GAS TURBINE ENGINE FAN ROTOR DISK AND GAS TURBINE ENGINE Russian patent published in 2012 - IPC F04D29/34 F04D19/00 F01D5/32 F02C7/00 

Abstract RU 2454572 C2

FIELD: engines and pumps.

SUBSTANCE: proposed rotor disk comprises, in fact, axial slots made along its edges to receive and lock vane roots with hooks on their rear ends. Note here that deformable zones are made at slot rear ends formed by cavities. Note also that said cavities are arranged in flanges jointing between-the-vanes surfaces.

EFFECT: decreased wear, longer life.

6 cl, 5 dwg

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RU 2 454 572 C2

Authors

Le Khong Son

Dates

2012-06-27Published

2008-01-17Filed