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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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