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    Aerodynamic Performance of Turbine Center Frames With Purge Flows—Part II: The Influence of Individual Hub and Tip Purge Flows

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 006::page 61010
    Author:
    Zerobin, Stefan
    ,
    Aldrian, Christian
    ,
    Peters, Andreas
    ,
    Heitmeir, Franz
    ,
    Göttlich, Emil
    DOI: 10.1115/1.4039363
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerodynamic behavior of turbine center frame (TCF) ducts under the presence of high-pressure turbine (HPT) purge flows was experimentally investigated in this two-part paper. While the first part of the paper demonstrated the impact of varying the purge flow rates (PFR) on the loss behavior of two different TCF designs, the second part concentrates on the influence of individual hub and tip purge flows on the main flow evolution and loss generation mechanisms through the TCF ducts. Therefore, measurements were conducted at six different operating conditions in a one and a half stage turbine test setup, featuring four individual purge flows injected through the hub and tip, forward and aft cavities of the HPT rotor. The outcomes of this first-time assessment indicate that a HPT purge flow reduction generally benefits TCF performance. Decreasing one of the rotor case PFRs leads to an improved duct pressure loss. The purge flows from the rotor aft hub and tip cavities are demonstrated to play a particularly important role for improving the duct aerodynamic behavior. In contrast, the forward rotor hub purge flow actually stabilizes the flow in the TCF duct and reducing this purge flow can penalize TCF performance. These particular HPT/TCF interactions should be taken into account whenever high-pressure turbine purge flow reductions are pursued.
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      Aerodynamic Performance of Turbine Center Frames With Purge Flows—Part II: The Influence of Individual Hub and Tip Purge Flows

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    contributor authorZerobin, Stefan
    contributor authorAldrian, Christian
    contributor authorPeters, Andreas
    contributor authorHeitmeir, Franz
    contributor authorGöttlich, Emil
    date accessioned2019-02-28T11:10:02Z
    date available2019-02-28T11:10:02Z
    date copyright5/3/2018 12:00:00 AM
    date issued2018
    identifier issn0889-504X
    identifier otherturbo_140_06_061010.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4253385
    description abstractThe aerodynamic behavior of turbine center frame (TCF) ducts under the presence of high-pressure turbine (HPT) purge flows was experimentally investigated in this two-part paper. While the first part of the paper demonstrated the impact of varying the purge flow rates (PFR) on the loss behavior of two different TCF designs, the second part concentrates on the influence of individual hub and tip purge flows on the main flow evolution and loss generation mechanisms through the TCF ducts. Therefore, measurements were conducted at six different operating conditions in a one and a half stage turbine test setup, featuring four individual purge flows injected through the hub and tip, forward and aft cavities of the HPT rotor. The outcomes of this first-time assessment indicate that a HPT purge flow reduction generally benefits TCF performance. Decreasing one of the rotor case PFRs leads to an improved duct pressure loss. The purge flows from the rotor aft hub and tip cavities are demonstrated to play a particularly important role for improving the duct aerodynamic behavior. In contrast, the forward rotor hub purge flow actually stabilizes the flow in the TCF duct and reducing this purge flow can penalize TCF performance. These particular HPT/TCF interactions should be taken into account whenever high-pressure turbine purge flow reductions are pursued.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAerodynamic Performance of Turbine Center Frames With Purge Flows—Part II: The Influence of Individual Hub and Tip Purge Flows
    typeJournal Paper
    journal volume140
    journal issue6
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4039363
    journal fristpage61010
    journal lastpage061010-8
    treeJournal of Turbomachinery:;2018:;volume 140:;issue 006
    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