Natural frequency tuning of gas turbine engine blades

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Blade cuff or shank construction

Reexamination Certificate

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Details

C416S500000, C416S248000

Reexamination Certificate

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10845237

ABSTRACT:
A tuning notch is defined preferably in the back of a blade root to tune the blade natural frequency in a gas turbine engine.

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