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    Measured Comparison of Leakage and Rotordynamic Characteristics for a Slanted Tooth and a Straight Tooth Labyrinth Seal

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 001::page 12501
    Author:
    Mehta, Naitik J.
    ,
    Childs, Dara W.
    DOI: 10.1115/1.4025267
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measured results are presented to compare rotordynamic coefficients and leakage of a slantedtooth labyrinth seal and a straighttooth labyrinth seal. Both seals had identical pitch, depth, and number of teeth. The teeth inclination angle of the teeth on the slantedtooth labyrinth was 65 deg from the normal axis. Experiments were carried out at an inlet pressure of 70 bara (1015 psia), pressure ratios of 0.4, 0.5, and 0.6, rotor speeds of 10.2, 15.35, and 20.2 krpm, and a radial clearance of 0.2 mm (8 mils). One zero and two positive inlet preswirl ratios were used. The results show only minute difference in the rotordynamic coefficients between the two seals. The slantedtooth labyrinth seal consistently leaked approximately 10% less at all conditions. Predictions were made using a one control volume bulkflow model (1CVM) which was developed for a straighttooth labyrinth seal design. 1CVM underpredicted the rotordynamic coefficients and the leakage.
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      Measured Comparison of Leakage and Rotordynamic Characteristics for a Slanted Tooth and a Straight Tooth Labyrinth Seal

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    https://yetl.yabesh.ir/yetl1/handle/yetl/154619
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorMehta, Naitik J.
    contributor authorChilds, Dara W.
    date accessioned2017-05-09T01:07:18Z
    date available2017-05-09T01:07:18Z
    date issued2014
    identifier issn1528-8919
    identifier othergtp_136_01_012501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154619
    description abstractMeasured results are presented to compare rotordynamic coefficients and leakage of a slantedtooth labyrinth seal and a straighttooth labyrinth seal. Both seals had identical pitch, depth, and number of teeth. The teeth inclination angle of the teeth on the slantedtooth labyrinth was 65 deg from the normal axis. Experiments were carried out at an inlet pressure of 70 bara (1015 psia), pressure ratios of 0.4, 0.5, and 0.6, rotor speeds of 10.2, 15.35, and 20.2 krpm, and a radial clearance of 0.2 mm (8 mils). One zero and two positive inlet preswirl ratios were used. The results show only minute difference in the rotordynamic coefficients between the two seals. The slantedtooth labyrinth seal consistently leaked approximately 10% less at all conditions. Predictions were made using a one control volume bulkflow model (1CVM) which was developed for a straighttooth labyrinth seal design. 1CVM underpredicted the rotordynamic coefficients and the leakage.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMeasured Comparison of Leakage and Rotordynamic Characteristics for a Slanted Tooth and a Straight Tooth Labyrinth Seal
    typeJournal Paper
    journal volume136
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4025267
    journal fristpage12501
    journal lastpage12501
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 001
    contenttypeFulltext
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