YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Engineering for Gas Turbines and Power
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Impact of Mistuned Underplatform Dampers on the Nonlinear Vibration of Bladed Disks

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 012::page 0121023-1
    Author:
    Quaegebeur, Samuel
    ,
    Chouvion, Benjamin
    ,
    Thouverez, Fabrice
    DOI: 10.1115/1.4051868
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Before the final experimental validation and certification of a turbo-engine, designers perform a numerical simulation of its vibratory properties, among other things, in order to estimate its lifespan and adjust the design in an optimization process. One possible practical solution to decrease the vibratory response is to add underplatform dampers to the system. These components dissipate energy by friction and are widely employed in turbomachinery. However, a specific underplatform damper is usually efficient only for a specific mode. The purpose of this work is to investigate the possibility of adding different kinds of underplatform dampers to the cyclic structure in order to decrease the vibratory energy over a larger panel of modes. Different methods exist to determine the vibrations of nonlinear cyclic symmetric systems, but creating a robust methodology to account for the additional effect of mistuning remains a big challenge in the community. In this paper, the structure is mistuned through the friction coefficient of the dampers and not by altering its geometry, as is usually done in the literature. First, assuming a cyclic symmetric structure, the performance of the dampers is assessed for specific modes. Then, employing a method recently developed, the efficiency of an intentional mistuning pattern of underplatform dampers is studied and an optimal pattern proposed.
    • Download: (1.579Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Impact of Mistuned Underplatform Dampers on the Nonlinear Vibration of Bladed Disks

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4278260
    Collections
    • Journal of Engineering for Gas Turbines and Power

    Show full item record

    contributor authorQuaegebeur, Samuel
    contributor authorChouvion, Benjamin
    contributor authorThouverez, Fabrice
    date accessioned2022-02-06T05:33:00Z
    date available2022-02-06T05:33:00Z
    date copyright10/13/2021 12:00:00 AM
    date issued2021
    identifier issn0742-4795
    identifier othergtp_143_12_121023.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4278260
    description abstractBefore the final experimental validation and certification of a turbo-engine, designers perform a numerical simulation of its vibratory properties, among other things, in order to estimate its lifespan and adjust the design in an optimization process. One possible practical solution to decrease the vibratory response is to add underplatform dampers to the system. These components dissipate energy by friction and are widely employed in turbomachinery. However, a specific underplatform damper is usually efficient only for a specific mode. The purpose of this work is to investigate the possibility of adding different kinds of underplatform dampers to the cyclic structure in order to decrease the vibratory energy over a larger panel of modes. Different methods exist to determine the vibrations of nonlinear cyclic symmetric systems, but creating a robust methodology to account for the additional effect of mistuning remains a big challenge in the community. In this paper, the structure is mistuned through the friction coefficient of the dampers and not by altering its geometry, as is usually done in the literature. First, assuming a cyclic symmetric structure, the performance of the dampers is assessed for specific modes. Then, employing a method recently developed, the efficiency of an intentional mistuning pattern of underplatform dampers is studied and an optimal pattern proposed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleImpact of Mistuned Underplatform Dampers on the Nonlinear Vibration of Bladed Disks
    typeJournal Paper
    journal volume143
    journal issue12
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4051868
    journal fristpage0121023-1
    journal lastpage0121023-8
    page8
    treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 012
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian