Bump check tool for gas turbine rotor

1. A bump check tool for determining an axial clearance between a shim of a thrust bearing and a rotor flange of a rotor shaft within a casing of a gas turbine engine, comprising:

a hydraulic cylinder;

a connection plate attached to the hydraulic cylinder and positioned about the rotor shaft; and

a support frame supporting the hydraulic cylinder and attached to the casing;

wherein the hydraulic cylinder drives the connection plate and the rotor shaft to determine the axial clearance between the shim of the thrust bearing and the rotor flange of the rotor shaft.

2. The bump check tool of claim 1 , wherein the hydraulic cylinder is a double action hydraulic cylinder.

3. The bump check tool of claim 1 , wherein the hydraulic cylinder pushes and pulls the rotor shaft.

4. The bump check tool of claim 1 , wherein the hydraulic cylinder is hand operated.

5. The bump check tool of claim 1 , wherein the hydraulic cylinder drives the connection plate with a piston.

6. The bump check tool of claim 1 , wherein the support frame comprises a plurality of support members.

7. The bump check tool of claim 1 , wherein the support frame is attached to the casing via a plurality of mounting bolts.

8. The bump check tool of claim 7 , wherein the casing comprises bolt holes therein for the plurality of mounting bolts.

9. The bump check tool of claim 1 , wherein the support frame comprises a plurality of load rings thereon.

10. The bump check tool of claim 1 , further comprising a bearing sensor to determine the clearance between the shim and the rotor flange.

11. The bump check tool of claim 1 , wherein the bump check tool is positioned about a forward end of the rotor shaft.

12. The bump check tool of claim 1 , wherein the bump check tool is positioned about an aft end of the rotor shaft.

13. The bump check tool of claim 1 , wherein the bump check tool is attached to the casing with the casing intact.

14. The bump check tool of claim 1 , wherein the bump check tool is detachable from the casing.

15. A method of performing a bump check test on a rotor shaft of a turbine engine, comprising:

attaching a bump check tool to a casing of the turbine engine with the casing intact;

wherein the bump check tool comprises a connection plate and a support frame;

moving the rotor shaft of the turbine engine with a hydraulic cylinder of the bump check tool;

determining an axial clearance between a shim of a thrust bearing and a rotor flange of the rotor shaft; and

removing the bump check tool from the casing.

16. A bump check tool for determining an axial clearance between a shim of a thrust bearing and a rotor flange of a rotor shaft within a casing of a turbine engine, comprising:

a hydraulic cylinder to push and pull the rotor shaft;

a connection plate attached to a piston of the hydraulic cylinder and positioned about the rotor shaft; and

a support frame supporting the hydraulic cylinder and attached to the casing by a plurality of mounting bolts;

wherein the hydraulic cylinder drives the connection plate and the rotor shaft to determine the axial clearance between the shim of the thrust bearing and the rotor flange of the rotor shaft.

17. The bump check tool of claim 16 , wherein the hydraulic cylinder is a double-action hydraulic cylinder.

18. The bump check tool of claim 16 , wherein the support frame comprises a plurality of support members.

19. The bump check tool of claim 16 , wherein the support frame comprises a plurality of load rings thereon.

20. The bump check tool of claim 16 , further comprising a bearing sensor to determine the clearance between the shim and the rotor flange.