Gas turbine component with cooling aperture having shaped inlet and method of forming the same

Patent metadata

Field	Value
Publication number	US-11220918-B2
Application number	US-202017019532-A
Country	US
Kind code	B2
Filing date	Sep 14, 2020
Priority date	Sep 15, 2016
Publication date	Jan 11, 2022
Grant date	Jan 11, 2022

Abstract

A method of manufacturing a cooled gas turbine component includes forming a core with an outer surface. The outer surface includes a core feature. The method also includes casting an outer wall of an airfoil about the core. The outer wall has an exterior surface and an interior surface. The interior surface includes a shaped inlet portion that corresponds to the core feature. Moreover, the method includes forming an outlet portion through the outer wall to fluidly connect the outlet portion to the shaped inlet portion. The shaped inlet portion and the outlet portion cooperatively define a cooling aperture through the outer wall.

First claim

What is claimed is:

1. A method of manufacturing a cooled gas component for a turbomachine, the method comprising:
forming a core with an outer surface, the outer surface including a core feature that tapers to reduce in width as the core feature projects from the core;
casting an outer wall about the core including casting a portion of the outer wall that covers and layers over the core feature, the portion including an exterior surface and an interior surface, the interior surface defining a shaped inlet portion that is cast to taper and inversely correspond to the core feature; and
after casting the outer wall, forming an outlet portion through the outer wall by progressively removing material through the portion of the outer wall in a direction from the exterior surface toward the interior surface and toward the shaped inlet portion to fluidly connect the outlet portion to the shaped inlet portion, the shaped inlet portion and the outlet portion cooperatively defining a cooling aperture through the outer wall.

2. The method of claim 1 , further comprising adjusting the outlet portion by changing a dimension of the outlet portion.

3. The method of claim 1 , further comprising:
re-casting the outer wall; and
forming an adjusted outlet portion through the re-cast outer wall.

4. The method of claim 3 , wherein forming the outlet portion through the outer wall includes forming the outlet portion at a first axis relative to the exterior surface of the outer wall;
wherein forming the adjusted outlet portion through the re-cast outer wall includes forming the adjusted outlet portion at a second axis relative to an exterior surface of the re-cast outer wall; and
wherein the second axis is disposed at an angle relative to the first axis.

5. The method of claim 1 , wherein forming the core includes forming the core feature to be at least partially conic.

6. The method of claim 1 , wherein forming the outlet portion includes extending the outlet portion along an axis;
wherein the axis extends at an acute angle relative to the exterior surface of the outer wall.

7. The method of claim 1 , wherein forming the outlet portion includes forming the outlet portion to have a substantially constant width along a length of the outlet portion.

8. The method of claim 1 , wherein forming the outlet portion includes extending the aperture through the shaped inlet portion, leaving at least part of the shaped inlet portion continuously encompassing the outlet portion.

9. The method of claim 1 , wherein forming the core includes molding the core within a die.

10. The method of claim 1 , wherein forming the core includes forming a recess on the outer surface of the core; and
wherein forming the core includes forming the core feature as a projection that is disposed in the recess.

11. The method of claim 1 , wherein a depth of the shaped inlet portion is, at most, one third of a length of the cooling aperture.

12. The method of claim 1 , wherein the inlet portion comprises a chamfer of the outlet portion.

13. The method of claim 1 , wherein casting the outer wall includes forming the shaped inlet portion to have a convex curvature.

14. A method of manufacturing a cooled gas component for a turbomachine, the method comprising:
forming a core with an outer surface, the outer surface including a core feature that tapers to reduce in width as the core feature projects from the core;
casting an outer wall about the core including casting a portion of the outer wall that covers the core feature, the portion including an exterior surface and an interior surface, the interior surface defining a shaped inlet portion that is cast to inversely correspond to the core feature;
after casting the outer wall, forming an outlet portion through the outer wall by progressively removing material through the portion of the outer wall in a direction from the exterior surface toward the interior surface and toward the shaped inlet portion to fluidly connect the outlet portion to the shaped inlet portion, the shaped inlet portion and the outlet portion cooperatively defining a cooling aperture through the outer wall;
re-casting the outer wall; and
forming an adjusted outlet portion through the re-cast outer wall.

15. The method of claim 14 , wherein forming the outlet portion through the outer wall includes forming the outlet portion at a first axis relative to the exterior surface of the outer wall;
wherein forming the adjusted outlet portion through the re-cast outer wall includes forming the adjusted outlet portion at a second axis relative to an exterior surface of the re-cast outer wall; and
wherein the second axis is disposed at an angle relative to the first axis.

16. The method of claim 14 , further comprising adjusting the outlet portion by changing a dimension of the outlet portion.

17. The method of claim 14 , wherein forming the core includes forming the core feature to be at least partially conic.

18. The method of claim 14 , wherein forming the outlet portion includes extending the outlet portion along an axis; and
wherein the axis extends at an acute angle relative to the exterior surface of the outer wall.

19. The method of claim 14 , wherein forming the outlet portion includes forming the outlet portion to have a substantially constant width along a length of the outlet portion.

20. The method of claim 14 , wherein forming the outlet portion includes extending the aperture through the shaped inlet portion, leaving at least part of the shaped inlet portion continuously encompassing the outlet portion.

Assignees

• Honeywell Int Inc

Inventors

• Howe Jeff
• Tapia Luis

Classifications

• F05D2260/202

  by film cooling · CPC title

• B22C7/02

  Lost patterns · CPC title

• F05D2250/323

  convergent · CPC title

• F05D2230/211

  by precision casting, e.g. microfusing or investment casting · CPC title

• F05D2220/32

  in gas turbines · CPC title