Turbine rotor blade assembly and method of assembling same

A rotor blade assembly (100) for a rotor (30) of a gas turbine engine (10) having an axis of rotation (8) includes a shank portion (106) formed from a ceramic matrix composite (CMC) material. The rotor blade assembly also includes a platform portion (104) formed from a substantially similar CMC mate...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Izon, Paul, Verrilli, Michael James, Marusko, Mark Willard, Noe, Mark Eugene, Paige II, Anthony Reid, Jamison, Joshua Brian
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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