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    Rim Seal Flow Analysis Through a Novel Technique in a Highly Instrumented Two Spool Rig

    Source: Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:005::page 7637
    Author:
    Mangini, Francesco
    ,
    Staggl, Marian
    ,
    Merli, Filippo
    ,
    Krajnc, Nicolas
    ,
    Hafizovic, Asim
    ,
    Krewinkel, Robert
    ,
    Marn, Andreas
    ,
    Göttlich, Emil
    DOI: 10.1115/1.4069849
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. This study introduces the first application of a sparsity-promoting linear regression technique to analyze the flow behavior within the rim seal region between the rotor and stator disks in a highly instrumented engine-representative turbine setup. This approach allows decomposing pressure fluctuations in the rim seal into multiple rotating structures, providing a more precise and detailed interpretation of data collected by flush-mounted, fast-response pressure transducers (Kulite XCQ-062). Many sources of periodic fluctuations, such as the HP rotor, the LP rotor, and the rotor–rotor interaction, characterize the flow in such a complex environment as a two-spool rig. Therefore, the decomposition provided by the linear regression algorithm is beneficial in identifying further periodic structures, such as nonblade passing-related cavity flow modes. The calculated angular speed of the identified structures is qualitatively validated by comparing it with the measured swirl ratio in the cavity at the same radial height. The research was conducted at the Institute of Thermal Turbomachinery at Graz University of Technology, specifically in the Transonic Test Turbine Facility (TTTF). The TTTF is a state-of-the-art facility that replicates engine-relevant flow conditions. It consists of the last high-pressure turbine stage, the turbine intermediate duct, and the first low-pressure turbine (LPT) rotor. Purge flows were supplied to all cavities to simulate engine-like conditions. The fast-response pressure transducers were installed in the downstream hub cavity (DHC), located between the high-pressure stage and the intermediate turbine duct. The measurements were performed across different purge flow rates (PFR) and different stator-clocking positions, producing a comprehensive dataset. The analysis uncovered low-intensity, nonblade passing-related flow modes within the cavity, which could not have been easily identified using other methodologies.
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      Rim Seal Flow Analysis Through a Novel Technique in a Highly Instrumented Two Spool Rig

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4316825
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    contributor authorMangini, Francesco
    contributor authorStaggl, Marian
    contributor authorMerli, Filippo
    contributor authorKrajnc, Nicolas
    contributor authorHafizovic, Asim
    contributor authorKrewinkel, Robert
    contributor authorMarn, Andreas
    contributor authorGöttlich, Emil
    date accessioned2026-08-23T08:37:34Z
    date available2026-08-23T08:37:34Z
    date copyright2026/05/01
    date issued2026
    identifier issn0742-4795
    identifier othergtp-25-1391.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316825
    description abstractAbstract. This study introduces the first application of a sparsity-promoting linear regression technique to analyze the flow behavior within the rim seal region between the rotor and stator disks in a highly instrumented engine-representative turbine setup. This approach allows decomposing pressure fluctuations in the rim seal into multiple rotating structures, providing a more precise and detailed interpretation of data collected by flush-mounted, fast-response pressure transducers (Kulite XCQ-062). Many sources of periodic fluctuations, such as the HP rotor, the LP rotor, and the rotor–rotor interaction, characterize the flow in such a complex environment as a two-spool rig. Therefore, the decomposition provided by the linear regression algorithm is beneficial in identifying further periodic structures, such as nonblade passing-related cavity flow modes. The calculated angular speed of the identified structures is qualitatively validated by comparing it with the measured swirl ratio in the cavity at the same radial height. The research was conducted at the Institute of Thermal Turbomachinery at Graz University of Technology, specifically in the Transonic Test Turbine Facility (TTTF). The TTTF is a state-of-the-art facility that replicates engine-relevant flow conditions. It consists of the last high-pressure turbine stage, the turbine intermediate duct, and the first low-pressure turbine (LPT) rotor. Purge flows were supplied to all cavities to simulate engine-like conditions. The fast-response pressure transducers were installed in the downstream hub cavity (DHC), located between the high-pressure stage and the intermediate turbine duct. The measurements were performed across different purge flow rates (PFR) and different stator-clocking positions, producing a comprehensive dataset. The analysis uncovered low-intensity, nonblade passing-related flow modes within the cavity, which could not have been easily identified using other methodologies.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRim Seal Flow Analysis Through a Novel Technique in a Highly Instrumented Two Spool Rig
    typeJournal Paper
    journal volume148
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4069849
    journal fristpage7637
    journal lastpage7657
    page21
    treeJournal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:005
    contenttypeFulltext
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