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    A Statistical Characterization of the Effects of Mistuning in Multistage Bladed Disks

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 001::page 12503
    Author:
    Kiran X. D’Souza
    ,
    Bogdan I. Epureanu
    DOI: 10.1115/1.4004153
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A great deal of research has been conducted on the effects of small random variations in structural properties, known as mistuning, in single stage bladed disks. Due to the inherent randomness of mistuning and the large dimensionality of the models of industrial bladed disks, a reduced order modeling approach is required to understand the effects of mistuning on a particular bladed disk design. Component mode mistuning (CMM) is an efficient compact reduced order modeling method that was developed to handle this challenge in single stage bladed disks. In general, there are multiple stages in bladed disk assemblies, and it has been demonstrated that for certain frequency ranges accurate modeling of the entire bladed disk assembly is required because multistage modes exist. In this work, a statistical characterization of structural mistuning in multistage bladed disks is carried out. The results were obtained using CMM combined with a multistage modeling approach previously developed. In addition to the statistical characterization, a new efficient classification method is detailed for characterizing the properties of a mode. Also, the effects of structural mistuning on the characterization of the mode is explored.
    keyword(s): Coordinate measuring machines , Modeling , Disks , Blades , Motion , Engines , Manufacturing AND Mechanical properties ,
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      A Statistical Characterization of the Effects of Mistuning in Multistage Bladed Disks

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    http://yetl.yabesh.ir/yetl1/handle/yetl/148949
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    contributor authorKiran X. D’Souza
    contributor authorBogdan I. Epureanu
    date accessioned2017-05-09T00:50:41Z
    date available2017-05-09T00:50:41Z
    date copyrightJanuary, 2012
    date issued2012
    identifier issn1528-8919
    identifier otherJETPEZ-27180#012503_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148949
    description abstractA great deal of research has been conducted on the effects of small random variations in structural properties, known as mistuning, in single stage bladed disks. Due to the inherent randomness of mistuning and the large dimensionality of the models of industrial bladed disks, a reduced order modeling approach is required to understand the effects of mistuning on a particular bladed disk design. Component mode mistuning (CMM) is an efficient compact reduced order modeling method that was developed to handle this challenge in single stage bladed disks. In general, there are multiple stages in bladed disk assemblies, and it has been demonstrated that for certain frequency ranges accurate modeling of the entire bladed disk assembly is required because multistage modes exist. In this work, a statistical characterization of structural mistuning in multistage bladed disks is carried out. The results were obtained using CMM combined with a multistage modeling approach previously developed. In addition to the statistical characterization, a new efficient classification method is detailed for characterizing the properties of a mode. Also, the effects of structural mistuning on the characterization of the mode is explored.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Statistical Characterization of the Effects of Mistuning in Multistage Bladed Disks
    typeJournal Paper
    journal volume134
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4004153
    journal fristpage12503
    identifier eissn0742-4795
    keywordsCoordinate measuring machines
    keywordsModeling
    keywordsDisks
    keywordsBlades
    keywordsMotion
    keywordsEngines
    keywordsManufacturing AND Mechanical properties
    treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 001
    contenttypeFulltext
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