Rotor for a compressor

minA rotor for a compressor, in particular in a gas turbine, has a number of rotor blades which are arranged around the rotation axis of the rotor in the form of a rim and are each held in a circumferential recess on the rotor by a blade root, with the blade root having a widening lower part which e...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Bachofner, René, Grigioni, Pietro, Kappis, Wolfgang
Format: Patent
Sprache:eng
Online-Zugang:Volltext bestellen
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