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An Overview of Magnetic Bearing Technology for Gas Turbine EnginesThe idea of the magnetic bearing and its use in exotic applications has been conceptualized for many years, over a century, in fact. Patented, passive systems using permanent magnets date back over 150 years. More recently, scientists of the 1930s began investigating active systems using electromagnets for high-speed ultracentrifuges. However, passive magnetic bearings are physically unstable and active systems only provide proper stiffness and damping through sophisticated controllers and algorithms. This is precisely why, until the last decade, magnetic bearings did not become a practical alternative to rolling element bearings. Today, magnetic bearing technology has become viable because of advances in micro-processing controllers that allow for confident and robust active control. Further advances in the following areas: rotor and stator materials and designs which maximize flux, minimize energy losses, and minimize stress limitations; wire materials and coatings for high temperature operation; high-speed micro processing for advanced controller designs and extremely robust capabilities; back-up bearing technology for providing a viable touchdown surface; and precision sensor technology; have put magnetic bearings on the forefront of advanced, lubrication free support systems. This paper will discuss a specific joint program for the advancement of gas turbine engines and how it implies the vitality of magnetic bearings, a brief comparison between magnetic bearings and other bearing technologies in both their advantages and limitations, and an examination of foreseeable solutions to historically perceived limitations to magnetic bearing.
Document ID
20040110826
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Clark, Daniel J.
(Toledo Univ. OH, United States)
Jansen, Mark J.
(Toledo Univ. OH, United States)
Montague, Gerald T.
(Army Research Lab. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2004
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ARL-TR-3254
E-14672
NASA/TM-2004-213177
Report Number: ARL-TR-3254
Report Number: E-14672
Report Number: NASA/TM-2004-213177
Funding Number(s)
WBS: WBS 22-708-01-03
PROJECT: DA Proj. 1L1-62211-A-47-A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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