Rotor with improved balancing features

Details Rotor with improved balancing features Rotor with improved balancing features

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/10 (2006.01) F01D 5/26 (2006.01)

Patent

CA 2663848

A rotor assembly for a gas turbine engine including a circumferential array of regularly spaced apart features provided on the disk which are each configured for receiving a balancing weight. The circumferential array of features has an angular orientation relative to the circumferential array of blades such that the features are each located at an at least substantially same offset angle from a stacking line of a respective adjacent blade.

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