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    Development of Scallop Cut Type Damper Seal for Centrifugal Compressors

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 003::page 32509
    Author:
    Takahashi, Naohiko
    ,
    Miura, Haruo
    ,
    Narita, Mitsuhiro
    ,
    Nishijima, Noriyo
    ,
    Magara, Yohei
    DOI: 10.1115/1.4028448
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper deals with a new type of damper seal developed for a highpressure centrifugal compressor. Honeycomb seals and hole pattern seals are popularly used as damper seals and provide superior rotordynamic damping characteristics. Honeycomb seals are expensive because the manufacturing process is complex. Hole pattern seals are easier to manufacture, but they are still expensive. Use of a scallop pattern is one way to reduce manufacturing cost and time. A new seal that has a scallop pattern and small teeth on the stator surface is proposed. This pattern is cut on the stator surface using a disk type tool. To estimate the rotordynamic coefficients of this new seal, a bulk flow model code that is based on a twocontrolvolume model developed by Matsuda for labyrinth seals was newly developed. This model uses the Hirs model for the viscous shear stresses. The friction factor coefficients for the rotor surface, the stator surface, and the surface between the twocontrolvolumes were determined by computational fluid dynamics (CFD) steady analysis. The rotordynamic coefficients can also be obtained by using CFD perturbation analysis. The high accuracy of the bulk flow model was demonstrated by comparing its results with CFD perturbation analysis results. In the perturbation analysis, the whirling motion was treated as a steadystate problem by using a rotating frame of reference. For the damper seal, the rotor surface and its neighboring region were treated with a rotating frame of reference and the neighboring region of the stator was treated with a stationary frame of reference. The damping property of the new seal was evaluated by conducting rotor stability tests using a highpressure compressor with an electromagnetic exciter. The new seal equipped with swirl brakes was used for the balance piston of the compressor. Stability was evaluated by exciting the rotor during operation and identifying the eigenvalues of the rotor. The experimental results showed that the new seal increases damping. Comparison of the damping effect with calculations based on the bulk flow analysis showed good agreement.
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      Development of Scallop Cut Type Damper Seal for Centrifugal Compressors

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    https://yetl.yabesh.ir/yetl1/handle/yetl/157896
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    contributor authorTakahashi, Naohiko
    contributor authorMiura, Haruo
    contributor authorNarita, Mitsuhiro
    contributor authorNishijima, Noriyo
    contributor authorMagara, Yohei
    date accessioned2017-05-09T01:17:39Z
    date available2017-05-09T01:17:39Z
    date issued2015
    identifier issn1528-8919
    identifier othergtp_137_03_032509.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/157896
    description abstractThis paper deals with a new type of damper seal developed for a highpressure centrifugal compressor. Honeycomb seals and hole pattern seals are popularly used as damper seals and provide superior rotordynamic damping characteristics. Honeycomb seals are expensive because the manufacturing process is complex. Hole pattern seals are easier to manufacture, but they are still expensive. Use of a scallop pattern is one way to reduce manufacturing cost and time. A new seal that has a scallop pattern and small teeth on the stator surface is proposed. This pattern is cut on the stator surface using a disk type tool. To estimate the rotordynamic coefficients of this new seal, a bulk flow model code that is based on a twocontrolvolume model developed by Matsuda for labyrinth seals was newly developed. This model uses the Hirs model for the viscous shear stresses. The friction factor coefficients for the rotor surface, the stator surface, and the surface between the twocontrolvolumes were determined by computational fluid dynamics (CFD) steady analysis. The rotordynamic coefficients can also be obtained by using CFD perturbation analysis. The high accuracy of the bulk flow model was demonstrated by comparing its results with CFD perturbation analysis results. In the perturbation analysis, the whirling motion was treated as a steadystate problem by using a rotating frame of reference. For the damper seal, the rotor surface and its neighboring region were treated with a rotating frame of reference and the neighboring region of the stator was treated with a stationary frame of reference. The damping property of the new seal was evaluated by conducting rotor stability tests using a highpressure compressor with an electromagnetic exciter. The new seal equipped with swirl brakes was used for the balance piston of the compressor. Stability was evaluated by exciting the rotor during operation and identifying the eigenvalues of the rotor. The experimental results showed that the new seal increases damping. Comparison of the damping effect with calculations based on the bulk flow analysis showed good agreement.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDevelopment of Scallop Cut Type Damper Seal for Centrifugal Compressors
    typeJournal Paper
    journal volume137
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4028448
    journal fristpage32509
    journal lastpage32509
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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