HGP component with effusion cooling element having coolant swirling chamber

1. A combustion cap for a combustor, comprising:

a body including a hot gas path (HGP) surface exposed to a hot gas path; and

effusion cooling elements in the body, the effusion cooling elements including:

a plurality of coolant swirling chambers embedded within the body,

a coolant delivery passage in the body configured to deliver a coolant to each of the plurality of coolant swirling chambers,

the coolant delivery passage including a plurality of sequentially coupled arcuate segments, each of the sequentially coupled arcuate segments circumventing a respective one of a plurality of fuel nozzles extending through the body,

wherein each of the plurality of coolant swirling chambers imparts a centrifugal force to the coolant, and

a plurality of effusion openings in the HGP surface, each of the plurality of effusion openings in fluid communication with a respective one of the plurality of coolant swirling chambers, and

each of the plurality of effusion openings having a smaller width than the respective one of the plurality of coolant swirling chambers.

2. The combustion cap of claim 1 , wherein the coolant delivery passage is in fluid communication with a source of coolant, wherein the source transmits the coolant to the coolant delivery passage.

3. The combustion cap of claim 1 , wherein the body includes a cap assembly plate of the combustor having the plurality of fuel nozzles extending therethrough, and the plurality of effusion openings are interposed between the plurality of fuel nozzles.

4. The combustion cap of claim 1 , wherein the coolant exits the plurality of effusion openings over substantially all of 360° about each of the plurality of effusion openings, creating a coolant film on the HGP surface.

5. The combustion cap of claim 1 , wherein each of the plurality of effusion openings includes a rounded mating surface with the HGP surface.

6. The combustion cap of claim 1 , wherein each of the plurality of coolant swirling chambers has a rounded cross-section, and wherein the coolant delivery passage in the body delivers the coolant to an interior of each of the plurality of coolant swirling chambers at a tangent to the rounded cross-section of each of the plurality of coolant swirling chambers such that the coolant swirls around the interior prior to exiting the respective one of the plurality of effusion openings.

7. The combustion cap of claim 1 , wherein the body includes a first member including the coolant delivery passage and the plurality of coolant swirling chambers, and a second member for mating coupling to the first member, the second member including the plurality of effusion openings and the HGP surface.

8. The combustion cap of claim 7 , wherein the first member includes a metal and the second member includes a ceramic pre-sintered preform (PSP) plate.

9. The combustion cap of claim 1 , wherein the body and the effusion cooling elements are additively manufactured as a unitary part.

10. The combustion cap of claim 1 , wherein each of the plurality of coolant swirling chambers has a substantially circular cross-section, and the coolant delivery passage delivers the coolant to each of the plurality of coolant swirling chambers at a first circumferential location of each of the plurality of coolant swirling chambers.

11. The combustion cap of claim 1 , wherein the HGP surface faces in a flow direction of the hot gas path.

12. The combustion cap of claim 1 , wherein at least one of the plurality of coolant swirling chambers is substantially equidistant from a selected group of the plurality of fuel nozzles on the HGP surface.

13. The combustion cap of claim 1 , wherein the coolant delivery passage is fluidly isolated from at least one other coolant delivery passage in the body.

14. The combustion cap of claim 1 , wherein each of the plurality of effusion openings extends perpendicularly with respect to an orientation of the coolant delivery passage within the body.

15. A gas turbine (GT) system, comprising:

a compressor;

a combustion section including a plurality of combustors for creating a flow of hot gasses that travels along a hot gas path,

each combustor of the plurality of combustors including a combustion cap,

each combustion cap including a body having a hot gas path (HGP) surface exposed to the hot gas path;

a turbine section downstream of the combustion section, the turbine section receiving the flow of hot gasses; and

each body of each combustion cap comprising effusion cooling elements, the effusion cooling elements of each body including:

a plurality of coolant swirling chambers embedded within the body,

a coolant delivery passage in the body configured to deliver a coolant to each of the plurality of coolant swirling chambers,

the coolant delivery passage including a plurality of sequentially coupled arcuate segments,

each of the plurality of sequentially coupled arcuate segments circumventing a respective one of a plurality of fuel nozzles extending through the body;

wherein the coolant delivery passages of each body is in fluid communication with a source of coolant that transmits the coolant to each of the coolant delivery passages,

wherein each of the plurality of coolant swirling chambers imparts a centrifugal force to the coolant,

wherein a plurality of effusion openings are formed in the HGP surface of each body, each of the plurality of effusion openings in fluid communication with a respective one of the plurality of coolant swirling chambers, and each of the plurality of effusion openings having a smaller width than the respective one of the plurality of coolant swirling chambers, and

wherein the coolant exits the plurality of effusion openings over substantially all of 360° about each of the plurality of effusion openings, creating a coolant film on the HGP surface.

16. The GT system of claim 15 , wherein each body includes a first metal member including the coolant delivery passage of the body and the plurality of coolant swirling chambers of the body, and a second ceramic pre-sintered preform (PSP) plate member for mating coupling to the first metal member, the second ceramic PSP plate member including the plurality of effusion openings of the body and the HGP surface of the body.

17. The GT system of claim 15 , wherein each body and the effusion cooling elements of the body are additively manufactured as a unitary part.

18. The GT system of claim 15 , wherein the HGP surface of each body faces in a flow direction of the hot gas path.