Burner system and process for natural gas production

Patent metadata

Field	Value
Publication number	US-11898747-B2
Application number	US-202117162309-A
Country	US
Kind code	B2
Filing date	Jan 29, 2021
Priority date	Apr 30, 2020
Publication date	Feb 13, 2024
Grant date	Feb 13, 2024

Abstract

A burner apparatus and process are described. The burner apparatus includes an inlet chamber in communication with a combustion chamber. The combustion chamber has a cylindrical shape defining a longitudinal axis and a radial direction orthogonal to the longitudinal axis. The combustion chamber has an upstream end and a downstream end, and an air inlet is disposed in the inlet chamber. A pilot, a fuel gas inlet, and a refractory material are disposed in the combustion chamber downstream of the air inlet. A mixed gas inlet is positioned downstream of the fuel gas inlet and the pilot in the combustion chamber. The mixed gas inlet includes a manifold having an inlet, a body, and a plurality of nozzles.

First claim

What is claimed is:

1. A burner apparatus comprising:
an inlet chamber in communication with a combustion chamber;
the combustion chamber having a round cross section and a longitudinal axis, combustion chamber having a radial direction orthogonal to the longitudinal axis, the combustion chamber having an upstream end and a downstream end;
an air inlet disposed in the inlet chamber;
a pilot, a fuel gas inlet disposed in the wall of the combustion chamber, and a refractory material disposed in the combustion chamber downstream of the air inlet and the pilot; and
a mixed gas inlet positioned in the combustion chamber downstream of the fuel gas inlet, the mixed gas inlet comprising a manifold having an inlet and a body,
wherein the body of the manifold extends completely around a circumference of the combustion chamber downstream of the fuel gas inlet.

2. The burner apparatus of claim 1 , wherein the combustion chamber has a diameter, and wherein the inlet chamber and the combustion chamber are joined by an opening defined by an upstream wall of the combustion chamber, wherein the opening is smaller than the diameter of the combustion chamber.

3. The burner apparatus of claim 2 , wherein the opening is defined by an upstream converging portion and a downstream diverging portion.

4. The burner apparatus of claim 2 , wherein the pilot extends from an outer wall of the combustion chamber toward the longitudinal axis of the combustion chamber.

5. The burner apparatus of claim 1 , wherein the fuel gas inlet is disposed at an angle relative to the longitudinal axis of the combustion chamber.

6. The burner apparatus of claim 5 , wherein the angle is between about 20 and about 70 degrees.

7. The burner apparatus of claim 1 , wherein the manifold comprises a plurality of nozzles.

8. The burner apparatus of claim 7 , wherein the plurality of nozzles is disposed around the circumference of the combustion chamber and are oriented at a further angle relative to the longitudinal axis of the combustion chamber.

9. A burner apparatus for comprising:
an inlet chamber in communication with a combustion chamber;
the combustion chamber having a cylindrical shape having a longitudinal axis and a radial direction orthogonal to the longitudinal axis, the combustion chamber having an upstream end and a downstream end;
an air inlet disposed in the inlet chamber;
a pilot, a fuel gas inlet disposed in the wall of the combustion chamber, and a refractory material disposed in the combustion chamber downstream of the air inlet and the pilot; and
a mixed gas inlet positioned in the combustion chamber downstream of the fuel gas inlet, the mixed gas inlet comprising a manifold having an inlet, a body, and a plurality of nozzles,
wherein the body of the manifold extends completely around a circumference of the combustion chamber downstream of the fuel gas inlet.

10. The burner apparatus of claim 9 , wherein each of the plurality of nozzles has a nozzle axis that is disposed at an angle relative to the longitudinal axis of the combustion chamber.

11. The burner apparatus of claim 9 , wherein each of the plurality of nozzles is spaced equally around a circumference of the combustion chamber.

12. The burner apparatus of claim 9 , the combustion chamber having walls comprising a refractory material, wherein the plurality of nozzles comprise a further material and extend through the refractory material of the combustion chamber.

13. The burner apparatus of claim 9 , wherein each of the plurality of nozzles is disposed on an inner surface of the body.

14. The burner apparatus of claim 9 , wherein the inlet chamber and the combustion chamber are joined by an opening defined by an upstream wall of the combustion chamber comprising a refractory material.

15. The burner apparatus of claim 14 , wherein the opening is formed by an upstream converging portion and a downstream diverging portion of the upstream wall of the combustion chamber.

16. The burner apparatus of claim 9 , wherein the fuel gas inlet has a nozzle axis that is disposed at a further angle relative to the longitudinal axis of the combustion chamber.

17. The burner apparatus of claim 10 , wherein the angle is between about 5 and about 45 degrees.

18. The burner apparatus of claim 16 , wherein the further angle is between about 20 and about 70 degrees.

19. A burner process comprising:
injecting air into an air inlet of a burner apparatus, the burner apparatus having an inlet chamber in communication with a combustion chamber, wherein the air inlet is disposed in the inlet chamber, and a pilot, a fuel gas inlet disposed in the wall of the combustion chamber, and a mixed gas inlet are disposed in the combustion chamber downstream of the fuel gas inlet, and wherein the combustion chamber is lined with a refractory material and has a cylindrical shape defining a longitudinal axis and a radial direction orthogonal to the longitudinal axis, the combustion chamber having an upstream end and a downstream end;
injecting a mixed gas stream into the mixed gas inlet, the mixed gas inlet disposed downstream of the fuel gas inlet, the mixed gas inlet comprising a manifold having an inlet, a body, and a plurality of nozzles, wherein the body of the manifold extends completely around a circumference of the combustion chamber downstream of the fuel gas inlet; and
combusting air and fuel gas in the combustion chamber.

Assignees

• Honeywell Int
• Honeywell Int Inc

Inventors

• Whyman William J
• Arnold Kenny

Classifications

• F23D11/107 Primary

  at least one of both being subjected to a swirling motion · CPC title

• F23C7/002

  the air being submitted to a rotary or spinning motion (cyclonic combustion chamber F23C3/006) · CPC title

• F23D2204/10

  gaseous and liquid fuel · CPC title

• F23G7/065 Primary

  using gaseous or liquid fuel · CPC title

• F23G5/32

  the waste being subjected to a whirling movement, e.g. cyclonic incinerators · CPC title