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    Effects of Impeller Squealer Tip on Centrifugal Compressor Performance

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 003::page 32603
    Author:
    Da Soghe, Riccardo
    ,
    Bianchini, Cosimo
    ,
    Tommaso Rubino, Dante
    ,
    Toni, Lorenzo
    DOI: 10.1115/1.4034541
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper summarizes the main results sorted out from a design of experiment (DoE) based on a validated computational fluid dynamics (CFD). Several tip recessed geometries applied to an unshrouded impeller were considered in conjunction with two tip clearance levels. The computations show that recessed tip geometries have positive effects when considering high-flow coefficient values, while in part-load conditions the gain is reduced. Starting from the results obtained when studying tip cavities, a single rim tip squealer geometry was then analyzed: the proposed geometry leads to performance improvements for all the tested conditions considered in this work.
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      Effects of Impeller Squealer Tip on Centrifugal Compressor Performance

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4233646
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    contributor authorDa Soghe, Riccardo
    contributor authorBianchini, Cosimo
    contributor authorTommaso Rubino, Dante
    contributor authorToni, Lorenzo
    date accessioned2017-11-25T07:15:44Z
    date available2017-11-25T07:15:44Z
    date copyright2016/11/10
    date issued2017
    identifier issn0742-4795
    identifier othergtp_139_03_032603.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4233646
    description abstractThis paper summarizes the main results sorted out from a design of experiment (DoE) based on a validated computational fluid dynamics (CFD). Several tip recessed geometries applied to an unshrouded impeller were considered in conjunction with two tip clearance levels. The computations show that recessed tip geometries have positive effects when considering high-flow coefficient values, while in part-load conditions the gain is reduced. Starting from the results obtained when studying tip cavities, a single rim tip squealer geometry was then analyzed: the proposed geometry leads to performance improvements for all the tested conditions considered in this work.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffects of Impeller Squealer Tip on Centrifugal Compressor Performance
    typeJournal Paper
    journal volume139
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4034541
    journal fristpage32603
    journal lastpage032603-7
    treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 003
    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
    yabeshDSpacePersian