NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Experimental on-stream elimination of resonant whirl in a large centrifugal compressorResonant whirl condition during operation of a multi-stage centrifugal compressor at higher than anticipated speeds and loads was reported. The condition was diagnosed by a large scale computerized Machinery Condition Monitoring System (MACMOS). This computerized system verified that the predominant subsynchronous whirl frequency locked in on the first resonant frequency of the compressor rotor and did not vary with compressor speed. Compressor stability calculations showed the rotor system had excessive hearing stiffness and inadequate effective damping. An optimum bearing design which was developed to minimize the unbalance response and to maximize the stability threshold is presented.
Document ID
19850005812
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bhat, G. I.
(Exxon Chemical Co., Inc. Baytown, TX, United States)
Eierman, R. G.
(Exxon Chemical Co., Inc. Baytown, TX, United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Rotordynamic Instability Problems in High-Performance Turbomachinery
Subject Category
Mechanical Engineering
Accession Number
85N14121
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available