Component with cooling passage for a turbine engine

Patent metadata

Field	Value
Publication number	US-11560803-B1
Application number	US-202117520146-A
Country	US
Kind code	B1
Filing date	Nov 5, 2021
Priority date	Nov 5, 2021
Publication date	Jan 24, 2023
Grant date	Jan 24, 2023

Abstract

An engine component for a turbine engine having a working airflow separated into a cooling airflow and a combustion airflow, the engine component comprising a wall defining an interior and having an outer surface over which flows the combustion airflow, the outer surface defining a first side and a second side. The engine component further comprising at least one cooling conduit provided in the interior and having conduit sidewalls and a set of cooling passages formed in the wall and fluidly coupling the at least one cooling conduit to the outer surface, at least one of the cooling passages in the set comprising a primary cooling passage portion and a secondary cooling passage portion. A diffusion slot located in the primary cooling passage portion and an impingement zone fluidly coupled to the diffusion slot.

First claim

What is claimed is:

1. An engine component for a turbine engine having a working airflow separated into a cooling airflow and a combustion airflow, the engine component comprising:
a wall defining an interior and having an outer surface over which flows the combustion airflow, the outer surface defining a first side and a second side and having an edge,
at least one cooling conduit provided in the interior and having conduit sidewalls;
a set of cooling passages formed in the wall and fluidly coupling the at least one cooling conduit to the outer surface, at least one of the cooling passages in the set comprising:
a primary cooling passage portion extending between an intermediate outlet and a passage outlet opening onto the outer surface proximate the edge;
a secondary cooling passage portion extending between an inlet fluidly connected to the at least one cooling conduit and the intermediate outlet, the primary and secondary cooling passage portions together defining the at least one cooling passage extending along a flow direction between the inlet and the passage outlet;
a diffusion slot located in the primary cooling passage portion and extending along the flow direction between a rear wall and the passage outlet, the diffusion slot having slot sidewalls defining a slot first centerline,
an impingement zone fluidly coupled to the diffusion slot proximate the rear wall, having an impingement surface, and fluidly connected to the secondary cooling passage portion at a junction proximate the rear wall and opposite the impingement surface.

2. The engine component of claim 1 wherein at least one of the primary or secondary cooling passage portions are curved.

3. The engine component of claim 1 wherein the secondary cooling passage portion is a curved passage.

4. The engine component of claim 3 wherein the diffusion slot is a curved diffusion slot and the curved diffusion slot and the curved passage are curved in opposite directions.

5. The engine component of claim 1 wherein the primary cooling passage portion is curved and includes an inflection point.

6. The engine component of claim 1 wherein the outer surface extends between an upstream edge and a downstream edge and between a root and a tip to define a span-wise direction.

7. The engine component of claim 6 wherein the set of cooling passages are located on the upstream edge.

8. The engine component of claim 7 wherein the flow direction extends in the span-wise direction along at least a portion of at least one of the cooling passages.

9. The engine component of claim 6 wherein the set of cooling passages is multiple cooling passages flanking the edge, extending in the span-wise direction, and located proximate to or at the upstream edge.

10. The engine component of claim 9 wherein the multiple cooling passages include a first side set of cooling passages and a second side set of cooling passages flanking the edge.

11. The engine component of claim 6 further comprising an outlet slot extending along the outer surface in the span-wise direction and the diffusion slot opens into the outlet slot.

12. The engine component of claim 1 further comprising at least one stagnation passage extending between a stagnation inlet fluidly connected to the at least one cooling conduit and a stagnation outlet located along the edge.

13. The engine component of claim 1 wherein the intermediate outlet is spaced from the rear wall to define a pocket.

14. The engine component of claim 1 wherein the at least one cooling passage is a pair of sequential cooling passages spaced from each other a first linear distance between sequential centers of the cooling passages at the passage outlet and a second linear distance is a closest distance between sequential centers of the cooling passages where a ratio between the first linear distance and the second linear distance is equal to or between 1 and 6.

15. A method of cooling the engine component of claim 1 , the method comprising:
flowing a cooling fluid into the interior of the engine component;
turning the cooling fluid from a first direction to a second direction different than the first direction through a curved passage;
impinging the cooling fluid on the impingement surface located in the diffusion slot in the outer wall;
diffusing the cooling fluid to an exterior of the engine component through the diffusion slot; and
exhausting the cooling fluid at the passage outlet.

16. The method of claim 15 further comprising exhausting the cooling fluid from the diffusion slot through the passage outlet opening onto an outer surface of the outer wall in a third direction different than the first or second directions.

17. The method of claim 15 further comprising exhausting the cooling fluid from the diffusion slot through the passage outlet opening onto an outer surface of the outer wall in the first direction.

18. The method of claim 15 further comprising expanding the cooling fluid in a span-wise direction.

19. The method of claim 15 further comprising passing the cooling fluid through a stagnation passage extending between the interior and an outer surface of the outer wall.

20. The method of claim 19 further comprising exhausting the cooling fluid at a stagnation outlet at the edge.

Assignees

• Gen Electric

Inventors

• Osgood Daniel Endecott
• Gallier Kirk Douglas
• Webster Zachary Daniel
• Garay Gregory Terrence
• Durstock Daniel Lee
• Caraballo Ricardo

Classifications

• F05D2260/202

  by film cooling · CPC title

• F01D5/187 Primary

  Convection cooling · CPC title

• F05D2260/232

  characterized by the cooling medium · CPC title

• F05D2260/201

  by impingement of a fluid · CPC title

• F01D5/085

  cooling fluid circulating inside the rotor · CPC title