Balancing apparatus for rotor assembly

Details Balancing apparatus for rotor assembly Balancing apparatus for rotor assembly

F - Mech Eng,Light,Heat,Weapons

16

F

F16F 15/34 (2006.01) F01D 5/02 (2006.01) F01D 5/10 (2006.01) F16F 15/28 (2006.01)

Patent

CA 2712143

A balancing assembly for a rotor assembly of a gas turbine engine includes a flange engaging portion defining a flange receiving opening for mating with the flange in a slidable manner. A hole extends through at least part of the flange engaging portion, the hole corresponding in size to a recess and adapted to receive a rivet or other suitable fastener to fix the balancing weight with respect to the disc.

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