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    Unsteady Flow Interactions Between a High- and Low-Pressure Turbine

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 010::page 0101012-1
    Author:
    Sterzinger, P. Z.
    ,
    Zerobin, S.
    ,
    Merli, F.
    ,
    Wiesinger, L.
    ,
    Dellacasagrande, M.
    ,
    Peters, A.
    ,
    Maini, G.
    ,
    Heitmeir, F.
    ,
    Göttlich, E.
    DOI: 10.1115/1.4046453
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the unsteady flow interactions between an engine-representative high-pressure turbine (HPT) and low-pressure turbine (LPT) stage, connected by a turbine center frame (TCF) duct with nonturning struts. The setup was tested at the high-speed two-spool test turbine facility at the Institute for Thermal Turbomachinery and Machine Dynamics at Graz University of Technology and includes relevant purge and turbine rotor tip leakage flows. Due to the complexity of such a test, the unsteady component interactions in an HPT–TCF–LPT module have not received much attention in the past and require additional analysis to determine new approaches for further performance improvements on the system level. The flow downstream of an HPT is highly unsteady and dominated by stator–rotor interactions, which affect the flow behavior through the downstream TCF and LPT. To capture the unsteady flow structures, time-resolved aerodynamic measurements were carried out with a fast-response aerodynamic pressure probe (FRAPP) at three different measurement planes. In this paper, the time-resolved and phase-averaged flow fields with respect to the HPT and LPT trigger are studied. Since the two rotors are uncorrelated, the applied method allows the identification of the flow structures induced by either of them. Upstream of the LPT stage, the HPT flow structures evolving through the TCF duct dominate the flow fields. Downstream of the LPT stage, the flow is affected by both the HPT and the LPT secondary flow structures. The interactions between the various stator rows and the two rotors are detected by means of time-space plots and modal decomposition. To describe the fluctuations induced by both rotors, particularly the rotor–rotor interaction, the rotor synchronic averaging (RSA) is used to analyze the flow field downstream of the LPT. This paper highlights the need to account for the HPT-induced unsteady mechanisms in addition to the LPT flow structures and the interaction of both to arrive at improved LPT designs.
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      Unsteady Flow Interactions Between a High- and Low-Pressure Turbine

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    contributor authorSterzinger, P. Z.
    contributor authorZerobin, S.
    contributor authorMerli, F.
    contributor authorWiesinger, L.
    contributor authorDellacasagrande, M.
    contributor authorPeters, A.
    contributor authorMaini, G.
    contributor authorHeitmeir, F.
    contributor authorGöttlich, E.
    date accessioned2022-02-04T22:21:23Z
    date available2022-02-04T22:21:23Z
    date copyright9/18/2020 12:00:00 AM
    date issued2020
    identifier issn0889-504X
    identifier otherturbo_142_10_101012.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4275403
    description abstractThis paper presents the unsteady flow interactions between an engine-representative high-pressure turbine (HPT) and low-pressure turbine (LPT) stage, connected by a turbine center frame (TCF) duct with nonturning struts. The setup was tested at the high-speed two-spool test turbine facility at the Institute for Thermal Turbomachinery and Machine Dynamics at Graz University of Technology and includes relevant purge and turbine rotor tip leakage flows. Due to the complexity of such a test, the unsteady component interactions in an HPT–TCF–LPT module have not received much attention in the past and require additional analysis to determine new approaches for further performance improvements on the system level. The flow downstream of an HPT is highly unsteady and dominated by stator–rotor interactions, which affect the flow behavior through the downstream TCF and LPT. To capture the unsteady flow structures, time-resolved aerodynamic measurements were carried out with a fast-response aerodynamic pressure probe (FRAPP) at three different measurement planes. In this paper, the time-resolved and phase-averaged flow fields with respect to the HPT and LPT trigger are studied. Since the two rotors are uncorrelated, the applied method allows the identification of the flow structures induced by either of them. Upstream of the LPT stage, the HPT flow structures evolving through the TCF duct dominate the flow fields. Downstream of the LPT stage, the flow is affected by both the HPT and the LPT secondary flow structures. The interactions between the various stator rows and the two rotors are detected by means of time-space plots and modal decomposition. To describe the fluctuations induced by both rotors, particularly the rotor–rotor interaction, the rotor synchronic averaging (RSA) is used to analyze the flow field downstream of the LPT. This paper highlights the need to account for the HPT-induced unsteady mechanisms in addition to the LPT flow structures and the interaction of both to arrive at improved LPT designs.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleUnsteady Flow Interactions Between a High- and Low-Pressure Turbine
    typeJournal Paper
    journal volume142
    journal issue10
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4046453
    journal fristpage0101012-1
    journal lastpage0101012-10
    page10
    treeJournal of Turbomachinery:;2020:;volume( 142 ):;issue: 010
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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