System for attaching a rotor blade to a rotor disk
AssigneeSociete Nationale d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
InventorsJacky Naudet, Jean-Louis Bertrand
Life of this patent
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Abstract
A locking and sealing system is disclosed for attaching a rotor blade to a rotor blade disk in a turbojet engine. The system has a first split ring member which locks the rotor blade foot portion onto the rotor blade disk. A second split ring member is inserted between the first split ring member in a downstream flange of the rotor blade foot portions to provide a positive seal to prevent air leakage between the foot portions and the notches formed in the rotor disk.
Claims13
A system for removably attaching and sealing a rotor blade to a rotor disk for a turbojet engine having a longitudinal axis comprising:
- (a) a plurality of substantially axially extending notches defined in the periphery of the rotor disk;
- (b) a foot formed on each rotor blade and adapted to be substantially axially slidably received in a notch of the rotor disk, the foot having thereon locating means to axially locate the foot with respect to the rotor disk, and a downstream flange defining a substantially circumferentially extending first groove opening radially inwardly;
- (c) a substantially circumferentially extending second groove defined by the rotor disk, the second groove opening radially outwardly;
- and
- (d) locking means to axially lock and seal the blade foot to the rotor disk comprising:
- (i) a first split ring member adapted to engage the first and second grooves;
- and,
- (ii) a second split ring member adapted to engage only the first grooves such that the sum of the axial thicknesses of the first and second members is substantially equal to the axial thickness of the first grooves.
A method of assembling, locking and sealing a rotor blade having a foot portion to a rotor wheel having a plurality of first notches defined by its periphery comprising the steps of:
- (a) displacing a first end of a first split ring member from the plane of the member;
- (b) circumferentially inserting the displaced end into a groove formed in the rotor disk and rotating the first split ring member until a second notch in the first split ring member is aligned with a first notch;
- (c) inserting the foot portion of the rotor blade into the first notch;
- (d) rotating the first split ring member until the second notch is aligned with a subsequent first notch causing the first split ring member to engage a groove formed in the foot of the inserted rotor blade to lock it in position;
- (e) repeating steps (c) and (d) until a rotor blade is inserted and locked in each first notch formed in the rotor disk;
- and,
- (f) inserting a second split ring member into the grooves defined by the foot portions of the blade between the first split ring member and a downstream portion of the blade foot.
Dependencies are inferred from the claim text.