Axial balancing clip weight for rotor assembly and method...

Details Axial balancing clip weight for rotor assembly and method... Axial balancing clip weight for rotor assembly and method...

F - Mech Eng,Light,Heat,Weapons

16

F

F16F 15/34 (2006.01) F01D 5/06 (2006.01) F01D 25/04 (2006.01)

Patent

CA 2709140

A balancing weight clip for balancing a rotor assembly of a gas turbine engine which includes a weight portion, and a first flange engaging portion and a second flange engaging portion extending from the weight portion. The weight portion and the first and second flange engaging portions define a flange receiving opening for receiving a flange of a disc of the rotor assembly. The first flange engaging portion is provided with a detent facing the second flange engaging portion and engageable with a mating groove provided on a face of the flange. At least one of the first and second flange engaging portions is elastically deformable so that the first and second flange engaging portions are elastically moveable away from one another to removably receive the flange in the flange receiving opening and engage the detent with the mating groove.

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