MULTISTAGE COMPRESSOR AND METHOD FOR OPERATING A MULTISTAGE COMPRESSOR

A multi-stage compressor is described, comprising a rotor having a plurality of axially stacked impellers and a tie rod extending through the stacked impellers and holding the impellers together. A gas compression path extends from a compressor inlet to a compressor outlet and through the impellers....

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: FORMICHINI MARCO, KOSAMANA BHASKARA, BIGI MANUELE, V KALYANKUMAR, BORGHETTI MASSIMILIANO, KURVA LAKSHMANUDU
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A multi-stage compressor is described, comprising a rotor having a plurality of axially stacked impellers and a tie rod extending through the stacked impellers and holding the impellers together. A gas compression path extends from a compressor inlet to a compressor outlet and through the impellers. A flow channel is provided between the tie rod and the stacked impellers. The flow channel develops along at least a portion of the tie rod. Hot gas is diverted from the compression path and flows through the flow channel to heat the tie rod during startup of the compressor.