Compressor arrangement

A compressor arrangement (1) has a common shaft (4), an axial compressor (2) having at least a single-stage, and a radial compressor (3) having at least single-stage. Assemblies of the, or each, axial compressor stage on the rotor side and assemblies of the, or each, radial compressor stage on the r...

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Bibliographische Detailangaben
Hauptverfasser: KLAUS HOERMEYER, DIRK ANDING, ROLAND EMMRICH, HENNING RESSING, BERNHARD EISENBERG
Format: Patent
Sprache:eng
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Zusammenfassung:A compressor arrangement (1) has a common shaft (4), an axial compressor (2) having at least a single-stage, and a radial compressor (3) having at least single-stage. Assemblies of the, or each, axial compressor stage on the rotor side and assemblies of the, or each, radial compressor stage on the rotor side are attached to a common shaft (4). A ratio between a maximum diameter of the shaft (4) in the region of the axial compressor (2) and a minimum radial impeller seat diameter of the shaft (4) in the region of the radial compressor (3) is between 1.5 and 3.0.