Systems for preventing wear on turbine blade tip shrouds

• US 20080145207A1
• Filed: 12/14/2006
• Published: 06/19/2008
• Est. Priority Date: 12/14/2006
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (General Electric Company)
• Original Assignee: General Electric Company
• Inventors: Williams, David, Fernandez, Emilio, Arnett, Michael, Collado, Carlos, Mohr, Patrick, Nowak, Daniel
• Granted Patent: US 7,771,171 B2
• Time in Patent Office: Days
• US Class Current: 415/173.1
• CPC Class Codes: F01D 5/225 by shrouding
• CPC Class Codes: F05C 2201/0463 Cobalt
• CPC Class Codes: F05D 2300/506 Hardness

Abstract

A system in a turbine engine for preventing wear on a tip shroud of a turbine blade that includes a pocket formed in a contact surface of the tip shroud and a plug that fits within the pocket and has a durable outer surface. The durable outer surface may include a cobalt-based hardfacing powder. The pocket may be machined out of the contact surface, and the plug may include a plug of predetermined size that fits snugly into the pocket. In some embodiments, the durable outer surface may substantially align with the contact surface after the plug is fitted into the pocket. In other embodiments, the durable outer surface may remain slightly raised from the contact surface after the plug has been fitted into the pocket.

Claims

1. A system in a turbine engine for preventing wear on a tip shroud of a turbine blade, the system comprising:

a pocket formed in a contact surface of the tip shroud;

a plug that fits within the pocket and has a durable outer surface.

2. The system of claim 1, wherein the durable outer surface comprises a cobalt-based hardfacing powder.

3. The system of claim 1, wherein the pocket is machined out of the contact surface and the plug comprises a plug of predetermined size that fits snugly into the pocket.

4. The system of claim 1, wherein the durable outer surface substantially aligns with the contact surface after the plug is fitted into the pocket.

5. The system of claim 1, wherein the durable outer surface remains slightly raised from the contact surface after the plug has been fitted into the pocket.

6. The system of claim 1, wherein the tip shroud comes into contact with an adjacent tip shroud during the operation of the turbine at the contact surface.

7. The system of claim 6, wherein the contact surface comprises a Z-interface, the Z-interface having an approximate profile of a “

Z”

.

8. The system of claim 7, wherein the tip shroud further comprises a cutting tooth that forms a ridge down the middle of a top surface of the tip shroud;

and

the Z-interface includes a middle contact face that corresponds to a middle leg of the approximate “

Z”

profile, the middle contact face having a substantially rectangular shape that substantially corresponds to a cross-sectional shape of the cutting tooth.

9. The system of claim 8, wherein the height of the pocket comprises the approximate thickness of the tip shroud at either the upper contact face or the lower contact face.

10. The system of claim 3, wherein the pocket is open through a lower interior face.

11. The system of claim 1, wherein the plug is brazed into the pocket.

12. The system of claim 6, wherein the durable outer surface of the plug opposes a second durable outer surface of a second plug of the adjacent tip shroud.

13. A system in a turbine engine for preventing wear on a tip shroud of a turbine blade, the system comprising a plate attached to a contact surface of the tip shroud, wherein the plate includes a durable outer surface.

14. The system of claim 13, wherein the durable outer surface comprises a cobalt-based hardfacing powder.

15. The system of claim 13, wherein the tip shroud comes into contact with an adjacent tip shroud during the operation of the turbine at the contact surface;

and

the contact surface comprises a Z-interface, the Z-interface having an approximate profile of a “

Z”

.

16. The system of claim 15, wherein the tip shroud further comprises a cutting tooth that forms a ridge down the middle of a top surface of the tip shroud;

and

the Z-interface includes a middle contact face that corresponds to a middle leg of the approximate “

Z”

profile, the middle contact face having;

a substantially rectangular shape that corresponds to the approximate cross-sectional shape of the cutting tooth.

17. The system of claim 16, wherein the plate is substantially rectangular and covers approximately all of the middle contact surface.

18. The system of claim 13, further comprising a dowel opening in the plate and the contact face for the insertion of a dowel.

19. The system of claim 15, wherein the durable outer surface of the plate opposes a second durable outer surface of a second plate of the adjacent tip shroud.

20. The system of claim 13, wherein the plate includes a lip that, upon installation of the plate against the contact surface, engages an edge of the contact surface.