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    Segmentation Effects on Brush Seal Leakage and Rotordynamic Coefficients

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 003::page 32501
    Author:
    Pugachev, Alexander O.
    ,
    Gaszner, Manuel
    ,
    Georgakis, Christos
    ,
    Cooper, Paul
    DOI: 10.1115/1.4031386
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper studies the effect of brush seal segmentation on the seal performance characteristics. A brush–labyrinth sealing configuration arranged of one brush seal downstream and two labyrinth fins upstream is studied experimentally and theoretically. The studied brush seal is of welded design installed with zero cold radial clearance. The brush seal front and back rings as well as the bristle pack are segmented radially in a single plane using the electrical discharge machining (EDM) technique. The segmentation procedure results in loss of bristles at the site of the cuts altering the leakage flow structure in the seal and its performance characteristics. Two test rigs are used to obtain leakage, as well as rotordynamic stiffness and damping coefficients of the seal at different pressure ratios. The computational fluid dynamics (CFD)based model is used to predict the seal performance and to study in detail local changes in the flow field due to the segmentation. A backtoback comparison of the performance of nonsegmented and segmented brush seals as well as baseline labyrinth seal is provided. The obtained results demonstrate that the segmentation in general negatively affects the performance of the studied brush–labyrinth sealing configuration. However, the segmented brush seal shows increased direct damping coefficients.
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      Segmentation Effects on Brush Seal Leakage and Rotordynamic Coefficients

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/161035
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    contributor authorPugachev, Alexander O.
    contributor authorGaszner, Manuel
    contributor authorGeorgakis, Christos
    contributor authorCooper, Paul
    date accessioned2017-05-09T01:28:13Z
    date available2017-05-09T01:28:13Z
    date issued2016
    identifier issn1528-8919
    identifier othergtp_138_03_032501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161035
    description abstractThis paper studies the effect of brush seal segmentation on the seal performance characteristics. A brush–labyrinth sealing configuration arranged of one brush seal downstream and two labyrinth fins upstream is studied experimentally and theoretically. The studied brush seal is of welded design installed with zero cold radial clearance. The brush seal front and back rings as well as the bristle pack are segmented radially in a single plane using the electrical discharge machining (EDM) technique. The segmentation procedure results in loss of bristles at the site of the cuts altering the leakage flow structure in the seal and its performance characteristics. Two test rigs are used to obtain leakage, as well as rotordynamic stiffness and damping coefficients of the seal at different pressure ratios. The computational fluid dynamics (CFD)based model is used to predict the seal performance and to study in detail local changes in the flow field due to the segmentation. A backtoback comparison of the performance of nonsegmented and segmented brush seals as well as baseline labyrinth seal is provided. The obtained results demonstrate that the segmentation in general negatively affects the performance of the studied brush–labyrinth sealing configuration. However, the segmented brush seal shows increased direct damping coefficients.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSegmentation Effects on Brush Seal Leakage and Rotordynamic Coefficients
    typeJournal Paper
    journal volume138
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4031386
    journal fristpage32501
    journal lastpage32501
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 003
    contenttypeFulltext
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