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contributor authorM. E. F. Kasarda
contributor authorG. R. Brown
contributor authorG. T. Gillies
contributor authorP. E. Allaire
contributor authorE. H. Maslen
date accessioned2017-05-08T23:56:39Z
date available2017-05-08T23:56:39Z
date copyrightJanuary, 1998
date issued1998
identifier issn1528-8919
identifier otherJETPEZ-26775#105_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120472
description abstractThe continual increase in the use of magnetic bearings in various capacities, including high-speed aerospace applications such as jet engine prototypes, dictates the need to quantify power losses in this type of bearing. The goal of this study is to present experimentally measured power losses during the high-speed operation of a pair of magnetic bearings. A large-scale test rotor has been designed and built to obtain unambiguous power loss measurements while varying a variety of test parameters. The test apparatus consists of a shaft supported in two radial magnetic bearings and driven by two electric motors also mounted on the shaft. The power losses of the spinning rotor are determined from the time rate of change of the kinetic energy of the rotor as its angular speed decays during free rotation. Measured results for the first set of magnetic bearings, a pair of eight-pole planar radial bearings, are presented here. Data from three different parameter studies including the effect of the bias flux density, the effect of the bearing pole configuration, and the effect of the motor stator on the power loss are presented. Rundown plots of the test with the bearings in the paired pole (NNSS) versus the alternating (NSNS) pole configuration show only small differences, with losses only slightly higher when the poles are in the alternating pole (NSNS) configuration. Loss data were also taken with the motor stators axially removed from the motor rotors for comparison with the case where the motor stators are kept in place. No measurable difference was observed between the two cases, indicating negligible windage and residual magnetic effects. Throughout most of the speed range, the dominant loss mechanism appears to be eddy currents.
publisherThe American Society of Mechanical Engineers (ASME)
titleHigh-Speed Rotor Losses in a Radial Eight-Pole Magnetic Bearing: Part 1—Experimental Measurement
typeJournal Paper
journal volume120
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2818059
journal fristpage105
journal lastpage109
identifier eissn0742-4795
keywordsPoles (Building)
keywordsRotors
keywordsMagnetic bearings
keywordsBearings
keywordsEngines
keywordsStators
keywordsMechanisms
keywordsKinetic energy
keywordsJet engines
keywordsSpin (Aerodynamics)
keywordsEngineering prototypes
keywordsAerospace industry
keywordsDensity
keywordsRotation
keywordsElectric motors
keywordsMeasurement AND Eddies (Fluid dynamics)
treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 001
contenttypeFulltext


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