Airfoils with low-angle holes and methods for drilling same

Patent metadata

Field	Value
Publication number	US-10316672-B2
Application number	US-201314038076-A
Country	US
Kind code	B2
Filing date	Sep 26, 2013
Priority date	Sep 26, 2013
Publication date	Jun 11, 2019
Grant date	Jun 11, 2019

Abstract

A method for fabricating an airfoil includes forming a diffuser section in an exterior surface of the airfoil. The diffuser section is defined by at least an outer surface and an inner surface that converge at a stop surface. The method also includes positioning a drilling element of a drilling device on the stop surface. The method further includes orienting the drilling element at a first angle relative to the exterior surface. The method also includes forming, using the drilling element, a cooling channel extending through the airfoil from the stop surface to an interior surface, thereby forming the cooling channel at substantially the first angle.

First claim

What is claimed is:

1. A method for fabricating an airfoil, said method comprising:
forming a diffuser section in an exterior surface of the airfoil, wherein the diffuser section is defined by at least an outer surface and an inner surface that converge at a stop surface;
forming a flow inlet section in an interior surface of the airfoil opposite to the exterior surface, the flow inlet section being offset a horizontal distance from the diffuser section and oriented at a first angle relative to the exterior surface;
positioning a drilling element of a drilling device on the stop surface;
orienting the drilling element at the first angle relative to the exterior surface; and
forming, using the drilling element, a channel extending through the airfoil from the stop surface to a drill discharge surface of the flow inlet section at an interior end of the channel proximate the flow inlet section in the interior surface, thereby forming the channel at substantially the first angle.

2. The method of claim 1 , wherein said positioning the drilling element comprises positioning the drilling element such that the stop surface facilitates maintaining a position of the drilling element at the stop surface during said forming of the channel.

3. The method of claim 1 , wherein said forming the diffuser section comprises forming the diffuser section with the outer surface having a second angle, relative to the exterior surface, that is larger than the first angle and that is less than about 90°.

4. The method of claim 1 , wherein said forming the diffuser section comprises forming the diffuser section with the inner surface having a third angle, relative to the exterior surface, that is less than the first angle.

5. The method of claim 1 , wherein said orienting the drilling element comprises orienting the drilling element at the first angle of between about 5° and about 25° relative to the exterior surface.

6. The method of claim 5 , wherein said orienting the drilling element comprises orienting the drilling element at the first angle of between about 10° and about 15° relative to the exterior surface.

7. The method of claim 1 , wherein said forming the diffuser section comprises forming the diffuser section including the stop surface that is substantially perpendicular to the first angle.

8. The method of claim 1 , wherein said forming the channel comprises forming the channel using one of electric discharge machining and a water jet process.

9. A method for fabricating an airfoil, said method comprising:
forming a diffuser section in an exterior surface of the airfoil, wherein the diffuser section is defined by at least an outer surface and an inner surface that converge at a stop surface;
forming a flow inlet section in an interior surface of the airfoil opposite the exterior surface, the flow inlet section being offset a horizontal distance from the diffuser section and oriented at a first angle relative to the exterior surface;
positioning a drilling element of a drilling device on the stop surface;
orienting the drilling element at the first angle relative to the exterior surface; and
forming, using the drilling element and after said forming the flow inlet section, a channel extending through the airfoil from the stop surface to the flow inlet section.

10. The method of claim 9 , wherein said forming the diffuser section comprises forming the diffuser section with the outer surface having a second angle, relative to the exterior surface, that is larger than the first angle and that is less than about 90°.

11. The method of claim 9 , wherein said forming the diffuser section comprises forming the diffuser section with the inner surface having a third angle, relative to the exterior surface, that is less than the first angle.

12. The method of claim 9 , wherein said orienting the drilling element comprises orienting the drilling element at the first angle of between about 5° and about 25° relative to the exterior surface.

13. The method of claim 12 , wherein said orienting the drilling element comprises orienting the drilling element at the first angle of between about 10° and about 15° relative to the exterior surface.

14. The method of claim 9 , wherein said forming the diffuser section comprises forming the diffuser section including the stop surface that is substantially perpendicular to said first angle.

15. An airfoil comprising:
a diffuser section formed in an exterior surface of the airfoil, wherein the diffuser section is defined by at least an upper surface and a lower surface, wherein the upper and lower surfaces extend from the exterior surface to a flow discharge plane, and wherein the upper and lower surfaces converge towards the flow discharge plane;
a flow inlet section formed in an interior surface of the airfoil opposite the exterior surface, the flow inlet section being offset a horizontal distance from the diffuser section and defining a curved surface; and
a channel extending through the airfoil along a channel axis and coupled in flow communication between the flow inlet section and the diffuser section, wherein the channel axis is oriented at an oblique first angle with respect to the exterior surface and the interior surface and is approximately perpendicular to the flow discharge plane, wherein the channel intersects the diffuser section at the flow discharge plane and intersects the curved surface at a flow inlet plane, and wherein the flow inlet plane is spaced from the flow discharge place along the channel axis and is approximately perpendicular to the channel axis.

16. The airfoil of claim 15 , wherein the channel is oriented at substantially the first angle, relative to the exterior surface, that is less than 30°.

17. The airfoil of claim 15 , wherein the channel is oriented at substantially the first angle of between about 5° and about 25° relative to the exterior surface.

18. The airfoil of claim 15 , wherein the channel is oriented at substantially the first angle of between about 10° and about 15° relative to the exterior surface.

Assignees

• Gen Electric

Inventors

• Smith Aaron Ezekiel
• Harris Jr John Wesley

Classifications

• F01D5/141

  Shape, i.e. outer, aerodynamic form (F01D5/148 - F01D5/20 take precedence; blade construction F01D5/147) · CPC title

• Y02T50/676

  Cross-Sectional Technologies · mapped topic

• F05D2230/12

  by spark erosion methods · CPC title

• F05D2230/10

  by removing material · CPC title

• B26F1/26

  Perforating by non-mechanical means, e.g. by fluid jet · CPC title