초록 ▼

A system for balancing a rotatable gas turbine engine component. The system includes two balance rings that are coupled to the component by mating splines on the respective item. Each of the rings has a mass asymmetry that is indexable relative to the primary component to achieve the imbalance corr

A system for balancing a rotatable gas turbine engine component. The system includes two balance rings that are coupled to the component by mating splines on the respective item. Each of the rings has a mass asymmetry that is indexable relative to the primary component to achieve the imbalance correction.

대표청구항 ▼

What is claimed: 1. A system comprising: a rotatable gas turbine engine component adapted to rotate about a centerline, said component including a first circular portion having a first splined surface with a plurality of first spline teeth; a pair of counterweight rings located adjacent one another

What is claimed: 1. A system comprising: a rotatable gas turbine engine component adapted to rotate about a centerline, said component including a first circular portion having a first splined surface with a plurality of first spline teeth; a pair of counterweight rings located adjacent one another and rotatable with said component, each of said rings having a mass asymmetric portion that is positioned relative to said component to effect an unbalance condition of said component and a second circular portion including a second splined surface with a plurality of second spline teeth for coupling with said plurality of first spline teeth; and wherein said component has a opening parallel with said centerline, said plurality of first spline teeth are located on an outer wall defining said opening, said second splined surface is defined on an outer surface of each of the pair of counterweight rings and said pair of counterweight rings are located within said opening. 2. The system of claim 1, wherein each of said pair of counterweight rings is hoop continuous and carries their own centrifugal load at the operating speeds of the rotatable gas turbine engine component. 3. The system of claim 1, wherein each of said pair of counterweight rings is a full substantially circular ring. 4. The system of claim 1, wherein each of said pair of counterweight rings has a known and equal level of imbalance. 5. The system of claim 4, wherein said pair of counterweight rings are substantially identical. 6. The system of claim 1, wherein said counterweight rings are not positioned concentrically and are not mechanically fastened together. 7. The system of claim 1, wherein said mass asymmetric portion is defined by an arc of up to 180째 in circumferential extent. 8. The system of claim 1, wherein each of said pair of counterweight rings requires no in situ change in mass during the balancing of the system. 9. The system of claim 1 wherein each of said pair of counterweight rings is a continuous structure and configured to carry their own centrifugal load at the operating speeds of the rotatable gas turbine engine component; and wherein said pair of counterweight rings are not arranged concentrically and are not mechanically fastened to one another. 10. The system of claim 1, wherein at least one of said pair of counterweight rings having an indicator for said mass asymmetric portion. 11. The system of claim 2, wherein said counterweight rings are not positioned concentrically and are not mechanically fastened together. 12. The system of claim 11, wherein each of said pair of counterweight rings requires no in situ change in mass during the balancing of the system. 13. The system of claim 12, wherein each of said pair of counterweight rings has a known and equal level of imbalance. 14. The system of claim 13, wherein at least one of said pair of counterweight rings having an indicator for said mass asymmetric portion.