Aerodynamic Design of Centrifugal Compressor Components Around Existing Rotor
Abstract
This case study covers the aerodynamic design of a centrifugal compressor that replaced an aging compressor experiencing leakage issues. The replacement compressor was required to reuse the existing rotor, bearings, seals, and baseplate. The existing diaphragms and casing internals were not available for inspection. A performance model had to be developed based on the existing spare rotor geometry and a flowpaththat was designed and matched to the rotor. The predicted performance exceeded the existing compressor performance and was verified on test.
Description
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Citation
Smith, Thomas; Scott, Shane (2020). Aerodynamic Design of Centrifugal Compressor Components Around Existing Rotor. Turbomachinery Laboratory, Texas A&M Engineering Experiment Station; Texas A & M University. Libraries; Texas A & M University. Libraries. Available electronically from https : / /hdl .handle .net /1969 .1 /196814.