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The Application of a Cylindrical-spherical Floating Ring Bearing as a Device to Control Stability of TurbogeneratorsThe development of a new device to control stability of turbogenerators is described. The device comprises a floating ring installed between the journal and bearing housing of a fluid film bearing. The journal and the inner surface of the ring are cylindrical while the outer surface of the ring and bearing surface are spherical providing axial location of the ring and self-alignment of the bearing. The employment of this device would lead to a consistent machine performance. System stability may be controlled by changing a number of bearing and floating ring parameters. This device also offers an additional advantage of having a very low frictional characteristic. A feasibility study was carried out to investigate the suitability of the new device to turbogenerator applications. Both theoretical analysis and experimental observations were carried out. Initial results suggest that the new floating ring device is a competitive alternative to other conventional arrangements.
Document ID
19920005153
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leung, P. S.
(Newcastle Polytechnic Newcastle-upon-Tyne (England)., United States)
Craighead, I. A.
(Newcastle Polytechnic Newcastle-upon-Tyne (England)., United States)
Wilkinson, T. S.
(NEI Parsons Ltd. Newcastle-upon-Tyne, United Kingdom)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Publication Information
Publication: NASA. Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1990
Subject Category
Mechanical Engineering
Accession Number
92N14371
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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