Exhaust treatment method and apparatus having particulate filters and scr
US-2024159174-A1 · May 16, 2024 · US
US9745879B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9745879-B2 |
| Application number | US-201214372810-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 25, 2012 |
| Priority date | Jan 25, 2012 |
| Publication date | Aug 29, 2017 |
| Grant date | Aug 29, 2017 |
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According to one embodiment, an apparatus ( 50 ) for mounting to an inner wall ( 33 ) of an exhaust tube ( 32 ) includes a tube engagement surface ( 52 ) and an exhaust engagement surface ( 54 A). The tube engagement surface comprises a convex surface of a constant first radius of curvature about a first axis. The exhaust engagement surface is adjacent the tube engagement surface, and includes a concave surface of a second radius of curvature about a second axis generally perpendicular to the first axis.
Opening claim text (preview).
The invention claimed is: 1. A reductant decomposition system for an exhaust aftertreatment system, comprising: a straight decomposition tube comprising an inlet and outlet; a first curved tube comprising an inlet and an outlet, the outlet coupled to the inlet of the straight decomposition tube, the first curved tube configured to redirect a flow of the exhaust gas from a first direction to a second direction different from the first direction towards the straight decomposition tube; a second curved tube comprising an inlet and an outlet, the inlet extending from the outlet of the straight decomposition tube, the second curved tube configured to redirect a flow of the exhaust gas from a third direction to a fourth direction different from the third direction away from the straight decomposition tube; a reductant injector port positioned upstream of the inlet of the straight decomposition tube; and a baffle secured to an inner wall of the second curved tube, the baffle comprising a leading concave surface. 2. The reductant decomposition system of claim 1 , wherein the baffle further comprises a trailing concave surface, and wherein the radii of curvature of the leading and trailing concave surfaces are the same. 3. The reductant decomposition system of claim 1 , wherein a radially innermost edge of the baffle defines a chord of the tube to which the baffle is secured, the chord being smaller than an inner diameter of the tube to which the baffle is secured. 4. The reductant decomposition system of claim 1 , wherein the baffle extends a radial distance into the tube to which the baffle is secured, the radial distance being between 10% and 50% of an inner radius of the tube to which the baffle is secured. 5. The reductant decomposition system of claim 1 , further comprising a second baffle, wherein the second baffle is secured to the inner wall of the straight decomposition tube, and one of the first curved tube and the second curved tube comprises an upstream curved tube, the outlet of the upstream curved tube being coupled to the inlet of the straight tube, wherein the second baffle is positioned a distance away from the outlet of the upstream curved tube, and wherein a ratio of the distance to a radius of curvature of the upstream curved tube is between 0.5 and 1.5. 6. The reductant decomposition system of claim 5 , wherein the ratio of the distance to the radius of curvature of the upstream curved tube is 0.9. 7. The reductant decomposition system of claim 1 , further comprising a second baffle, wherein the second baffle is secured to the inner wall of the straight decomposition tube, and one of the first curved tube and the second curved tube is an upstream curved tube, the outlet of the upstream curved tube being coupled to the inlet of the straight tube, wherein the second baffle is positioned between 200 mm and 250 mm away from the reductant injector port. 8. The reductant decomposition system of claim 1 , further comprising a second baffle, wherein the second baffle is secured to the inner wall of the straight decomposition tube, and one of the first curved tube and the second curved tube comprises an upstream curved tube, the outlet of the upstream curved tube being coupled to the inlet of the straight tube, wherein the second baffle is oriented such that the leading and trailing concave surfaces are perpendicular to an exhaust flow direction through the straight decomposition tube. 9. The reductant decomposition system of claim 1 , further comprising a second baffle, wherein the second baffle is secured to the inner wall of the straight decomposition tube, and one of the first curved tube and the second curved tube comprises an upstream curved tube, the outlet of the upstream curved tube being coupled to the inlet of the straight tube, wherein the second baffle is positioned on a portion of the inner wall receiving the highest velocity exhaust gases out of the upstream curved tube. 10. The reductant decomposition system of claim 1 , wherein one of the first curved tube and the second curved tube comprises a downstream curved tube, the inlet of the downstream curved tube being coupled to the outlet of the straight tube, the baffle being positioned a distance away from the inlet of the downstream curved tube, and wherein a ratio of the distance to a radius of curvature of the downstream curved tube is between 0.1 and 0.5. 11. The reductant decomposition system of claim 10 , wherein the ratio of the distance to the radius of curvature of the downstream curved tube is 0.33. 12. The reductant decomposition system of claim 1 , wherein one of the first curved tube and the second curved tube comprises a downstream curved tube, the inlet of the downstream curved tube being coupled to the outlet of the straight tube, the baffle is oriented such that the leading concave surface is perpendicular to an exhaust flow direction through the straight decomposition tube. 13. The reductant decomposition system of claim 1 , wherein the baffle further comprises one of a recess and protrusion, the inner wall comprising the other of the recess and protrusion, and wherein the recess and protrusion are engageable to properly position the baffle relative to the inner wall. 14. The reductant decomposition system of claim 1 , wherein the baffle is secured to the inner wall of the straight decomposition tube, and one of the first curved tube and the second curved tube comprises an upstream curved tube, the outlet of the upstream curved tube being coupled to the inlet of the straight tube, wherein the reductant injector port is formed in the upstream curved tube. 15. A reductant decomposition system for an exhaust aftertreatment system, comprising: a straight decomposition tube comprising an inlet and outlet; a curved tube comprising an inlet and an outlet; a reductant injector port positioned upstream of the inlet of the straight decomposition tube; and a baffle comprising a leading concave surface, wherein the baffle is secured to the inner wall of the straight decomposition tube, and the curved tube comprises an upstream curved tube, the outlet of the upstream curved tube being coupled to the inlet of the straight tube, wherein the baffle is positioned a distance away from the outlet of the upstream curved tube, and wherein a ratio of the distance to a radius of curvature of the upstream curved tube is between 0.5 and 1.5. 16. The reductant decomposition system of claim 15 , wherein the ratio of the distance to the radius of curvature of the upstream curved tube is 0.9. 17. A reductant decomposition system for an exhaust aftertreatment system, comprising: a straight decomposition tube comprising an inlet and outlet; a curved tube comprising an inlet and an outlet; a reductant injector port positioned upstream of the inlet of the straight decomposition tube; and a baffle comprising a leading concave surface, wherein the curved tube comprises a downstream curved tube, the inlet of the downstream curved tube being coupled to the outlet of the straight decomposition tube, wherein the baffle is secured to an inner wall of the downstream curved tube, the baffle being positioned a distance away from the inlet of the downstream curved tube, and wherein a ratio of the distance to a radius of curvature of the downstream curved tube is between 0.1 and 0.5. 18. The reductant decomposition system of claim 17 , wherein the ratio of the distance to the radius of curvature of the downstream curved tube is 0.33. 19. A reductant decomposition system for an exhaust aftertr
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