Turbine rotor locking assembly and method
AssigneeRaytheon Technologies Corporation
InventorsJonathan Jeffery Eastwood, Christopher M. Juh
Life of this patent
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Abstract
A power turbine rotor locking assembly including a rotor shaft. The assembly also includes an aft rotor stage surrounding the rotor shaft. The assembly further includes a locknut torqued to the rotor shaft. The assembly yet further includes a plurality of torque resistance features located on an aft side of the aft rotor stage. The assembly also includes a tooling fixture having a plurality of corresponding torque resistance features, the corresponding torque resistance features selectively engageable with the torque resistance features of the aft rotor stage to resist circumferential movement during assembly and disassembly of the locknut with the rotor shaft.
Claims6
A power turbine rotor locking assembly comprising:
- a rotor shaft;
- an aft rotor stage surrounding the rotor shaft;
- a locknut torqued to the rotor shaft;
- a plurality of torque resistance features located on an aft side of the aft rotor stage, the plurality of torque resistance features radially extending from the aft side of the aft rotor stage, each of the plurality of torque resistance features defined as a tab extending from a tab base to a tab distal end, the tab distal end disposed radially inboard of the tab base;
- and
- a tooling fixture having a plurality of corresponding torque resistance features, the corresponding torque resistance features selectively engageable with the plurality of torque resistance features of the aft rotor stage to resist circumferential movement during assembly and disassembly of the locknut with the rotor shaft, the plurality of corresponding torque resistance features axially extending from the tooling fixture.
Dependencies are inferred from the claim text.