The 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.
Skip Nav Destination
Article navigation
January 1998
Research Papers
High-Speed Rotor Losses in a Radial Eight-Pole Magnetic Bearing: Part 1—Experimental Measurement
M. E. F. Kasarda,
M. E. F. Kasarda
Department of Mechanical, Nuclear, and Aerospace Engineering, University of Virginia, Charlottesville, VA 22903
Search for other works by this author on:
P. E. Allaire,
P. E. Allaire
Department of Mechanical, Nuclear, and Aerospace Engineering, University of Virginia, Charlottesville, VA 22903
Search for other works by this author on:
E. H. Maslen,
E. H. Maslen
Department of Mechanical, Nuclear, and Aerospace Engineering, University of Virginia, Charlottesville, VA 22903
Search for other works by this author on:
G. R. Brown,
G. R. Brown
NASA Lewis Research Center, Cleveland, OH 44135
Search for other works by this author on:
G. T. Gillies
G. T. Gillies
Department of Mechanical, Nuclear, and Aerospace Engineering, University of Virginia, Charlottesville, VA 22903
Search for other works by this author on:
M. E. F. Kasarda
Department of Mechanical, Nuclear, and Aerospace Engineering, University of Virginia, Charlottesville, VA 22903
P. E. Allaire
Department of Mechanical, Nuclear, and Aerospace Engineering, University of Virginia, Charlottesville, VA 22903
E. H. Maslen
Department of Mechanical, Nuclear, and Aerospace Engineering, University of Virginia, Charlottesville, VA 22903
G. R. Brown
NASA Lewis Research Center, Cleveland, OH 44135
G. T. Gillies
Department of Mechanical, Nuclear, and Aerospace Engineering, University of Virginia, Charlottesville, VA 22903
J. Eng. Gas Turbines Power. Jan 1998, 120(1): 105-109 (5 pages)
Published Online: January 1, 1998
Article history
Received:
February 1, 1996
Online:
November 19, 2007
Citation
Kasarda, M. E. F., Allaire, P. E., Maslen, E. H., Brown, G. R., and Gillies, G. T. (January 1, 1998). "High-Speed Rotor Losses in a Radial Eight-Pole Magnetic Bearing: Part 1—Experimental Measurement." ASME. J. Eng. Gas Turbines Power. January 1998; 120(1): 105–109. https://doi.org/10.1115/1.2818059
Download citation file:
Get Email Alerts
Cited By
On Leakage Flows In A Liquid Hydrogen Multi-Stage Pump for Aircraft Engine Applications
J. Eng. Gas Turbines Power
A Computational Study of Temperature Driven Low Engine Order Forced Response In High Pressure Turbines
J. Eng. Gas Turbines Power
The Role of the Working Fluid and Non-Ideal Thermodynamic Effects on Performance of Gas Lubricated Bearings
J. Eng. Gas Turbines Power
Tool wear prediction in broaching based on tool geometry
J. Eng. Gas Turbines Power
Related Articles
Experimentally Determined Rotor Power Losses in Homopolar and Heteropolar Magnetic Bearings
J. Eng. Gas Turbines Power (October,1999)
High-Speed Rotor Losses in a Radial Eight-Pole Magnetic Bearing: Part 2—Analytical/Empirical Models and Calculations
J. Eng. Gas Turbines Power (January,1998)
Rotor Power Losses in Planar Radial Magnetic Bearings—Effects of Number of Stator Poles, Air Gap Thickness, and Magnetic Flux Density
J. Eng. Gas Turbines Power (October,1999)
Bond Graph Modeling of an Internally Damped Nonideal Flexible Spinning Shaft
J. Dyn. Sys., Meas., Control (November,2010)
Related Proceedings Papers
Related Chapters
Key Components of Liquid Cooled Systems
Thermal Design of Liquid Cooled Microelectronic Equipment
Characteristics Measurement and FPGA Controller Design for an Air Motor and Electric Motor Hybrid Power System
International Conference on Instrumentation, Measurement, Circuits and Systems (ICIMCS 2011)
A Utility Perspective of Wind Energy
Wind Turbine Technology: Fundamental Concepts in Wind Turbine Engineering, Second Edition