Trapped vortex combustor and method for operating the same

Patent metadata

Field	Value
Publication number	US-11073286-B2
Application number	US-201715709958-A
Country	US
Kind code	B2
Filing date	Sep 20, 2017
Priority date	Sep 20, 2017
Publication date	Jul 27, 2021
Grant date	Jul 27, 2021

Abstract

Various embodiments include a trapped vortex combustor and a method for operating trapped vortex combustor. In one embodiment, the trapped vortex combustor comprises a trapped vortex combustion zone and at least one secondary combustion zone disposed downstream of the trapped vortex combustion zone. The trapped vortex combustion zone is operable to receive and combust a first fuel and a first air and produce a first combustion product flowing toroidally therein. The at least one secondary combustion zone is operable to receive and combust the first combustion product and at least one second injection consisting of fuel and/or air and produce at least one second combustion product therein. The combustor may reduce the residence time of the highest temperature combustion products and achieve the lower NOx emission.

First claim

What is claimed is:

1. A trapped vortex combustor defining an axial direction, comprising:
a wall defining a trapped vortex combustion zone,
the trapped vortex combustion zone operable to receive and combust a first fuel and a first air and produce a first combustion product therein,
the first air directed into the trapped vortex combustion zone at a plurality of axial and radial locations along a periphery of the wall in a plurality of directions, the plurality of directions varying from aft to partially forward, each of the plurality of directions forming an oblique angle with the wall at the plurality of locations such that the first air flows toroidally within the trapped vortex combustion zone to thereby flow the first combustion product toroidally therein;
at least one secondary combustion fuel nozzle that is disposed downstream of the trapped vortex combustion zone, that is directed in a direction that forms a first angle that is an acute angle with respect to the axial direction, and that is operable to inject at least one second injection comprising fuel; and
at least one secondary combustion zone disposed downstream of the trapped vortex combustion zone, and operable to receive and combust the first combustion product and the at least one second injection from the secondary combustion fuel nozzle and produce at least one second combustion product therein.

2. The trapped vortex combustor of claim 1 , further comprising a combustor exit, wherein the at least one secondary combustion zone is located nearer to the combustor exit than the trapped vortex combustion zone.

3. The trapped vortex combustor of claim 1 , wherein the at least one secondary combustion zone comprises a secondary combustion zone and at least one tertiary combustion zone disposed downstream of the secondary combustion zone, and the at least one tertiary combustion zone is operable to receive and combust the at least one second combustion product and at least one third injection consisting of fuel and/or air and produce at least one third combustion product therein.

4. The trapped vortex combustor of claim 1 , wherein the trapped vortex combustor comprises an annular combustor, and the trapped vortex combustion zone is configured as arcuate or rectangular or circular in cross-section.

5. The trapped vortex combustor of claim 1 , wherein an air jet partition is disposed between the trapped vortex combustion zone and the at least one secondary combustion zone, and the air jet partition is operable to jet air for separating combusting in the trapped vortex combustion zone from combusting in the at least one secondary combustion zone.

6. The trapped vortex combustor of claim 1 , wherein a structural partition is disposed between the trapped vortex combustion zone and the at least one secondary combustion zone, and the structural partition is utilized for separating combusting in the trapped vortex combustion zone from combusting in the at least one secondary combustion zone.

7. The trapped vortex combustor of claim 1 , wherein the trapped vortex combustion zone is configured as a trapped vortex combustion cavity, and the first air is directed into the trapped vortex combustor along a periphery of the trapped vortex combustion cavity.

8. The trapped vortex combustor of claim 7 , wherein at least one of the first air and the first combustion product in the trapped vortex combustion cavity is operable to flow in a clockwise direction or in a counterclockwise direction or a combination thereof.

9. The trapped vortex combustor of claim 1 , wherein the secondary combustion fuel nozzle is operable to inject the at least one second injection in the direction that forms a second angle between 30 to 90 degrees relative to the first combustion product exiting the trapped vortex combustion zone.

10. The trapped vortex combustor of claim 9 , wherein the second angle is between 30 to 60 degrees.

11. The trapped vortex combustor of claim 1 , wherein the first product exiting the trapped vortex combustion zone forms a third angle that is an acute angle with respect to the axial direction.

12. A trapped vortex combustor comprising:
a wall defining a trapped vortex combustion zone,
the trapped vortex combustion zone operable to receive and combust a first fuel and a first air and produce a first combustion product therein, the first air directed into the trapped vortex combustion zone at a plurality of axial and radial locations along a periphery of the wall in a plurality of directions, the plurality of directions varying from aft to partially forward, each of the plurality of directions forming an oblique angle with the wall at the plurality of locations such that the first air flows toroidally within the trapped vortex combustion zone to thereby flow the first combustion product toroidally therein;
at least one secondary combustion fuel nozzle that is disposed downstream of the trapped vortex combustion zone and that is operable to inject at least one second injection comprising fuel in a direction that forms an angle of between 30 and 60 degrees with respect to the first combustion product exiting the trapped vortex zone; and
at least one secondary combustion zone disposed downstream of the trapped vortex combustion zone, and operable to receive and combust the first combustion product and the at least one second injection from the secondary combustion fuel nozzle and produce at least one second combustion product therein.

13. The trapped vortex combustor of claim 12 , wherein the first product exiting the trapped vortex combustion zone forms another angle that is an acute angle with respect to an axial direction defined by the trapped vortex combustor.

Assignees

• Gen Electric

Inventors

• Boardman Gregory Allen
• Benjamin Michael Anthony
• Cooper Clayton Stuart
• Zelina Joseph
• Stevens Eric John

Classifications

• F23R3/346

  for staged combustion · CPC title

• F23R2900/00015

  Trapped vortex combustion chambers · CPC title

• F23R3/18

  Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants · CPC title

• F23R3/34 Primary

  Feeding into different combustion zones · CPC title

• F23R3/12

  inducing a vortex · CPC title