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...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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