Exhaust gas and reductant mixer for an aftertreatment system

Patent metadata

Field	Value
Publication number	US-11761365-B2
Application number	US-202017642628-A
Country	US
Kind code	B2
Filing date	Sep 11, 2020
Priority date	Sep 13, 2019
Publication date	Sep 19, 2023
Grant date	Sep 19, 2023

Abstract

Apparatus and method for mixing reductant in an exhaust gas flow using virtual interception. Embodiments include an exhaust gas and reductant mixer comprising a body, a first flow device, and a reductant entry port. The body defines an exhaust gas flow path having a central portion. The first flow device swirls the exhaust gas in a circumferential direction with respect to the gas flow path. The reductant entry port introduces the reductant into the gas flow path at a location downstream from the first flow device and in an introduction direction (1) offset from the central portion, and (2) opposite the circumferential direction.

First claim

What is claimed is:

1. An exhaust gas and reductant mixer, comprising:
a body defining an exhaust gas flow path, wherein the exhaust gas flow path has a central portion;
a first flow device to swirl the exhaust gas in a circumferential direction with respect to the gas flow path; and
a reductant entry port to introduce the reductant into the gas flow path at a location downstream from the first flow device and in an introduction direction (1) offset from the central portion, and (2) opposite the circumferential direction.

2. The mixer of claim 1 wherein the introduction direction is a direction about an axis between 5° and 85° away from an axis extending from the reductant entry port to the central portion of the gas flow path.

3. The mixer of claim 1 wherein the introduction direction is a direction about an axis between 25° and 35° away from an axis extending from the reductant entry port to the central portion of the gas flow path.

4. The mixer of claim 1 and further including a doser for introducing a conical or fan shaped bolus of the reductant through the reductant entry port.

5. The mixer of claim 1 wherein:
the body includes an exhaust inlet portion upstream from the reductant entry port; and
the first flow device is located at the exhaust inlet portion.

6. The mixer of claim 1 , wherein the mixer is free of splash plates.

7. The mixer of claim 1 , wherein the first flow device comprises a plurality of vanes.

8. The mixer of claim 7 wherein each of the vanes of the first flow device defines a vane angle between 45° and 89° with respect to the gas flow path.

9. The mixer of claim 7 wherein each of the vanes of the first flow device defines a vane angle between 65° and 85° with respect to the gas flow path.

10. The mixer of claim 7 wherein each of the vanes of the first flow device defines a vane angle between 70° and 80° with respect to the gas flow path.

11. The mixer of claim 7 wherein two or more of the vanes of the first flow device overlap one another in the circumferential direction.

12. The mixer of claim 7 wherein two or more of the vanes of the first flow device have adjacent edges defining a gap in the circumferential direction.

13. The mixer of claim 7 wherein the reductant entry port and first flow device are configured to optimize mixing uniformity of the reductant in the exhaust gas flow.

14. The mixer of claim 7 wherein the vanes of the first flow device extend around a portion between 130° and 230° of a circumference of the gas flow path.

15. The mixer of claim 7 wherein the vanes of the first flow device extend around a portion between 170° and 190° of a circumference of the gas flow path.

16. The mixer of claim 7 wherein the vanes of the first flow device extend around a portion less than 360° of a circumference of the gas flow path.

17. The mixer of claim 16 and further including a first blocking member in a circumferential portion of gas flow path where the vanes of the first flow device do not extend and upstream from the reductant entry port.

18. The mixer of claim 17 wherein the first blocking member is located in a circumferential portion of the gas flow path corresponding to the location of the reductant entry port.

19. The mixer of claim 17 wherein the blocking member is located generally parallel to the first flow device.

20. The mixer of claim 1 and further including a second flow device at a location downstream from the reductant entry port to swirl the exhaust gas in a circumferential direction.

21. The mixer of claim 20 wherein the second flow device swirls the exhaust gas in the same circumferential direction that the first flow device swirls the exhaust gas.

22. The mixer of claim 20 wherein the second flow device swirls the exhaust gas in an opposite circumferential direction that the first flow device swirls the exhaust gas.

23. The mixer of claim 20 wherein a hub of one or both of the first flow device and the second flow device is radially offset from a mixer center axis.

24. The mixer of claim 20 wherein the second flow device comprises a plurality of vanes.

25. The mixer of claim 24 wherein each of the second flow device vanes defines a vane angle between 45° and 89° with respect to the gas flow path.

26. The mixer of claim 24 wherein each of the second flow device vanes defines a vane angle between 55° and 75°.

27. The mixer of claim 24 wherein two or more of the second flow device vanes overlap one another in the circumferential direction.

28. The mixer of claim 24 wherein two or more of the second flow device vanes have adjacent edges defining a gap in the circumferential direction.

29. The mixer of claim 24 wherein the reductant entry port and second flow device are configured to optimize mixing uniformity of the reductant in the exhaust gas flow.

30. The mixer of claim 24 wherein the vanes of the second flow device extend around a portion of between 200° and 280° of a circumference of the gas flow path.

31. The mixer of claim 24 wherein the vanes of the second flow device extend around a portion between 220° and 260° of a circumference of the gas flow path.

32. The mixer of claim 24 wherein the vanes of the second flow device extend around a portion of less than 360° of a circumference of the gas flow path.

33. The mixer of claim 32 and further including a second blocking member in a circumferential portion of gas flow path where the vanes of the second flow device do not extend and downstream from the reductant entry port.

34. The mixer of claim 33 wherein the second blocking member is located in a circumferential portion of the gas flow path corresponding the location of the reductant entry port.

35. The mixer of claim 33 wherein the second blocking member is located generally parallel to the vanes of the second flow device.

36. An exhaust aftertreatment system including the mixer of claim 1 .

37. A method for mixing reductant in an exhaust gas flow, comprising:
swirling the exhaust gas flow in a circumferential direction with respect to a flow path by a flow device; and
introducing the reductant into the swirling exhaust gas flow at a location downstream from the flow device in a direction offset from a central portion of the flow and opposite the circumferential direction of the flow.

Assignees

• Cummins Inc

Inventors

• Liu Z Gerald
• Kalyankar Apoorv
• Schmidt Niklas
• Mannannur Achuth

Classifications

• F01N3/2892 Primary

  Exhaust flow directors or the like, e.g. upstream of catalytic device · CPC title

• F01N2240/20

  a flow director or deflector · CPC title

• F01N2610/1453

  Sprayers or atomisers; Arrangement thereof in the exhaust apparatus · CPC title

• F01N2610/02

  the substance being ammonia or urea · CPC title

• F01N2610/03

  the substance being hydrocarbons, e.g. engine fuel · CPC title