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NASA NTRS · 19800021212

Asynchronous vibration problem of centrifugal compressor

Abstract

An unstable asynchronous vibration problem in a high pressure centrifugal compressor and the remedial actions against it are described. Asynchronous vibration of the compressor took place when the discharge pressure (Pd) was increased, after the rotor was already at full speed. The typical spectral data of the shaft vibration indicate that as the pressure Pd increases, pre-unstable vibration appears and becomes larger, and large unstable asynchronous vibration occurs suddenly (Pd = 5.49MPa). A computer program was used which calculated the logarithmic decrement and the damped natural frequency of the rotor bearing systems. The analysis of the log-decrement is concluded to be effective in preventing unstable vibration in both the design stage and remedial actions.

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BibTeXRIS

Fujikawa, T., Ishiguro, N., Ito, M.. 1980-01-01. Asynchronous vibration problem of centrifugal compressor. https://ntrs.nasa.gov/citations/19800021212

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