Exhaust gas additive/treatment system and mixer for use therein

• US 8,141,353 B2
• Filed: 04/25/2008
• Issued: 03/27/2012
• Est. Priority Date: 04/25/2008
• Status: Expired due to Fees

• Current Assignee: Tenneco Automotive Operating Company Incorporated (Apollo Global Management, Inc.)
• Original Assignee: Tenneco Automotive Operating Company Incorporated (Apollo Global Management, Inc.)
• Inventors: Zheng, Guanyu, Zhang, Yongyue, Popovich, Jeremy D., Yetken, Dervis A., Kotrba, Adam J.
• Primary Examiner(s): Denion, Thomas
• Assistant Examiner(s): BRADLEY, AUDREY KLASTERKA
• Application Number:
  US12/150,269
• Publication Number:
  US 20090266064A1
• Time in Patent Office: 1,432 Days
• Field of Search: 602/86, 602/95, 603/03, 603/24, 607/48, 607/70, 123/527, 123/590, 553/91, 181/213, 239/432, 239/590, 239/590.5, 366336-340, 415/185, 415/191, 415/208.2, 415/209.4, 415/210.1, 415/211.2
• US Class Current: 60/324
• CPC Class Codes: B01F 23/2132 using nozzles
• CPC Class Codes: B01F 25/25 Mixing by jets impinging against collision plates
• CPC Class Codes: B01F 25/3131 with additional mixing means other than injector mixers, e.g. screens, baffles or rotating elements
• CPC Class Codes: B01F 25/4315 the baffles being deformed flat pieces of material B01F25/4314 takes precedence
• CPC Class Codes: B01F 25/431974 Support members, e.g. tubular collars, with projecting baffles fitted inside the mixing tube or adjacent to the inner wall
• CPC Class Codes: F01N 2240/20 a flow director or deflector
• CPC Class Codes: F01N 3/2066 Selective catalytic reduction [SCR]
• CPC Class Codes: F01N 3/2892 Exhaust flow directors or the like, e.g. upstream of catalytic device
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

An exhaust mixer (16) is provided for use in an engine exhaust system (10) downstream from an additive injector (14). The mixer (16) includes a first wall structure (20), and a second wall structure (22) carrying a set of mixer vanes (30), the second wall structure (22) being cone shaped and extending radially outwardly from the first wall structure (20).

Claims

1. An exhaust mixer for use in an engine exhaust system downstream from an additive injector, the mixer comprising:

a first disc-shaped wall structure with a plurality of flow openings formed therein; and

a second wall structure carrying a set of mixer vanes, the second wall structure having a cone shape extending radially outwardly from and intersecting the first wall structure such that the first wall structure truncates the cone shape.

2. The mixer of claim 1 wherein each of the vanes of the set of mixer vanes is trapezoidal shaped.

3. The mixer of claim 1 wherein each of the vanes of the set of mixer vanes extends radially inwardly from the cone shaped wall structure.

4. The mixer of claim 1 wherein the first wall structure has two semicresent shaped openings formed therein.

5. The mixer of claim 1 wherein the first wall structure has at least two openings passing therethrough.

6. The mixer of claim 5 wherein the at least two openings have no mixer vane structure associated therewith.

7. An exhaust mixer for use in an engine exhaust system downstream from an additive injector, the mixer comprising:

a first disc-shaped wall structure with a plurality of flow openings formed therein;

a second wall structure carrying a set of mixer vanes, the second wall structure being cone shaped and extending radially outwardly from of the first wall structure; and

wherein the vanes of the set are perforate.

8. An exhaust mixer for use in an engine exhaust system downstream from an additive injector, the mixer comprising:

a first disc-shaped wall structure with a plurality of flow openings formed therein;

a second wall structure carrying a set of mixer vanes, the second wall structure being cone shaped and extending radially outwardly from of the first wall structure; and

wherein the first wall structure carries an inner set of mixer vanes.

9. The mixer of claim 8 wherein the inner set of mixer vanes are of a different size than the set of mixer vanes carried on the second wall structure.

10. The mixer of claim 8 wherein the inner set of mixer vanes are of a different shape than the set of mixer vanes carried on the second wall structure.

11. An exhaust mixer for use in an engine exhaust system downstream from an additive injector, the mixer comprising:

a first set of mixer vanes having a first size and shape; and

a second set of mixer vanes having a second size and shape and located radially outwardly from the first set of mixer vanes the second size and shape being different from the first size and shape, wherein the first set of mixer vanes is carried on a disc-shaped wall structure, wherein the second set of mixer vanes is carried on a cone shaped wall structure.

12. The mixer of claim 11 wherein the first set of mixer vanes are each triangular shaped.

13. The mixer of claim 11 wherein the second set of mixer vanes are each trapezoidal shaped.

14. An exhaust mixer for use in an engine exhaust system downstream from an additive injector, the mixer comprising:

a first set of triangular shaped mixer vanes; and

a second set of trapezoidal shaped mixer vanes spaced radially outwardly from the first set of vanes, wherein the first set of mixer vanes is carried on a disc-shaped wall structure, wherein the second set of mixer vanes is carried on a cone shaped wall structure.

15. The mixer of claim 14 wherein the first set of mixer vanes are of a different size than the second set of mixer vanes.

16. The mixer of claim 14 wherein each of the mixer vanes of the first set are less than half the size of mixer vanes of the second set.

17. An exhaust mixer for use in an engine exhaust system downstream from an additive injector, the mixer comprising:

a first disc-shaped wall structure with a plurality of flow openings formed therein;

a second wall structure carrying a set of mixer vanes, the second wall structure being cone shaped and extending radially outwardly from of the first wall structure; and

wherein at least one of the vanes of the set of mixer vanes is divided to form at least a pair of subvanes, each of the subvanes having a different angle of intersection with the second wall structure from the other of the subvanes.