Gas turbine engine balancing

Details Gas turbine engine balancing Gas turbine engine balancing

F - Mech Eng,Light,Heat,Weapons

16

F

F16F 15/34 (2006.01) F01D 5/02 (2006.01) F01D 5/10 (2006.01) F02C 7/12 (2006.01)

Patent

CA 2715271

An apparatus and method for balancing a gas turbine engine rotor includes a plurality of balancing weights adapted to be selectively attached to at least one of inlets or outlets of a cooling passage of the rotor. The weights include cooling access which permits coolant to communicate with the cooling passage.

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