ROTOR FOR A TURBOMACHINE AND TURBOMACHINE

The invention relates to a rotor for a turbomachine, having at least one blade and having at least one rotor main part, which has at least one recess, in which a blade root of the least one blade is interlockingly received, wherein the blade root comprises at least one depression, in which at least...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Freno, Dieter, Pernleitner, Martin, Dopfer, Manfred, Hummel, Tino, Wittig, Klaus
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:The invention relates to a rotor for a turbomachine, having at least one blade and having at least one rotor main part, which has at least one recess, in which a blade root of the least one blade is interlockingly received, wherein the blade root comprises at least one depression, in which at least one protrusion of the at least one rotor main part which protrusion delimits the at least one recess in regions is received, wherein the at least one depression is delimited by a first delimiting face on the blade root side and the at least one protrusion is delimited by a second delimiting face on the rotor main part side. At least the first delimiting face has at least one elevation which narrows a gap at least in regions, which extends between the first delimiting face and the second delimiting face.