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    Rotordynamic Performance of the Interlocking Labyrinth Seal With a Tilting Rotor

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 001::page 011012-1
    Author:
    Zhang, Wanfu
    ,
    Wang, Yingfei
    ,
    Gu, Qianlei
    ,
    Yin, Lu
    ,
    Yang, Jiangang
    DOI: 10.1115/1.4048909
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Numerical analysis model of an interlocking labyrinth seal (ILS) is established for studying the effect of tilting rotor on its rotordynamic characteristics. The dynamic characteristic identification method based on infinitesimal theory is applied to solve the dynamic force coefficient of the seal with arbitrary elliptical orbits and eccentric positions under field conditions. The paper investigated the dynamic characteristics of the interlocking labyrinth seal with various misalignment angles (θ = 0, 0.1 deg, 0.2 deg, 0.3 deg, 0.4 deg, 0.5 deg, 0.6 deg), different pressure ratios (Pin = 6.9 bar, PR = 0.5, 0.8), locations of misalignment center (Loc = 0, L/2, L). Results show that the tilting rotor could minimize the leakage flow rate of the ILS. When the misalignment angle θ = 0.6 deg, the mass flow rate can be reduced about 2.5%. The effect of each cavity in the ILS on the stability of the system is different. The cavity with the inlet close to the rotor and the outlet away from the rotor helps to improve the system stability due to its locally antirotational flow. The effective damping of the entire ILS increases as the misalignment angle increases. The system shows the best stability when the misalignment center is close to the seal inlet. The tilting rotor has a positive effect on the stability of the ILS only except for high whirling frequency (>100 Hz) under Loc = L.
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      Rotordynamic Performance of the Interlocking Labyrinth Seal With a Tilting Rotor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4277302
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorZhang, Wanfu
    contributor authorWang, Yingfei
    contributor authorGu, Qianlei
    contributor authorYin, Lu
    contributor authorYang, Jiangang
    date accessioned2022-02-05T22:17:59Z
    date available2022-02-05T22:17:59Z
    date copyright1/4/2021 12:00:00 AM
    date issued2021
    identifier issn0742-4795
    identifier othergtp_143_01_011012.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277302
    description abstractNumerical analysis model of an interlocking labyrinth seal (ILS) is established for studying the effect of tilting rotor on its rotordynamic characteristics. The dynamic characteristic identification method based on infinitesimal theory is applied to solve the dynamic force coefficient of the seal with arbitrary elliptical orbits and eccentric positions under field conditions. The paper investigated the dynamic characteristics of the interlocking labyrinth seal with various misalignment angles (θ = 0, 0.1 deg, 0.2 deg, 0.3 deg, 0.4 deg, 0.5 deg, 0.6 deg), different pressure ratios (Pin = 6.9 bar, PR = 0.5, 0.8), locations of misalignment center (Loc = 0, L/2, L). Results show that the tilting rotor could minimize the leakage flow rate of the ILS. When the misalignment angle θ = 0.6 deg, the mass flow rate can be reduced about 2.5%. The effect of each cavity in the ILS on the stability of the system is different. The cavity with the inlet close to the rotor and the outlet away from the rotor helps to improve the system stability due to its locally antirotational flow. The effective damping of the entire ILS increases as the misalignment angle increases. The system shows the best stability when the misalignment center is close to the seal inlet. The tilting rotor has a positive effect on the stability of the ILS only except for high whirling frequency (>100 Hz) under Loc = L.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRotordynamic Performance of the Interlocking Labyrinth Seal With a Tilting Rotor
    typeJournal Paper
    journal volume143
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4048909
    journal fristpage011012-1
    journal lastpage011012-14
    page14
    treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 001
    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
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