Method of balancing a gas turbine engine rotor

G - Physics – 01 – M

Patent

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G01M 1/38 (2006.01) F01D 5/10 (2006.01) F16F 15/22 (2006.01)

Patent

CA 2694165

A method of balancing an assembly of rotary parts of a gas turbine engine (10) comprising measuring at least one of the concentricity and parallelism of each component and considering globally all possible component stacking positions to generate an optimized stacking position for each component of the assembly to minimize assembly unbalance.

L'invention concerne un procédé d'équilibrage d'un ensemble de composants rotatifs d'un moteur à turbine à gaz (10), le procédé comprenant la mesure d'au moins la concentricité ou le parallélisme de chaque composant et la prise en compte de manière globale de toutes les positions d'empilement de composants possibles pour générer une position d'empilement optimisée pour chaque composant de l'ensemble afin de réduire au minimum le déséquilibre de l'ensemble.

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