Mixer assembly
12158096 ยท 2024-12-03
Assignee
Inventors
- Sascha HAVERKAMP (Jockgrim, DE)
- Joachim GEHRLEIN (Rheinzabern, DE)
- Stefan KOHRS (Neustadt/Weinstrasse, DE)
- Eric A. HEIN (Neustadt-Diedesfeld, DE)
- Attila KOVACS (Karlsruhe, DE)
Cpc classification
F01N3/0293
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/206
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/4323
PERFORMING OPERATIONS; TRANSPORTING
F01N3/2066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2610/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2260/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2892
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/3141
PERFORMING OPERATIONS; TRANSPORTING
International classification
F01N3/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F23/21
PERFORMING OPERATIONS; TRANSPORTING
B01F23/213
PERFORMING OPERATIONS; TRANSPORTING
B01F25/31
PERFORMING OPERATIONS; TRANSPORTING
B01F25/314
PERFORMING OPERATIONS; TRANSPORTING
B01F25/432
PERFORMING OPERATIONS; TRANSPORTING
F01N3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A mixer assembly comprises a tubular housing including an exhaust gas inlet, an exhaust gas outlet, and a reductant inlet on a side of the tubular housing. An upstream mixing element is positioned within the tubular housing upstream from the reductant inlet. A downstream mixing element is positioned within the tubular housing downstream from the reductant inlet and the upstream mixing element. The upstream and downstream mixing elements at least partially define a reductant receiving mixing chamber in which the injected reductant and exhaust gas mix. A divider is positioned within the tubular housing downstream from the upstream mixing element to split the exhaust into two divided flow streams prior to exiting through the exhaust gas outlet.
Claims
1. A mixer assembly for mixing an injected reductant with an exhaust gas output from a combustion engine, comprising: a tubular housing including a reductant inlet, an exhaust gas inlet and an exhaust gas outlet, the tubular housing defining a longitudinal axis along which the exhaust gas enters the housing, wherein the reductant inlet is positioned on a side of the tubular housing longitudinally between the exhaust gas inlet and the exhaust gas outlet; an upstream mixing element positioned within the tubular housing upstream from the reductant inlet; a downstream mixing element positioned within the tubular housing downstream from the reductant inlet and the upstream mixing element, wherein the upstream mixing element and the downstream mixing element at least partially define a reductant receiving mixing chamber in which the injected reductant and the exhaust gas mix, the downstream mixing element being configured to urge the exhaust gas to flow radially in a direction away from the reductant inlet; and a divider positioned within the tubular housing downstream from the upstream mixing element, the divider including first and second curved surfaces configured to be impacted by the radially flowing exhaust gas to split the exhaust gas into two divided flow streams prior to exiting through the exhaust gas outlet.
2. The mixer assembly of claim 1, wherein the reductant receiving mixing chamber is shaped to impart a swirling motion on the mixed injected reductant and exhaust gas.
3. The mixer assembly of claim 1, wherein the divider is intersected by an axis along which the reductant is injected.
4. The mixer assembly of claim 1, wherein the two divided flow streams swirl in opposite directions to one another.
5. The mixer assembly of claim 1, wherein the injected reductant impacts the two divided flow streams.
6. The mixer assembly of claim 1, wherein the divider is fixed to the upstream mixing element.
7. The mixer assembly of claim 1, wherein the divider is fixed to an inner surface of the tubular housing.
8. The mixer assembly of claim 1, further including a mixing pipe extending across the tubular housing at an angle relative to the longitudinal axis, wherein the mixing pipe includes an inlet aligned with the reductant inlet and at least one aperture extending through the mixing pipe.
9. The mixer assembly of claim 8, wherein the mixing pipe extends substantially perpendicularly to the longitudinal axis.
10. A mixer assembly for mixing an injected reductant with an exhaust gas output from a combustion engine, comprising: a tubular housing including a reductant inlet, an exhaust gas inlet and an exhaust gas outlet, the tubular housing defining a longitudinal axis along which the exhaust gas enters the housing, wherein the reductant inlet is positioned on a side of the tubular housing longitudinally between the exhaust gas inlet and the exhaust gas outlet; an upstream mixing element positioned within the tubular housing upstream from the reductant inlet; a downstream mixing element positioned within the tubular housing downstream from the reductant inlet and the upstream mixing element, wherein the upstream mixing element and the downstream mixing element at least partially define a reductant receiving mixing chamber in which the injected reductant and the exhaust gas mix; and a divider positioned within the tubular housing downstream from the upstream mixing element to split the exhaust gas into two divided flow streams prior to exiting through the exhaust gas outlet, wherein the divider includes a longitudinally extending ridge separating two concave surfaces.
11. A method of mixing an injected reductant with an exhaust gas output from a combustion engine, comprising; receiving exhaust gas in an exhaust gas inlet of a tubular housing; positioning an upstream mixing element within the tubular housing upstream from a reductant inlet of the tubular housing; positioning a downstream mixing element within the tubular housing downstream from the upstream mixing element and the reductant inlet, wherein the upstream mixing element and the downstream mixing element at least partially define a reductant receiving mixing chamber, the reductant inlet being positioned on a side of the tubular housing longitudinally between the exhaust gas inlet and an exhaust gas outlet; injecting reductant into the reductant receiving mixing chamber; positioning a divider within the tubular housing downstream from the upstream mixing element; directing the exhaust gas to flow radially within the tubular housing to impact the divider; splitting the exhaust gas into two divided flow streams as the exhaust gas flows over the divider; mixing the injected reductant with the exhaust gas; and outputting a mixture of exhaust gas and injected reductant through the exhaust gas outlet.
12. The method of claim 11, further including positioning the divider such that an axis along which the reductant is injected intersects the divider.
13. The method of claim 11, further comprising impacting the injected reductant with the two divided flow streams.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Further advantages and details of the invention are explained in the patent claims and in the description and figures, in which:
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DETAILED DESCRIPTION OF THE INVENTION
(11) The mixing device 1 shown in
(12) The outflow side 3.2 of the intermediate wall 3 is according to
(13) Both flow guide elements S1, S2 bound a mixing chamber 2.3, which due to the opposite arrangement of the inflow openings E1, E2 on the one hand and the outflow openings A1, A2 on the other is predominantly flowed through by the exhaust gas stream T in the radial direction.
(14) As can be seen in
(15) In the profile view A-A shown in
(16) In the profile view B-B according to
(17) According to
(18) Decisive for the definition of the angle is the straight line G, which connects the intersection points of the intermediate wall 3 and the pipe wall 2.1, wherein the two intersection points have the greatest distance from each other with respect to the exhaust gas stream or the direction of the mid-axis 2.2.
(19) According to
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(21) A wedge-shaped flow guide element S3 is provided in the area of the wall section W2, which divides the impinging exhaust gas stream T into two partial streams T3, T4. Due to the wedge-shaped design of the flow guide element S3, a partial stream T3 is created with respect to the flow direction, which is deflected in an anticlockwise direction, while the partial stream T4 is deflected in a clockwise direction.
(22) According to
(23) Within the second intermediate wall Z2, further slit-shaped outflow openings Ax are provided, the outflow profile Xa of which is subordinate relative to the outflow opening A1. These then merely serve to prevent a stream bottleneck in the area of the upper wall section W1. Additionally, in the first intermediate wall Z1, further slit-shaped inflow openings Ex are provided, the inflow profile Xe of which is subordinate relative to the inflow profile QE of the inflow opening E1. These serve to prevent a stream bottleneck in front of the first intermediate wall Z1 in the area of the lower wall section W2. A flow blade 9.1 is provided on the respective inflow opening E1, through which the auxiliary stream that flows through the inflow opening Ex can be deflected in a radial direction.
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(25) In the exemplary embodiment shown in
LIST OF REFERENCE NUMERALS
(26) 1 Mixing device 2 Housing 2.1 Tubular wall 2.2 Mid-axis 2.3 Mixing chamber 2.4 Bridge between A1, A2 2.5 Baffle plate 2.6 Bridge between E1, E2 3 Intermediate wall 3.1 Inflow side, windward side 3.2 Off-flow side, lee side 4.1 Exhaust pipe 4.2 Exhaust pipe 5 Feed device 5.1 Feed nozzle 6 Mixer, mixer pipe 6.1 Perforation 7 Corrugated base 8 Cone, ramp, flow guide element 9.1 Blade of Ex 9.2 Blade of Ax A1 Outflow opening A2 Outflow opening Ax Outflow opening E1 Inflow opening E2 Inflow opening Ex Inflow opening G Connection straight line, straight line LE Plane L1 Longitudinal axis of S1 L2 Longitudinal axis of S2 Q Profile of 2 QA Outflow profile QE Inflow profile QF Outflow area S1 Flow guide element S2 Flow guide element S3 Flow guide element Sy Symmetry axis T Exhaust gas stream T1 Partial stream of exhaust gas stream T2 Partial stream of exhaust gas stream T3 Partial stream of exhaust gas stream T4 Partial stream of exhaust gas stream W1 Wall section W2 Wall section Xa Outflow profile of total Ax Xe Inflow profile of total Ex Z1 Intermediate wall Z2 Intermediate wall Angle