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A New 1000 F Magnetic Bearing Test RigNASA and the Army are currently exploring the possibility of using magnetic bearings in gas turbine engines. The use of magnetic bearings in gas turbine engines could increase the reliability by eliminating the lubrication system. The use of magnetic bearings could also increase the speed and the size of the shafts in the engine, thus reducing vibrations and possibly eliminating third bearings. Magnetic bearings can apply forces to the shafts and move them so that blade tips and seals do not rub. This could be part of an active vibration cancellation system. Also, whirling (displacing the shaft center line) may delay rotating stall and increase the stall margin of the engine. Magnetic bearings coupled with an integral starter generator could result in a more efficient 'more electric' engine. The IHPTET program, a joint DOD-industry program, has identified a need for a high temperature, (as high as 1200 F), magnetic bearing that could be demonstrated in a phase m engine. A magnetic bearing is similar to an electric motor. The magnetic bearing has a laminated rotor and stator made out of cobalt steel. The stator has a series of coils of wire wound around it. These coils f u. a series of electromagnets around the circumference. These magnets exert a force on the rotor to keep the rotor in the center of the cavity. The centering force is commanded by a controller based on shaft position, (measured by displacement probes). The magnetic bearing can only pull and is basically unstable before active control is applied The engine shafts, bearings, and case form a flexible structure which contain a large number of modes. A controller is necessary to stabilize these modes. A power amplifier is also necessary to provide the current prescribed by the controller to the magnetic bearings. In case of very high loads, a conventional back up bearing will engage and stop the rotor and stator from rubbing.
Document ID
19970026140
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kascak, Albert F.
(Army Research Lab. Cleveland, OH United States)
Montague, Gerald T.
(Army Research Lab. Cleveland, OH United States)
Brown, Gerald V.
(NASA Lewis Research Center Cleveland, OH United States)
Palazzolo, Alan B.
(Texas A&M Univ. College Station, TX United States)
Date Acquired
August 17, 2013
Publication Date
April 1, 1997
Publication Information
Publication: Physics and Process Modeling (PPM) and Other Propulsion R and T
Volume: 2
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
Paper-30
Accession Number
97N25488
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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