Aerofoil assembly

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

Reexamination Certificate

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Details

C416S21900R, C416S500000, C029S889210

Reexamination Certificate

active

08066489

ABSTRACT:
An aerofoil assembly includes a plurality of rotatable blades. A damping member is disposed between at least two of the blades, each of the at least two blades having an aerofoil portion, a stem portion and a root portion. A recess is provided on two cooperating stem portions with a first shelf extending from a first end of each recess, and a second shelf extending from a second end of each recess to define a compartment. When the blades are aligned the damping member is held on one side of the shelves within the compartment. The damping member is provided with a projection at one corner and a projection on a diagonally opposite corner, the longitudinal distance between ends of the projections being greater than the distance between edges of the first and second shelf.

REFERENCES:
patent: 4566857 (1986-01-01), Brumen
patent: 5256035 (1993-10-01), Norris et al.
patent: 5261790 (1993-11-01), Dietz et al.
patent: 5924699 (1999-07-01), Airey et al.
patent: 6659725 (2003-12-01), Yeo et al.
patent: 7322797 (2008-01-01), Lee et al.
patent: 1 291 492 (2003-03-01), None
patent: 1 635 037 (2006-03-01), None

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