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Full load shop testing of 18,000-hp gas turbine driven centrifugal compressor for offshore platform service: Evaluation of rotor dynamics performanceThe results for in-plant full load testing of a 13.4 MW (18000 HP) gas turbine driven centrifugal compressor are presented and compared to analytical predictions of compressor rotor stability. Unique problems from both oil seals and labyrinth gas seals were encountered during the testing. The successful resolution of these problems are summarized.
Document ID
19860020689
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kirk, R. G. (Ingersoll-Rand Co. Phillipsburg, NJ, United States)
Simpson, M. (Ingersoll-Rand Co. Ltd. Wythenshawe (England), United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1985
Publication Information
Publication: NASA. Lewis Research Center Instability in Rotating Machinery
Subject Category
Mechanical Engineering
Accession Number
86N30161
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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