Ducted fuel injection

Patent metadata

Field	Value
Publication number	US-10161626-B2
Application number	US-201615363966-A
Country	US
Kind code	B2
Filing date	Nov 29, 2016
Priority date	Jul 1, 2015
Publication date	Dec 25, 2018
Grant date	Dec 25, 2018

Abstract

Various technologies presented herein relate to enhancing mixing inside a combustion chamber to form one or more locally premixed mixtures comprising fuel and charge-gas to enable minimal, or no, generation of soot and/or other undesired emissions during ignition and subsequent combustion of the locally premixed mixtures. To enable sufficient mixing of the fuel and charge-gas, a jet of fuel can be directed to pass through a bore of a duct causing charge-gas to be drawn into the bore creating turbulence to mix the fuel and the drawn charge-gas. The duct can be located proximate to an opening in a tip of a fuel injector. The various technologies presented herein can be utilized in a number of combustion systems, such as compression-ignition (CI) reciprocating engines, spark-ignition (SI) reciprocating engines, gas-turbine (GT) engines, burners and boilers, wellhead/refinery flaring, etc.

First claim

What is claimed is:

1. A combustion system, comprising:
a fuel injector comprising a plurality of openings, wherein a fuel is injected through the openings into a combustion chamber of an engine; and
a plurality of ducts located in the combustion chamber, each duct formed from a hollow tube, wherein each duct is aligned with a respective opening in the openings such that the fuel exiting the openings of the fuel injector is injected through the hollow tubes and into the combustion chamber, wherein passage of the fuel through the hollow tubes causes charge-gas present in the combustion chamber to be drawn into the hollow tubes thereby mixing the injected fuel with the charge-gas.

2. The combustion system of claim 1 , wherein the combustion system is a compression-ignition reciprocating engine.

3. The combustion system of claim 1 , wherein the combustion system is a spark-ignition reciprocating engine.

4. The combustion system of claim 1 , wherein the combustion system is a gas-turbine engine.

5. The combustion system of claim 1 , wherein the combustion system is included in a burner apparatus.

6. The combustion system of claim 1 , wherein the combustion system is included in a boiler apparatus.

7. The combustion system of claim 1 , wherein the combustion system is included in an apparatus configured to burn flammable gas in a gas flare operation.

8. A method for mixing a fuel with a charge-gas in a combustion chamber, comprising:
injecting fuel through a plurality of openings in a fuel injector, the openings located in the combustion chamber; and
mixing the injected fuel with the charge-gas in a plurality of ducts located within the combustion chamber, wherein each of the ducts comprises a hollow tube and is aligned with a respective opening in the openings such that the injected fuel travels through the hollow tubes and into the combustion chamber, the passage of the fuel through the hollow tubes causing turbulent flow of the fuel within the hollow tube and thereby causing charge-gas present in the combustion chamber to be drawn into the hollow tubes and mixing the injected fuel with the charge-gas.

9. The method of claim 8 , wherein the combustion chamber forms part of a compression-ignition reciprocating engine.

10. The method of claim 8 , wherein the combustion chamber forms part of a spark-ignition reciprocating engine.

11. The method of claim 8 , wherein the combustion chamber forms part of a gas-turbine engine.

12. The method of claim 8 , wherein the combustion chamber is included in a burner apparatus.

13. The method of claim 8 , wherein the combustion chamber is included in a boiler apparatus.

14. The method of claim 8 , wherein the combustion chamber is included in an apparatus configured to burn flammable gas in a gas flare operation.

15. A fuel injection system, comprising:
a fuel injector comprising a first opening and a second opening, wherein a first jet of fuel is injected through the first opening into a combustion chamber, and a second jet of fuel is injected through the second opening into the combustion chamber;
a first duct positioned in the combustion chamber and formed from a first hollow tube, wherein the first duct is aligned such that the first jet of fuel exiting the first opening is injected through the first hollow tube and into the combustion chamber such that the passage of the fuel through the first hollow tube causes charge-gas present in the combustion chamber to be drawn in the first hollow tube thereby mixing the injected fuel with the charge-gas; and
a second duct positioned in the combustion chamber and formed from a second hollow tube, wherein the second duct is aligned such that the second jet of fuel exiting the second opening is injected through the second hollow tube and into the combustion chamber such that the passage of the fuel through the second hollow tube causes charge-gas present in the combustion chamber to be drawn in the second hollow tube thereby mixing the injected fuel with the charge-gas.

16. The fuel injection system of claim 15 , wherein the fuel injection system is located in a compression-ignition reciprocating engine.

17. The fuel injection system of claim 15 , wherein the fuel injection system is located in a spark-ignition reciprocating engine.

18. The fuel injection system of claim 15 , wherein the fuel injection system is located in a gas-turbine engine.

19. The fuel injection system of claim 15 , wherein the fuel injection system is included in a burner apparatus.

20. The fuel injection system of claim 15 , wherein the fuel injection system is included in an apparatus configured to burn flammable gas in a gas flare operation.

Assignees

• Nat Tech & Eng Solutions Sandia Llc

Inventors

• Mueller Charles J

Classifications

• F23D11/383 Primary

  with swirl means · CPC title

• F02M57/00

  Fuel-injectors combined or associated with other devices · CPC title

• F23D14/08

  with axial outlets at the burner head · CPC title

• F02B1/06 Primary

  Methods of operating · CPC title

• F23D11/408

  Flow influencing devices in the air tube · CPC title