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    Test Results and Analytical Predictions for MIL STD 167 Vibration Testing of a Direct Drive Compressor Supported on Magnetic Bearings

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 005::page 52507
    Author:
    Hawkins, Lawrence A.
    ,
    Khatri, Rasish K.
    ,
    Nambiar, Koman B.
    DOI: 10.1115/1.4028684
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: External vibration testing was performed on a semihermetic, direct drive compressor on magnetic bearings intended for U.S. Navy Shipboard use. The compressor was placed on a U.S. Navy MILSTD167 shaker platform and driven at sinusoidal frequencies from 4 to 33 Hz at graduated displacements equal to a maximum of 1.5 Gs. During the machine design phase, a linear forced response analysis of the coupled rotordynamic system model of the rotor, housing, and magnetic bearings was performed to predict rotor/housing displacements and actuator loads. The results were used to guide bearing sizing and control algorithm design. The measured rotor motion and actuator currents correlated well with predictions at all tested frequencies, amplitudes, and orientations. Analysis methodology, test results, and comparisons are reported here.
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      Test Results and Analytical Predictions for MIL STD 167 Vibration Testing of a Direct Drive Compressor Supported on Magnetic Bearings

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/157950
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorHawkins, Lawrence A.
    contributor authorKhatri, Rasish K.
    contributor authorNambiar, Koman B.
    date accessioned2017-05-09T01:17:51Z
    date available2017-05-09T01:17:51Z
    date issued2015
    identifier issn1528-8919
    identifier othergtp_137_05_052507.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/157950
    description abstractExternal vibration testing was performed on a semihermetic, direct drive compressor on magnetic bearings intended for U.S. Navy Shipboard use. The compressor was placed on a U.S. Navy MILSTD167 shaker platform and driven at sinusoidal frequencies from 4 to 33 Hz at graduated displacements equal to a maximum of 1.5 Gs. During the machine design phase, a linear forced response analysis of the coupled rotordynamic system model of the rotor, housing, and magnetic bearings was performed to predict rotor/housing displacements and actuator loads. The results were used to guide bearing sizing and control algorithm design. The measured rotor motion and actuator currents correlated well with predictions at all tested frequencies, amplitudes, and orientations. Analysis methodology, test results, and comparisons are reported here.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTest Results and Analytical Predictions for MIL STD 167 Vibration Testing of a Direct Drive Compressor Supported on Magnetic Bearings
    typeJournal Paper
    journal volume137
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4028684
    journal fristpage52507
    journal lastpage52507
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 005
    contenttypeFulltext
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