Mixing Device
20190211732 ยท 2019-07-11
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
F01N3/206
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2260/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2892
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/4233
PERFORMING OPERATIONS; TRANSPORTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F01N2610/02
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
B01F25/3141
PERFORMING OPERATIONS; TRANSPORTING
F01N3/0253
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01N3/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A mixer assembly comprises a tubular housing including a reductant inlet, an exhaust gas inlet and an exhaust gas outlet. The tubular housing defines a longitudinal axis along which exhaust enters the housing. The reductant inlet is positioned on a first side of the tubular housing. An upstream element covers approximately one-half of the cross sectional area of the enhaust gas inlet and is positioned upstream of the reductant inlet. An upstream surface of the upstream mixing element directs exhaust gas flow transversly toward the reductant inlet. A downstream mixing element along with the upstream mixing element at least partially defines a reductant receiving duct in which injected reductant and exhaust gas mix.
Claims
1-15. (canceled)
16. 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 enters the housing, wherein the reductant inlet is positioned on a first side of the tubular housing; an upstream mixing element covering approximately one-half of the cross-sectional area of the exhaust gas inlet, wherein the upstream mixing element is positioned upstream from the reductant inlet, wherein an upstream surface of the upstream mixing element directs the exhaust gas flow transversely across the tubular housing toward the reductant inlet; and a downstream mixing element positioned 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 duct in which the injected reductant and the exhaust gas mix.
17. The mixer assembly of claim 16, wherein a surface of the upstream mixing element or the downstream mixing element that is positioned downstream from the upstream surface of the upstream mixing device includes a divider to split the exhaust gas into two divided flow streams.
18. The mixer assembly of claim 17, wherein the two divided flow streams swirl in opposite directions to one another.
19. The mixer assembly of claim 18, wherein the injected reductant impacts the two divided flow streams.
20. The mixer assembly of claim 17, wherein the divider is intersected by an axis along which the reductant is injected.
21. The mixer assembly of claim 16, wherein the downstream mixing element urges the exhaust gas to flow radially in a direction away from the reductant inlet.
22. The mixer assembly of claim 16, wherein the downstream mixing element covers approximately one-half of the cross-sectional area of the tubular housing.
23. The mixer assembly of claim 16, wherein the reductant receiving duct is shaped to impart a swirling motion on the mixed injected reductant and exhaust gas.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0037] Further advantages and details of the invention are explained in the patent claims and in the description and figures, in which:
[0038]
[0039]
[0040]
[0041]
[0042]
[0043]
[0044]
[0045]
[0046]
DETAILED DESCRIPTION OF THE INVENTION
[0047] The mixing device 1 shown in
[0048] The outflow side 3.2 of the intermediate wall 3 is according to
[0049] 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.
[0050] As can be seen in
[0051] In the profile view A-A shown in
[0052] In the profile view B-B according to
[0053] According to
[0054] 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.
[0055] According to
[0056]
[0057] 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.
[0058] According to
[0059] 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.
[0060]
[0061] In the exemplary embodiment shown in
LIST OF REFERENCE NUMERALS
[0062] 1 Mixing device [0063] 2 Housing [0064] 2.1 Tubular wall [0065] 2.2 Mid-axis [0066] 2.3 Mixing chamber [0067] 2.4 Bridge between A1, A2 [0068] 2.5 Baffle plate [0069] 2.6 Bridge between E1, E2 [0070] 3 Intermediate wall [0071] 3.1 Inflow side, windward side [0072] 3.2 Off-flow side, lee side [0073] 4.1 Exhaust pipe [0074] 4.2 Exhaust pipe [0075] 5 Feed device [0076] 5.1 Feed nozzle [0077] 6 Mixer, mixer pipe [0078] 6.1 Perforation [0079] 7 Corrugated base [0080] 8 Cone, ramp, flow guide element [0081] 9.1 Blade of Ex [0082] 9.2 Blade of Ax [0083] A1 Outflow opening [0084] A2 Outflow opening [0085] Ax Outflow opening [0086] E1 Inflow opening [0087] E2 Inflow opening [0088] Ex Inflow opening [0089] G Connection straight line, straight line [0090] LE Plane [0091] L1 Longitudinal axis of S1 [0092] L2 Longitudinal axis of S2 [0093] Q Profile of 2 [0094] QA Outflow profile [0095] QE Inflow profile [0096] QF Outflow area [0097] S1 Flow guide element [0098] S2 Flow guide element [0099] S3 Flow guide element [0100] Sy Symmetry axis [0101] T Exhaust gas stream [0102] T1 Partial stream of exhaust gas stream [0103] T2 Partial stream of exhaust gas stream [0104] T3 Partial stream of exhaust gas stream [0105] T4 Partial stream of exhaust gas stream [0106] W1 Wall section [0107] W2 Wall section [0108] Xa Outflow profile of total Ax [0109] Xe Inflow profile of total Ex [0110] Z1 Intermediate wall [0111] Z2 Intermediate wall [0112] Angle