Radial balancing clip weight for rotor assembly
AssigneePratt & Whitney Canada Corp.
InventorsDAVID F. GLASSPOOLE, FRANCOIS CARON
Life of this patent
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AssigneePratt & Whitney Canada Corp.
InventorsDAVID F. GLASSPOOLE, FRANCOIS CARON
Estimating the term…
A balancing weight clip with a mass adapted to balance a rotor assembly of a gas turbine engine, includes a weight portion, a first flange engaging portion and a second flange engaging portion extending from the weight portion, each being engageable with a sidewall of at least one recess located on an edge of a flange of a disc of the rotor assembly. Each flange engaging portion is provided with a hook engageable with a mating groove provided on a face of the flange. At least one of the first and second flange engaging portions is resiliently biased so that the first and second flange engaging portions are elastically moveable away from one another to removably secure the balancing weight clip to the flange and engage each hook with the mating groove.
A rotor assembly for a gas turbine engine, comprising:
A balancing weight clip having a mass adapted to balance a rotor assembly of a gas turbine engine, comprising:
A method for balancing a rotor disc having two opposed faces and an axially extending flange projecting from one of the two opposed faces of the disc and circularly extending thereon, an edge of the flange having at least one recess, the flange having a groove discontinuously extending about a circumference thereof, the method comprising:
Dependencies are inferred from the claim text.