Granted Patent B2

US 12,312,975 · App. 18/536,428 · Granted May 27, 2025

Inventors: Anquan Wang (Mason, OH); Ryan Christopher Jones (Cincinnati, OH); Paul Christopher Schilling (Waynesville, OH); Craig Alan Gonyou (Blanchester, OH)

Assignee: General Electric Company

F01D5/186

Abstract

Claims (31)

1. A component for a turbine engine which generates a hot gas fluid flow, and provides a cooling fluid flow, comprising:

a wall separating the hot gas fluid flow from the cooling fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow; and

at least one cooling hole including a connecting passage extending from a first inlet located at the cooled surface, to a first outlet located at the heated surface, the connecting passage defining a downstream flow direction from the first inlet to the first outlet, the connecting passage comprising a metering section fluidly coupled to the first inlet and defining a metered centerline and a diffusing section, downstream of the metering section, defining a diffused centerline, and fluidly coupling the metering section to the first outlet;

wherein the diffusing section terminates in a hood defined at least in part by the wall and covering at least a portion of the diffusing section upstream of the first outlet;

wherein the metered centerline forms an entrance angle with the heated surface;

wherein the diffused centerline forms an exit angle with the heated surface that is less than the entrance angle; and

wherein the at least one cooling hole is a set of cooling holes including a first cooling hole and a second cooling hole located downstream from the first cooling hole relative to a direction of the hot gas fluid flow, the second cooling hole comprising a second inlet located at the cooled surface beneath the first outlet and a second outlet located at the heated surface, where the first outlet and the second outlet each define a modified outlet shape.

2. The component of claim 1 , wherein the diffused centerline is curvilinear and transitions between an orientation with the entrance angle to an orientation with the exit angle.

3. The component of claim 1 , wherein the at least one cooling hole further comprises a step down feature formed as a turn.

4. The component of claim 3 , wherein a transition from the entrance angle to the exit angle comprises an abrupt change defined by the turn.

5. The component of claim 4 , wherein the hood covers the turn.

6. The component of claim 5 , wherein the entrance angle ranges from 20 to 40 degrees.

7. The component of claim 6 , wherein the exit angle is less than 20 degrees.

8. The component of claim 1 , wherein the modified outlet shape comprises at least one expansion section having an increasing width.

9. The component of claim 8 , wherein the modified outlet shape comprises a contraction section downstream of the at least one expansion section and having a decreasing width.

10. The component of claim 9 , wherein the modified outlet shape comprises a constant section upstream of the contraction section.

11. The component of claim 10 , wherein the entrance angle ranges from 20 to 40 degrees.

12. The component of claim 11 , wherein the exit angle is less than 20 degrees.

13. A component for a turbine engine which generates a hot gas fluid flow, and provides a cooling fluid flow, comprising:

a wall separating the hot gas fluid flow from the cooling fluid flow and having a heated surface along which the hot gas fluid flow flows and a cooled surface facing the cooling fluid flow; and

at least one cooling hole including a connecting passage extending from a first inlet located at the cooled surface, to a first outlet located at the heated surface, the connecting passage defining a downstream flow direction from the first inlet to the first outlet, the connecting passage comprising a metering section fluidly coupled to the first inlet and defining a metered centerline and a diffusing section, downstream of the metering section, defining a diffused centerline, and fluidly coupling the metering section to the first outlet;

wherein the diffusing section terminates in a hood defined at least in part by the wall and covering at least a portion of the diffusing section upstream of the first outlet;

wherein the metered centerline forms an entrance angle with the heated surface;

wherein the diffused centerline forms an exit angle with the heated surface that is less than the entrance angle; and

wherein the at least one cooling hole comprises a first pair of cooling holes and a second pair of cooling holes located downstream from the first pair of cooling holes relative to a direction of the hot gas fluid flow.

14. The component of claim 13 , wherein each cooling hole in the first pair of cooling holes comprises a first inlet located at the cooled surface and a first outlet located at the heated surface, the first outlet comprising a modified outlet shape including a constant section, and wherein each cooling hole in the second pair of cooling holes comprises a second inlet located at the cooled surface beneath the first outlet and a second outlet located at the heated surface, the second outlet comprising the modified outlet shape.

15. The component of claim 14 , wherein the modified outlet shape comprises at least one expansion section having an increasing width.

16. The component of claim 15 , wherein the modified outlet shape comprises a contraction section downstream of the at least one expansion section and having a decreasing width.

17. The component of claim 16 , wherein the constant section is upstream of the contraction section.

18. The component of claim 17 , wherein the constant section enables tight spacing of the first and second pair of cooling holes with respect to each other.

19. The component of claim 18 , wherein the first and second pair of cooling holes together form a patterned layout.

Assignments (1)

Continuity (3)

References Cited (35)