BLADE FOR A ROTOR ASSEMBLY OF A TURBINE ENGINE

A blade for mounting on a rotor disc of a turbine engine includes platform segments between a airfoil and blade root and extending laterally from the blade, the platform segment having a curved profile defining a platform recess on a root side of the platform segment, the recess configured to cooper...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: LECUYER, Daniel, HUSZAR, Robert
Format: Patent
Sprache:eng
Schlagworte:
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