Turbine blades having damper pin slot features and methods of fabricating the same

Patent metadata

Field	Value
Publication number	US-10519785-B2
Application number	US-201715431950-A
Country	US
Kind code	B2
Filing date	Feb 14, 2017
Priority date	Feb 14, 2017
Publication date	Dec 31, 2019
Grant date	Dec 31, 2019

Abstract

A turbine blade includes an airfoil that extends radially between a root end and a tip end, a platform coupled to the root end, and a shank that extends radially inwardly from the platform. The shank includes a cover plate. The cover plate includes an outer surface, an opposite inner surface, and a contoured face that at least partially defines a damper pin slot. The contoured face extends from the outer surface to a first blend edge. The cover plate also includes a blended surface that extends from the first blend edge to a second blend edge. The second blend edge intersects with the inner surface.

First claim

What is claimed is:

1. A method of forming a damper pin slot for a turbine blade, the turbine blade including a platform and a shank that extends radially inward from the platform, wherein the shank includes a cover plate, said method comprising:
providing the cover plate having an outer surface, an opposite inner surface, a thickness defined between the outer surface and the inner surface adjacent to the platform, and a contoured face extending from the outer surface to the inner surface, the contoured face intersecting the inner surface along each of a first edge and a second edge, wherein the second edge extends as a continuation of the first edge; and
modifying the second edge such that a blended surface is formed between the contoured face and the inner surface, the blended surface having a blend width in a range of from 40 percent to 60 percent of the cover plate thickness, wherein the contoured face having the modified second edge at least partially defines the damper pin slot.

2. The method according to claim 1 , wherein said modifying the second edge comprises machining the second edge.

3. The method according to claim 1 , wherein said modifying the second edge comprises:
forming a first blend edge between the contoured face and the blended surface; and
forming a second blend edge between the blended surface and the inner surface.

4. The method according to claim 3 , further comprising smoothing at least one of the first blend edge and the second blend edge.

5. The method according to claim 1 , wherein said modifying the second edge comprises forming the blended surface having a concave shape.

6. The method according to claim 5 , wherein said forming the blended surface having the concave shape comprises forming the blended surface having a radius of curvature in a range of from 0.030 inches to 0.060 inches.

7. The method according to claim 1 , wherein said modifying the second edge comprises modifying the second edge such that the first edge merges into the blended surface.

8. The method according to claim 1 , wherein said providing the cover plate comprises providing a downstream cover plate.

9. The method according to claim 1 , wherein said providing the cover plate comprises providing an upstream cover plate.

10. A method of forming a damper pin slot for a turbine blade, the turbine blade including a platform and a shank that extends radially inward from the platform, wherein the shank includes a cover plate, said method comprising:
providing the cover plate having an outer surface, an opposite inner surface, a thickness defined between the outer surface and the inner surface adjacent to the platform, and a contoured face extending from the outer surface to the inner surface, the contoured face intersecting the inner surface along each of a first edge and a second edge, wherein the second edge extends as a continuation of the first edge; and
modifying the second edge such that a blended surface is formed between the contoured face and the inner surface, the blended surface having a blend width of about 50 percent of the cover plate thickness, wherein the contoured face having the modified second edge at least partially defines the damper pin slot.

11. The method according to claim 10 , wherein said modifying the second edge comprises machining the second edge.

12. The method according to claim 10 , wherein said modifying the second edge comprises:
forming a first blend edge between the contoured face and the blended surface; and
forming a second blend edge between the blended surface and the inner surface.

13. The method according to claim 10 , further comprising smoothing at least one of the first blend edge and the second blend edge.

14. The method according to claim 10 , wherein said modifying the second edge comprises forming the blended surface having a concave shape.

15. The method according to claim 14 , wherein said forming the blended surface having the concave shape comprises forming the blended surface having a radius of curvature in a range of from 0.030 inches to 0.060 inches.

16. The method according to claim 10 , wherein said modifying the second edge comprises modifying the second edge such that the first edge merges into the blended surface.

17. The method according to claim 10 , wherein said providing the cover plate comprises providing a downstream cover plate.

18. The method according to claim 10 , wherein said providing the cover plate comprises providing an upstream cover plate.

Assignees

• Gen Electric

Inventors

• Zemitis William Scott
• Myers Melbourne James
• Pilson Richard Ryan
• Sims Calvin Levy

Classifications

• F01D25/06

  for preventing blade vibration (means on blade-carrying members or blades F01D5/00) · CPC title

• F01D5/143

  Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour · CPC title

• F05D2240/80

  Platforms for stationary or moving blades · CPC title

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F01D5/24 Primary

  using wire or the like · CPC title