Retention system for bar-type damper of rotor blade

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Axially extending shroud ring or casing

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Details

416193A, 416248, 416500, F01D 526

Patent

active

057497052

ABSTRACT:
A rotor blade for a rotor of a gas turbine engine having an axis of rotation including a root portion, a platform portion connected to the root portion and having a damper pocket formed therein, an airfoil portion connected to the platform portion, a generally bar-shaped damping member loosely arranged in the damper pocket having at least one scrubbing surface, and at least one retainer pin for retaining the bar-shaped damping member in the damper pocket. The bar-shaped damping member is slidably displaceable and rotatable within the damper pocket during rotation of the rotor. The damper pocket in the platform portion has a rear surface with an upper portion and a lower portion at an angle to the upper portion, a pair of spaced side surfaces, and a pair of spaced lower surfaces extending from the rear surface lower portion which are substantially coplanar. The damper pocket lower surfaces are provided by a first flange extending laterally inward from one of the side surfaces and a second flange extending laterally inward from the other side surface, where a retainer pin extends through and is connected to at least one of the first and second flanges so as to retain the bar-shaped damping member within the damper pocket.

REFERENCES:
patent: 3266770 (1966-08-01), Harlow
patent: 4516910 (1985-05-01), Bouiller et al.
patent: 5215442 (1993-06-01), Steckle et al.
patent: 5226784 (1993-07-01), Mueller et al.
patent: 5261790 (1993-11-01), Dietz et al.
patent: 5302085 (1994-04-01), Dietz et al.
patent: 5369882 (1994-12-01), Dietz et al.

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