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    Investigations on the Discharge and Total Temperature Increase Characteristics of the Labyrinth Seals With Honeycomb and Smooth Lands

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 004::page 41009
    Author:
    Xin Yan
    ,
    Jun Li
    ,
    Liming Song
    ,
    Zhenping Feng
    DOI: 10.1115/1.3068320
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The viscous work generated by the rotating components of a seal not only represents a direct loss of power but also causes an increase in the total temperature of fluid (windage effect). In order to study the discharge and total temperature increase characteristics of the stepped labyrinth seals with smooth and honeycomb lands, 3D Reynolds-averaged Navier–Stokes solutions from CFX is used in this work. At first, the influences of the inlet preswirl, leakage flow rate, and rotational speed on the total temperature increase in the convergent and divergent stepped labyrinth seals with smooth and honeycomb lands are conducted. The obtained 3D numerical results are well in agreement with the referenced experimental data. It shows that the utilized numerical approach has sufficient precision to predict the total temperature increase in seals. Then, a range of pressure ratios and four sizes of sealing clearance are performed to investigate the effects of sealing clearances and pressure ratio impact on the discharge and total temperature increase of the stepped labyrinth seals with honeycomb and smooth liners.
    keyword(s): Pressure , Flow (Dynamics) , Temperature , Clearances (Engineering) , Heating , Sealing (Process) , Leakage flows AND Leakage ,
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      Investigations on the Discharge and Total Temperature Increase Characteristics of the Labyrinth Seals With Honeycomb and Smooth Lands

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/142139
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    • Journal of Turbomachinery

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    contributor authorXin Yan
    contributor authorJun Li
    contributor authorLiming Song
    contributor authorZhenping Feng
    date accessioned2017-05-09T00:35:45Z
    date available2017-05-09T00:35:45Z
    date copyrightOctober, 2009
    date issued2009
    identifier issn0889-504X
    identifier otherJOTUEI-28758#041009_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142139
    description abstractThe viscous work generated by the rotating components of a seal not only represents a direct loss of power but also causes an increase in the total temperature of fluid (windage effect). In order to study the discharge and total temperature increase characteristics of the stepped labyrinth seals with smooth and honeycomb lands, 3D Reynolds-averaged Navier–Stokes solutions from CFX is used in this work. At first, the influences of the inlet preswirl, leakage flow rate, and rotational speed on the total temperature increase in the convergent and divergent stepped labyrinth seals with smooth and honeycomb lands are conducted. The obtained 3D numerical results are well in agreement with the referenced experimental data. It shows that the utilized numerical approach has sufficient precision to predict the total temperature increase in seals. Then, a range of pressure ratios and four sizes of sealing clearance are performed to investigate the effects of sealing clearances and pressure ratio impact on the discharge and total temperature increase of the stepped labyrinth seals with honeycomb and smooth liners.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigations on the Discharge and Total Temperature Increase Characteristics of the Labyrinth Seals With Honeycomb and Smooth Lands
    typeJournal Paper
    journal volume131
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3068320
    journal fristpage41009
    identifier eissn1528-8900
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsClearances (Engineering)
    keywordsHeating
    keywordsSealing (Process)
    keywordsLeakage flows AND Leakage
    treeJournal of Turbomachinery:;2009:;volume( 131 ):;issue: 004
    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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