Mixing device
11466606 · 2022-10-11
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
F01N3/206
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
B01F23/21
PERFORMING OPERATIONS; TRANSPORTING
B01F25/31
PERFORMING OPERATIONS; TRANSPORTING
F01N3/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/42
PERFORMING OPERATIONS; TRANSPORTING
B01F25/43
PERFORMING OPERATIONS; TRANSPORTING
F01N3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F23/213
PERFORMING OPERATIONS; TRANSPORTING
B01F25/314
PERFORMING OPERATIONS; TRANSPORTING
B01F25/421
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A mixer assembly for mixing an injected reductant with an exhaust gas comprises a tubular housing including a reductant inlet, an exhaust gas inlet and an exhaust gas outlet. The reductant inlet is positioned on a first side of the tubular housing and oriented to direct injected reductant along an injection access that extends transversely to a longitudinal axis. A first flow guide element is shaped as a sheet including a first aperture extending therethrough as well as a surface facing upstream. Exhaust gas flowing through the first aperture is impinged by the injected redundant. A second flow guide element is shaped as a sheet, positioned downstream from the first flow guide element and fixed to the first flow guide element to define a mixing chamber between the first flow guide element and the second flow guide element in which the injected redundant and the exhaust gas mix.
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 flows through the housing, wherein the reductant inlet is positioned on a first side of the tubular housing and oriented to direct injected reductant along an injection axis that extends transversely to the longitudinal axis; a first flow guide element extending across the tubular housing to block a portion of the cross-sectional area of the exhaust gas inlet, the first flow guide element including a first aperture extending therethrough as well as a surface facing upstream, the first flow guide element being positioned upstream from the reductant inlet such that exhaust gas flowing through the first aperture is impinged by the injected reductant; a second flow guide element being positioned downstream from the first flow guide element and directly fixed to the first flow guide element to define a mixing chamber between the first flow guide element and the second flow guide element in which the injected reductant and the exhaust gas mix, the first aperture being positioned on the same side of the tubular housing as the reductant inlet; and an intermediate wall integrally formed with one of the first flow guide element and the second flow guide element, wherein the other of the first flow guide element and the second flow guide element is fixed to the intermediate wall.
2. The mixer assembly of claim 1, wherein the mixing chamber is open in an area of an outer circumference of the tubular housing for receiving injected reductant at the reductant inlet.
3. The mixer assembly of claim 1, wherein the surface facing upstream is convex.
4. The mixer assembly of claim 1, wherein the first flow guide element is formed as a monolithic one-piece metal panel and the second flow guide element is formed as a monolithic one-piece metal panel.
5. The mixer assembly of claim 1, wherein the first flow guide element includes a second aperture spaced apart from the first aperture, the first and second spaced apart apertures each being positioned on the same side of the tubular housing as the reductant inlet and on opposite sides of the injection axis.
6. The mixer assembly of claim 5, wherein exhaust gas flows through the second aperture and the exhaust gas is impinged by the injected reductant.
7. The mixer assembly of claim 1, wherein the second flow guide element defines first and second spaced apart exhaust gas outlets positioned on an opposite side of the tubular housing as the reductant inlet and on opposite sides of the injection axis.
8. The mixer assembly of claim 7, wherein the exhaust gas upstream of the first flow guide element flows parallel to the longitudinal axis of the tubular housing and is redirected to flow at an angle to the longitudinal axis as the exhaust gas enters the mixing chamber and is redirected again to flow through the first and second spaced apart exhaust gas outlets in opposite circumferential directions.
9. The mixer assembly of claim 7, wherein the exhaust gas exiting the mixer through the first and second spaced apart exhaust gas outlets is separated into two divided exhaust streams.
10. The mixer assembly of claim 9, wherein the two divided exhaust streams swirl in opposite directions to one another.
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:
(2)
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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 α 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
(20)
(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.
(24)
(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 α Angle