Cooling hole with enhanced flow attachment

Patent metadata

Field	Value
Publication number	US-9416665-B2
Application number	US-201213544074-A
Country	US
Kind code	B2
Filing date	Jul 9, 2012
Priority date	Feb 15, 2012
Publication date	Aug 16, 2016
Grant date	Aug 16, 2016

Abstract

A gas turbine engine component includes a wall having first and second wall surfaces, a cooling hole extending through the wall and a convexity. The cooling hole includes an inlet located at the first wall surface, an outlet located at the second wall surface, a metering section extending downstream from the inlet and a diffusing section extending from the metering section to the outlet. The diffusing section includes a first lobe diverging longitudinally and laterally from the metering section and a second lobe adjacent the first lobe and diverging longitudinally and laterally from the metering section. The convexity is located near the outlet.

First claim

The invention claimed is:

1. A gas turbine engine component comprising:
a wall having first and second wall surfaces;
a cooling hole extending through the wall and comprising:
an inlet located at the first wall surface;
an outlet located at the second wall surface;
a metering section extending downstream from the inlet and having a longitudinal axis; and
a diffusing section extending from the metering section to the outlet, the diffusing section comprising:
a first lobe diverging longitudinally and laterally from the metering section; and
a second lobe adjacent the first lobe and diverging longitudinally and laterally from the metering section; and

a convexity located near the outlet, wherein the convexity extends longitudinally from the first lobe to the second lobe and forms a curved surface on the second wall surface generally perpendicular to the longitudinal axis of the metering section such that the convexity is generally perpendicular to a flow direction of cooling air that flows through the cooling hole during use; and an indentation located on the second wall surface downstream from the convexity and downstream from the outlet, wherein the indentation is oriented such that it is one of either C-shaped or reverse C-shaped with respect to air flowing through the cooling hole.

2. The component of claim 1 , wherein the indentation has a lateral width that is greater than or equal to a lateral width of the outlet.

3. The component of claim 1 , wherein the indentation has a lateral width that is between about 100% and about 150% of the lateral width of the convexity.

4. The component of claim 1 , wherein the indentation has a longitudinal length that is substantially equal to a longitudinal length of the convexity.

5. The component of claim 1 , wherein the diffusing section further comprises:
an interlobe region having a portion that extends between the first and second lobes, the interlobe region having an end adjacent the outlet.

6. The component of claim 5 , wherein the interlobe region has a second portion located between the outlet and the first and second lobes.

7. The component of claim 1 , wherein the indentation has a circular arc extending towards the first wall surface.

8. The component of claim 1 , wherein the indentation has an elliptical arc extending towards the first wall surface.

9. The component of claim 1 , wherein a distance between the indentation and the outlet on the second wall surface is larger than a distance between the first and second wall surfaces.

10. The component of claim 1 , wherein the diffusing section comprises a bottom surface, and wherein the convexity is formed along the bottom surface of the diffusing section and the second wall surface.

11. The component of claim 1 , further comprising:
a second convexity.

12. The component of claim 11 , wherein the convexity is located downstream from the first lobe and the second convexity is located downstream from the second lobe.

13. The component of claim 1 , further comprising:
a second indentation located downstream from the indentation.

14. The component of claim 13 , wherein the diffusing section comprises a bottom surface, and wherein the convexity is formed by the bottom surface of the diffusing section and the second wall surface; and the component further comprises:
a second convexity located between the indentation and the second indentation, wherein the second convexity is formed by a downstream portion of the indentation and the second wall surface downstream from the indentation.

15. A wall of a component of a gas turbine engine, the wall comprising:
first and second wall surfaces;
an inlet located at the first wall surface;
an outlet located at the second wall surface;
a metering section commencing at the inlet and extending downstream from the inlet and having a longitudinal axis;
a diffusing section extending from the metering section and terminating at the outlet, the diffusing section comprising:
a first lobe diverging longitudinally and laterally from the metering section; and
a second lobe adjacent the first lobe and diverging longitudinally and laterally from the metering section; and

a convexity located on the second wall surface downstream of the outlet, wherein the convexity extends laterally in a direction generally perpendicular to the longitudinal axis of the metering section such that the convexity is generally perpendicular with respect to a flow direction of air that flows through the cooling hole; and a concavity located downstream from the convexity on the second wall surface and downstream from the outlet, wherein the concavity is oriented such that it is one of either C-shaped or reverse C-shaped with respect to air flowing through the cooling hole.

16. The wall of claim 15 , wherein the diffusing section further comprises:
an interlobe region having a portion that extends between the first and second lobes, the interlobe region having an end adjacent the outlet.

Assignees

• Xu Jinquan
• Levasseur Glenn
• United Technologies Corp

Inventors

• Xu Jinquan
• Levasseur Glenn

Classifications

• F01D5/186 Primary

  Film cooling (F01D5/187 takes precedence) · CPC title

• F01D9/065

  Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids (see also F01D25/16, F01D25/24 and F01D25/26) · CPC title

• F05D2240/81

  Cooled platforms · CPC title

• F05D2260/202

  by film cooling · CPC title

• F23R2900/03042

  Film cooled combustion chamber walls or domes · CPC title