrangement of these blades around the disk to reduce the effects of unintentional mistuning. First, a pure optimization effort is undertaken to obtain the pattern(s) of the A and B blades that yields small/the smallest value of the largest amplitude of response to a given excitation in the absence of unintentional mistuning. Then, in the second step, a pattern screening technique based on a recently introduced measure of localization is used to determine which of the patterns does have a large/small sensitivity to random unintentional mistuning. In this manner, expensive Monte Carlo simulations can be eliminated. Examples of application involving both simple bladed disk models and a 17-blade industrial rotor clearly demonstrate the significant benefits of using this class of intentionally mistuned disks.
    keyword(s): Optimization , Disks , Blades AND Rotors ,
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      Optimization of Intentional Mistuning Patterns for the Reduction of the Forced Response Effects of Unintentional Mistuning: Formulation and Assessment

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/128422
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorB.-K. Choi
    contributor authorJ. Lentz
    contributor authorA. J. Rivas-Guerra
    contributor authorM. P. Mignolet
    date accessioned2017-05-09T00:10:17Z
    date available2017-05-09T00:10:17Z
    date copyrightJanuary, 2003
    date issued2003
    identifier issn1528-8919
    identifier otherJETPEZ-26819#131_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128422
    description abstractThe focus of the present investigation is on the use of intentional mistuning of bladed disks to reduce their sensitivity to unintentional random mistuning. The class of intentionally mistuned disks considered here is limited, for cost reasons, to arrangements of two types of blades (A and B, say). A two-step procedure is then described to optimize the arrangement of these blades around the disk to reduce the effects of unintentional mistuning. First, a pure optimization effort is undertaken to obtain the pattern(s) of the A and B blades that yields small/the smallest value of the largest amplitude of response to a given excitation in the absence of unintentional mistuning. Then, in the second step, a pattern screening technique based on a recently introduced measure of localization is used to determine which of the patterns does have a large/small sensitivity to random unintentional mistuning. In this manner, expensive Monte Carlo simulations can be eliminated. Examples of application involving both simple bladed disk models and a 17-blade industrial rotor clearly demonstrate the significant benefits of using this class of intentionally mistuned disks.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptimization of Intentional Mistuning Patterns for the Reduction of the Forced Response Effects of Unintentional Mistuning: Formulation and Assessment
    typeJournal Paper
    journal volume125
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1498270
    journal fristpage131
    journal lastpage140
    identifier eissn0742-4795
    keywordsOptimization
    keywordsDisks
    keywordsBlades AND Rotors
    treeJournal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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