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Analysis and identification of subsynchronous vibration for a high pressure parallel flow centrifugal compressorThe summary of a complete analytical design evaluation of an existing parallel flow compressor is presented and a field vibration problem that manifested itself as a subsynchronous vibration that tracked at approximately 2/3 of compressor speed is reviewed. The comparison of predicted and observed peak response speeds, frequency spectrum content, and the performance of the bearing-seal systems are presented as the events of the field problem are reviewed. Conclusions and recommendations are made as to the degree of accuracy of the analytical techniques used to evaluate the compressor design.
Document ID
19800021209
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kirk, R. G.
(Ingersoll-Rand Co. Easton, PA, United States)
Nicholas, J. C.
(Ingersoll-Rand Co. Easton, PA, United States)
Donald, G. H.
(Ingersoll-Rand Co. Easton, PA, United States)
Murphy, R. C.
(Ingersoll-Rand Co. Easton, PA, 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
Subject Category
Mechanical Engineering
Accession Number
80N29710
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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