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Practical experience with unstable compressorsUsing analytical mathematical modeling techniques for the system components, an attempt is made to gauge the destabilizing effects in a number of compressor designs. In particular the overhung (or cantilevered) compressor designs and the straddle-mounted (or simply supported) compressor designs are examined. Recommendations are made, based on experiences with stable and unstable compressors, which can be used as guides in future designs. High and low pressure compressors which operate well above their fundamental rotor-bearing lateral natural frequencies can suffer from destructive subsynchronous vibration. Usually the elements in the system design which contribute to this vibration, other than the shafting and the bearings, are the seals (both gas labyrinth and oil breakdown bushings) and the aerodynamic components.
Document ID
19800021208
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Malanoski, S. B.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Publication Information
Publication: NASA. Lewis Res. Center Rotordyn. Instability Probl. in High-Performance Turbomachinery p35-43 (SEE N80-29706 20-37)
Subject Category
Mechanical Engineering
Accession Number
80N29709
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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