Volute trapped vortex combustor assembly

Patent metadata

Field	Value
Publication number	US-10976052-B2
Application number	US-201715793104-A
Country	US
Kind code	B2
Filing date	Oct 25, 2017
Priority date	Oct 25, 2017
Publication date	Apr 13, 2021
Grant date	Apr 13, 2021

Abstract

A combustor assembly is generally provided. The combustor assembly includes a volute wall extended annularly around a combustor centerline. The volute wall is extended at least partially as a spiral curve from a circumferential reference line around the combustor centerline. The volute wall defines a combustion chamber therewithin. An annular inner wall is extended at least partially along a lengthwise direction from the volute wall. An annular outer wall is extended at least partially along the lengthwise direction from the volute wall. The inner wall and the outer wall are each separated along a radial direction from the combustor centerline. A primary flow passage is defined between the inner wall and the outer wall in fluid communication from the combustion chamber.

First claim

What is claimed is:

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

Assignees

• Gen Electric

Inventors

• Boardman Gregory Allen
• Naik Pradeep
• Zelina Joseph
• Cooper Clayton Stuart

Classifications

• F23R3/425

  Combustion chambers comprising a tangential or helicoidal arrangement of the flame tubes · CPC title

• F23R3/42 Primary

  characterised by the arrangement or form of the flame tubes or combustion chambers · CPC title

• F23R3/28

  characterised by the fuel supply (burners F23D) · CPC title

• F23R3/12

  inducing a vortex · CPC title

• F23R3/286 Primary

  having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title