Affiliation:
1. Dresser-Rand Company, Olean, NY
Abstract
This paper describes the rotor dynamic stability analysis and the PTC-10 Class 1 test of a three body centrifugal compressor train for high pressure natural gas injection service. This train had a full load full pressure string test on hydrocarbon gasses to a final discharge pressure of 500 BAR (7250 PSIA). Each compressor is of the back to back configuration, and is equipped with tilting pad seats, damper bearings, and a honeycomb labyrinth at the division wall with shunt holes. The driver is a gas turbine.
Publisher
American Society of Mechanical Engineers
Cited by
2 articles.
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1. SPECIALTY OF ROTOR’S DRIVE MECHANISM OSCILLATIONS;Science and Transport Progress. Bulletin of Dnipropetrovsk National University of Railway Transport;2016-02-25
2. Dynamic Characteristics of the Diverging Taper Honeycomb-Stator Seal;Journal of Turbomachinery;2004-03-01