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Vibration and destabilizing effects of floating ring seals in compressorsOperating experience on a compressor commissioned 12 years ago has presented an interesting history of sporadic increases in shaft vibration. Initial operation was satisfactory with low levels of vibration. However, after some time the shaft vibration level increased to several mils. Initially this was believed to be due to rotor unbalance from deposits formed in the passages due to process upsets. After cleaning up the rotor, operation was again increased. It was then found that the rotor vibration was primarily subsynchronous. Further investigation revealed that the original seal design was subject to wear and was no longer properly pressure balanced. A modified seal design was installed and it has operated successfully for the past six years.
Document ID
19830007371
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Emerick, M. F.
(Allis-Chalmers Mfg. Co. Milwaukee, WI, United States)
Date Acquired
August 11, 2013
Publication Date
December 1, 1982
Publication Information
Publication: NASA. Lewis Research Center Rotordyn. Instability Probl. in High-Performance Turbomachinery
Subject Category
Mechanical Engineering
Accession Number
83N15642
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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