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The Effects of Manufacturing Tolerances on the Vibration of Aero-engine Rotor-damper AssembliesA range of rotor assemblies incorporating one and two squeeze film dampers with various static misalignments is investigated. Waterfall diagrams are constructed which demonstrate the effects of such misalignment and damper support flexibility on the nature and severity of subsynchronous resonance and jump phenomena. Vibration signatures of similar rotor-bearing assemblies are shown to contrast strongly due to different accumulations of tolerances during manufacture, fitting, and operation.
Document ID
19920005131
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sykes, J. E. H.
(Southampton Univ.)
Holmes, R.
(Southampton Univ.)
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
92N14349
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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