IP Library Granted Patent US 8,661,792
Granted Patent B2
US 8,661,792 · App. 13/378,433 · Granted Mar 4, 2014

Exhaust line with injection system

Inventors: Frederic Greber (Ecot, FR); Yohann Perrot (Belleville-en-Caux, FR); Jean-Paul Brunel (Meslieres, FR)
Assignee: Faurecia Systemes d'Echappement
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Quick Facts
Patent No.
US 8,661,792
App. No.
13/378,433
Granted
Mar 4, 2014
Kind
B2
Abstract

An exhaust line has upstream and downstream blocks for processing exhaust gases. An injection section is arranged between an upstream face defined by the upstream block and a downstream face defined by the downstream block and includes a circulation channel for the exhaust gas flow extending from the upstream face to the downstream face. The channel includes a central line having a determined length between the upstream and downstream faces. The injection section includes a reagent injector capable of injecting a reagent into the injection section. The injection section has a first cup inside the circulation channel in the flow path such that the average path of exhaust gas jets is higher by at least 20% in relation to the predetermined length. A second cup is arranged inside the circulation channel between the upstream face and the first cup. The reagent is done between the first cup and the second cup.

Claims (24)

1. An automobile exhaust line comprising:

upstream and downstream blocks for processing exhaust gases flowing in the exhaust line, the upstream and downstream blocks being arranged in series in the exhaust line;

an injection section arranged between an upstream face defined by the upstream block and a downstream face defined by the downstream block and including a circulation channel for exhaust gas flow extending from the upstream face to the downstream face, the circulation channel including a central line having a determined length between the upstream and downstream faces, the injection section including a reagent injector mounted on the injection section and capable of injecting a reagent into the injection section;

the injection section comprises at least a first cup arranged inside the circulation channel in the path of the exhaust gas flow such that an average path of exhaust gas jets is higher by at least 20% in relation to the determined length;

wherein the injection section comprises a second cup arranged inside the circulation channel between the upstream face and the first cup; and

wherein the injection of the reagent is done between the first cup and the second cup.

2. The exhaust line according to claim 1 , wherein the determined length is substantially comprised between 40 and 140 mm.

3. The exhaust line according to claim 1 , wherein a bottom of the first cup winds in a spiral around central line of the injection section.

4. The exhaust line according to claim 3 , wherein the bottom of the first cup winds in a spiral around the central line of the injection section, performing three quarters of a revolution.

5. The exhaust line according to claim 3 , wherein the first cup has an opening at an end of the spiral furthest from the upstream face.

6. The exhaust line according to claim 3 , wherein the first cup has a spoiler at an end of the spiral furthest from the upstream face.

7. The exhaust line according to claim 6 , wherein the spoiler extends the bottom of the first cup toward an upstream face and toward the outside of the spiral.

8. The exhaust line according to claim 1 , wherein the second cup has a bottom wound in a spiral around the central line of the injection section.

9. The exhaust line according to claim 8 , wherein the second cup has an opening at an end of the spiral furthest from the upstream face.

10. The exhaust line according to claim 8 , wherein the second cup has an opening at an end of the spiral closest to the upstream face.

11. The exhaust line according to claim 1 , wherein the first and second cups define a spiral-shaped conduit between them, starting from an opening of the second cup and going to an opening of the first cup, extending over at least 180°, and having a straight section substantially greater than 2300 mm 2 .

12. The exhaust line according to claim 1 , wherein the first cup includes a rounded wall having a central zone protruding toward the upstream face and a hollow peripheral zone facing the upstream face surrounding the central zone, an opening being formed in the wall of the first cup between the central zone and the hollow peripheral zone.

13. The exhaust line according to claim 12 , wherein the second cup comprises a rounded wall having a hollow central zone facing the upstream face and a peripheral zone protruding toward the upstream face surrounding the hollow central zone, an opening being formed in the wall of the second cup between the hollow central zone and the peripheral zone.

14. The exhaust line according to claim 13 , wherein the first and second cups are shaped to impart a helical movement to the exhaust gases from the opening of the second cup to the opening of the first cup.

15. The exhaust line according to claim 1 , wherein an opening of the first cup and an opening of the second cup are angularly offset relative to one another around the central line.

16. The exhaust line according to claim 1 , wherein the second cup has perforations with a diameter substantially equal to 5 mm or an opening.

17. The exhaust line according to claim 1 , wherein the first cup comprises a wire mesh layer over at least part of a surface of the first cup.

18. The exhaust line according to claim 1 , wherein the reagent injector is oriented so that an injection direction is perpendicular to the injection section.

19. The exhaust line according to claim 1 , wherein the reagent injector is oriented so that an injection direction is parallel to a tangent to the injection section.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 15, 2014
From: GREBER, FREDERIC; PERROT, YOHANN; BRUNEL, JEAN-PAUL
To: FAURECIA SYSTEMES D'ECHAPPEMENT
Reel/Frame 031971/0168 →
Priority Claims (1)
FR 09 54199 · Jun 19, 2009 · national
Continuity (1)
Related Publication 20120216513A1 · Aug 30, 2012