Aircraft fan blade damping apparatus

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Blade received in well or slot

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Details

416217, 416248, 416500, F01D 526

Patent

active

052057143

ABSTRACT:
Disclosed is apparatus to prevent vibration of a pinned root fan blade during low speed revolution of the blade comprising a damping device which extends between the airfoil of the blade and the engine structure.

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