Volute trapped vortex combustor assembly

1. A combustor assembly defining a lengthwise direction, a radial direction, and a circumferential direction, the combustor assembly comprising:

a volute wall extended annularly around a combustor centerline, wherein the volute wall is extended at least partially as a spiral curve from a circumferential reference line around the combustor centerline, and wherein the volute wall defines a combustion chamber therewithin;

an annular inner wall extended at least partially along the lengthwise direction from the volute wall; and

an annular outer wall extended at least partially along the lengthwise direction from the volute wall,

wherein the annular inner wall and the annular outer wall are separated along the radial direction from the combustor centerline,

wherein a primary flow passage is defined between the annular inner wall and the annular outer wall in fluid communication with the combustion chamber,

wherein the volute wall defines a primary opening having a primary fuel injector extending therethrough,

wherein a portion of the volute wall and a portion of the annular outer wall together define a secondary flow passage in fluid communication with one or more secondary openings,

wherein a secondary fuel injector is extended at least partially through the secondary flow passage,

wherein the annular outer wall defines a tertiary opening therethrough adjacent to the primary flow passage, and

wherein a tertiary fuel injector is extended at least partially through the tertiary opening at the annular outer wall.

2. A combustor assembly defining a lengthwise direction, a radial direction, and a circumferential direction, the combustor assembly comprising:

a volute wall extended annularly around a combustor centerline, wherein the volute wall is extended at least partially as a spiral curve from a circumferential reference line around the combustor centerline, and wherein the volute wall defines a combustion chamber therewithin;

an annular inner wall extended at least partially along the lengthwise direction from the volute wall;

an annular outer wall extended at least partially along the lengthwise direction from the volute wall; and

a primary fuel injector,

wherein the annular inner wall and the annular outer wall are separated along the radial direction from the combustor centerline,

wherein a primary flow passage is defined between the annular inner wall and the annular outer wall in fluid communication with the combustion chamber,

wherein the volute wall defines a primary opening through which the primary fuel injector is extended at least partially into the combustion chamber,

wherein a reference chord is defined from the volute wall within a plane perpendicular to the circumferential direction and parallel to the longitudinal direction,

wherein the primary fuel injector Is extended at least partially into the combustion chamber at an acute angle relative to the reference chord,

wherein the volute wall and the annular outer wall together define a secondary flow passage, and

wherein a secondary fuel injector is extended at least partially through the secondary flow passage.

3. The combustor assembly of claim 1 , wherein the primary fuel injector is extended at least partially into the combustion chamber at a tangent angle relative to the volute wall and the combustor centerline.

4. The combustor assembly of claim 1 , wherein the one or more secondary openings are adjacent to the combustion chamber and in fluid communication therewith.

5. The combustor assembly of claim 4 , wherein the annular outer wall defines one or more inlet openings in fluid communication with the secondary flow passage and the one or more secondary openings.

6. The combustor assembly of claim 5 , wherein the secondary flow passage defines a decreasing cross sectional area from approximately the one or more inlet openings to approximately the one or more secondary openings.

7. A combustor assembly defining a lengthwise direction, a radial direction, and a circumferential direction, the combustor assembly comprising:

a volute wall extended annularly around a combustor centerline, wherein the volute wall is extended at least partially as a spiral curve from a circumferential reference line around the combustor centerline, and wherein the volute wall defines a combustion chamber therewithin;

an annular inner wall extended at least partially along the lengthwise direction from the volute wall; and

an annular outer wall extended at least partially along the lengthwise direction from the volute wall;

wherein the annular inner wall and the annular outer wall are separated along the radial direction from the combustor centerline,

wherein a primary flow passage is defined between the annular inner wall and the annular outer wall in fluid communication with the combustion chamber,

wherein the volute wall defines a primary opening having a primary fuel injector extending therethrough,

wherein a portion of the volute wall and a portion of the annular outer wall together define a secondary flow passage therebetween,

wherein the volute wall and the annular outer wall together define one or more secondary openings adjacent to the combustion chamber and in fluid communication therewith,

wherein the annular outer wall defines one or more inlet openings in fluid communication with the secondary flow passage and the one or more secondary openings,

wherein the secondary flow passage defines a decreasing cross sectional area from approximately the one or more inlet openings to approximately the one or more secondary openings, and

wherein a secondary fuel injector is extended at least partially into the secondary flow passage through the one or more inlet openings.

8. The combustor assembly of claim 4 , wherein the volute wall extends B from a first radius disposed approximately at the one or more secondary openings to a second radius disposed approximately at the annular inner wall, and wherein the first radius is greater than the second radius.

9. The combustor assembly of claim 4 , wherein the secondary flow passage is extended at least partially annularly relative to the combustor centerline.

10. The combustor assembly of claim 4 , wherein a secondary flow passage wall is extended to the portion of the volute wall and the portion of the annular outer wall together defining the secondary flow passage, wherein the secondary flow passage wall defines two or more discrete secondary flow passages in adjacent circumferential arrangement around the combustor centerline.

11. The combustor assembly of claim 2 ,

wherein the volute wall and the annular outer wall together define one or more secondary openings, and

wherein the annular outer wall defines a tertiary opening therethrough adjacent to the primary flow passage.

12. The combustor assembly of claim 1 , wherein the tertiary fuel injector is extended at least partially at a tangent angle relative to the annular outer wall and the combustor centerline.

13. The combustor assembly of claim 1 , wherein the volute wall defines one or more volute wall openings therethrough in fluid communication with the combustion chamber.

14. The combustor assembly of claim 13 , wherein the volute wall defines a volute wall passage extended to the one or more volute wall openings, the volute wall passage extended from a pressure plenum surrounding the volute wall, the annular inner wall, and the annular outer wall.

15. The combustor assembly of claim 14 , wherein a second reference chord is defined from the volute wall, and wherein the volute wall defines the volute wall passage at an acute angle relative to the second reference chord.

16. The combustor assembly of claim 1 , further comprising a diffuser case surrounding the volute wall, the annular inner wall, and the annular outer wall, the diffuser case comprising an inner diffuser wall defined inward of the annular inner wall and the volute wall along the radial direction, and an outer diffuser wall defined outward of the annular outer wall and the volute wall along the radial direction, and wherein the diffuser case is extended at least partially along the lengthwise direction, the diffuser case defining a pressure plenum surrounding the volute wall, the annular outer wall, and the annular inner wall.

17. The combustor assembly of claim 1 , further comprising

a second inner wall disposed inward of the annular inner wall along the radial direction,

wherein the second inner wall is extended at least partially along the lengthwise direction, and

wherein an inner cooling flow passage is defined therebetween.

18. The combustor assembly of claim 1 , further comprising

a second outer wall disposed outward of the annular outer wall along the radial direction,

wherein the second outer wall is extended at least partially along the lengthwise direction, and

wherein an outer cooling flow passage is defined therebetween.

19. The combustor assembly of claim 1 , wherein the secondary fuel injector is extended at least partially into the secondary flow passage through one or more inlet openings of the annular outer wall.