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High Speed, High Temperature, Fault Tolerant Operation of a Combination Magnetic-Hydrostatic Bearing Rotor Support System for TurbomachineryClosed loop operation of a single, high temperature magnetic radial bearing to 30,000 RPM (2.25 million DN) and 540 C (1000 F) is discussed. Also, high temperature, fault tolerant operation for the three axis system is examined. A novel, hydrostatic backup bearing system was employed to attain high speed, high temperature, lubrication free support of the entire rotor system. The hydrostatic bearings were made of a high lubricity material and acted as journal-type backup bearings. New, high temperature displacement sensors were successfully employed to monitor shaft position throughout the entire temperature range and are described in this paper. Control of the system was accomplished through a stand alone, high speed computer controller and it was used to run both the fault-tolerant PID and active vibration control algorithms.
Document ID
20040050626
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Jansen, Mark
(Toledo Univ. OH, United States)
Montague, Gerald
(Army Research Lab. Cleveland, OH, United States)
Provenza, Andrew
(NASA Glenn Research Center Cleveland, OH, United States)
Palazzolo, Alan
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2004
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
GT2004-53321
E-14391
NASA/TM-2004-212952
ARL-TR-3156
NAS 1.15-212952
Meeting Information
Meeting: Turbo Expo 2004
Location: Vienna
Country: Austria
Start Date: June 14, 2004
End Date: June 17, 2004
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
OTHER: 1L162211A47A
WBS: WBS-22-714-70-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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