BLADED ROTOR WHEEL

The invention provides a bladed rotor wheel of an aero turbine stage comprising a portion of a rotor blade with a shank portion and a bottom surface; a portion of a forged rotor disk with a rim portion and an outer surface; and a joining structure provided by an additive manufacturing process config...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: BALANDIER, Quentin Luc
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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Beschreibung
Zusammenfassung:The invention provides a bladed rotor wheel of an aero turbine stage comprising a portion of a rotor blade with a shank portion and a bottom surface; a portion of a forged rotor disk with a rim portion and an outer surface; and a joining structure provided by an additive manufacturing process configured for integrally merging the portion of a rotor blade with the portion of a forged rotor disk. The invention also provides an aero turbine comprising such bladed rotor wheel and an aircraft comprising such aero turbine.