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High stability design for new centrifugal compressorIt is essential that high-performance centrifugal compressors be free of subsynchronous vibrations. A new high-performance centrifugal compressor has been developed by applying the latest rotordynamics knowledge and design techniques: (1) To improve the system damping, a specially designed oil film seal was developed. This seal attained a damping ratio three times that of the conventional design. The oil film seal contains a special damper ring in the seal cartridge. (2) To reduce the destabilizing effect of the labyrinth seal, a special swirl canceler (anti-swirl nozzle) was applied to the balance piston seal. (3) To confirm the system damping margin, the dynamic simulation rotor model test and the full load test applied the vibration exciting test in actual load conditions.
Document ID
19890013546
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kanki, H.
(Mitsubishi Heavy Industries Ltd. Takasago, Japan)
Katayama, K.
(Mitsubishi Heavy Industries Ltd. Takasago, Japan)
Morii, S.
(Mitsubishi Heavy Industries Ltd. Takasago, Japan)
Mouri, Y.
(Mitsubishi Heavy Industries Ltd. Takasago, Japan)
Umemura, S.
(Mitsubishi Heavy Industries Ltd. Takasago, Japan)
Ozawa, U.
(Mitsubishi Heavy Industries Ltd. Takasago, Japan)
Oda, T.
(Mitsubishi Heavy Industries Ltd. Takasago, Japan)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Publication Information
Publication: NASA, Lewis Research Center, Rotordynamic Instability Problems in High-Performance Turbomachinery, 1988
Subject Category
Mechanical Engineering
Accession Number
89N22917
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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