Components with re-entrant shaped cooling channels and methods of manufacture

Patent metadata

Field	Value
Publication number	US-9249491-B2
Application number	US-201213669922-A
Country	US
Kind code	B2
Filing date	Nov 6, 2012
Priority date	Nov 10, 2010
Publication date	Feb 2, 2016
Grant date	Feb 2, 2016

Abstract

A method of fabricating a component is provided. The component includes a substrate that has at least one interior space. The method includes forming one or more grooves in the component. Each groove extends at least partially along an outer surface of the substrate and narrows at an opening thereof, such that each groove is re-entrant shaped. A cross-sectional area A of each groove is in a range of about 2 to about 3 times an area R=W*D, where W is the width of the opening and D is the depth of the re-entrant-shaped groove. Components with grooves formed in the substrate and components with grooves formed at least partially in a structural coating are also provided.

First claim

The invention claimed is:

1. A method of fabricating a component comprising a substrate that has at least one interior space, the method comprising forming one or more grooves in the component,
wherein each groove has a base and extends at least partially along an outer surface of the substrate and narrows at an opening thereof, such that each groove comprises a re-entrant shaped groove,
wherein the base of a respective groove is rounded to define an overall teardrop shaped groove, and
wherein a cross-sectional area A of each groove is in a range of about 2 to about 3 times an area R=W*D, where W is a width of the opening of the re-entrant-shaped groove, and D is a depth of the re-entrant-shaped groove.

2. The method of claim 1 , wherein each groove is symmetric about the centerline.

3. The method of claim 1 , wherein each groove has an asymmetric cross-section.

4. The method of claim 1 , further comprising forming one or more access holes in the substrate, wherein each access hole connects one of the groove(s) in fluid communication with the respective interior space.

5. The method of claim 1 , wherein the grooves are formed in the outer surface of the substrate.

6. The method of claim 1 , further comprising disposing a coating over at least a portion of the surface of the substrate, wherein the groove(s) and the coating together define one or more re-entrant shaped channels for cooling the component.

7. The method of claim 6 , wherein a fill ratio for the coating deposited in each groove is less than twenty percent.

8. The method of claim 7 , wherein the fill ratio for the coating deposited in each groove is less than ten percent.

9. The method of claim 6 , wherein the coating comprises at least a structural coating and an addition coating, and wherein each groove is at least partially formed in the structural coating.

10. A component comprising:
a substrate having an outer surface and an inner surface, wherein the inner surface defines at least one interior space, wherein the outer surface defines one or more grooves, wherein each groove has a base and extends at least partially along the surface of the substrate and narrows at an opening thereof, such that each groove comprises a re-entrant shaped groove, wherein the base of a respective groove is rounded to define an overall teardrop shaped groove and wherein a cross-sectional area A of each groove is in a range of about 2 to about 3 times an area R=W*D, where W is a width of the opening of the re-entrant-shaped groove, and D is a depth of the re-entrant-shaped groove; and
at least one coating disposed over at least a portion of the outer surface of the substrate, wherein the groove(s) and the coating together define one or more re-entrant shaped channels for cooling the component.

11. The component of claim 10 , wherein each groove is symmetric about the centerline.

12. The component of claim 10 , wherein each groove has an asymmetric cross-section.

13. The component of claim 10 , wherein one or more access holes are formed in the substrate, and wherein each access hole connects the respective groove in fluid communication with the respective interior space.

14. The component of claim 10 , wherein a fill ratio for the coating deposited in each groove is less than twenty percent.

15. The method of claim 14 , wherein the coating is disposed by performing a thermal spray process.

16. The component of claim 14 , wherein the fill ratio for the coating deposited in each groove is less than ten percent.

17. A component comprising:
a substrate having an outer surface and an inner surface, wherein the inner surface defines at least one interior space; and
at least one coating disposed over at least a portion of the surface of the substrate, wherein the coating comprises at least an inner layer of a structural coating disposed on the outer surface of the substrate and an additional coating,
wherein one or more grooves are formed at least partially in the structural coating, wherein each groove has a base and extends at least partially along the surface of the substrate and narrows at an opening thereof, such that each groove comprises a re-entrant shaped groove,
wherein the base of a respective groove is rounded to define an overall teardrop shaped groove,
wherein a cross-sectional area A of each groove is in a range of about 2 to about 3 times an area R=W*D, where W is a width of the opening of the re-entrant-shaped groove and D is a depth of the re-entrant-shaped groove, and
wherein the groove(s) and the additional coating together define one or more re-entrant shaped channels for cooling the component.

18. The component of claim 17 , wherein each groove is symmetric about the centerline.

19. The component of claim 17 , wherein each groove has an asymmetric cross-section.

20. The component of claim 17 , wherein one or more access holes are formed in the substrate, and wherein each access hole connects the respective groove in fluid communication with the respective interior space.

21. The component of claim 17 , wherein a fill ratio for the coating deposited in each groove is less than twenty percent.

22. The component of claim 21 , wherein the fill ratio for the coating deposited in each groove is less than ten percent.

Assignees

• Gen Electric

Inventors

• Bunker Ronald Scott
• Gray Dennis Michael

Classifications

• C23C24/04

  Impact or kinetic deposition of particles · CPC title

• B23P15/04

  turbine or like blades from several pieces · CPC title

• Y02T50/67

  Cross-Sectional Technologies · mapped topic

• B23P2700/13

  Parts of turbine combustion chambers · CPC title

• Y02T50/672

  Cross-Sectional Technologies · mapped topic