MIXER ASSEMBLY
20230003160 · 2023-01-05
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
F01N3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/432
PERFORMING OPERATIONS; TRANSPORTING
B01F25/43
PERFORMING OPERATIONS; TRANSPORTING
B01F25/421
PERFORMING OPERATIONS; TRANSPORTING
B01F25/42
PERFORMING OPERATIONS; TRANSPORTING
F01N3/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/31
PERFORMING OPERATIONS; TRANSPORTING
B01F23/213
PERFORMING OPERATIONS; TRANSPORTING
B01F23/21
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A mixer comprises a tubular housing defining a longitudinal axis along which exhaust gas flows. Injected reductant flows along an injection axis that extends at a non-parallel angle to the longitudinal axis. A first flow guide element extends across and blocks a portion of the tubular housing and includes a first aperture extending therethrough. The first flow guide element is positioned upstream from the reductant inlet such that exhaust gas flowing through the first aperture is impinged by the reductant. A second flow guide element is positioned downstream from the first flow guide element and fixed to the first flow guide element to define a mixing chamber in which injected reductant and exhaust gas mix. An intermediate wall is integrally formed with one of the first and second flow guide elements. The other of the first and second flow guide elements is fixed to the intermediate wall.
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 gas flows through the housing, wherein the reductant inlet is oriented to direct injected reductant along an injection axis that extends at a non-parallel angle 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 tubular housing, the first flow guide element including a first aperture extending therethrough, 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 fixed to the first flow guide element to define a mixing chamber in which the injected reductant and the exhaust gas mix; 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.
17. The mixer assembly of claim 16, wherein the first flow guide element includes a second aperture spaced apart from the first aperture.
18. The mixer assembly of claim 17, wherein an exhaust gas flowing through the second aperture is directed toward the injected reductant.
19. The mixer assembly of claim 16, wherein the non-parallel angle is substantially 90 degrees.
20. The mixer assembly of claim 16, wherein the second flow guide element includes an exhaust gas outlet positioned downstream from the reductant inlet.
21. The mixer assembly of claim 16, 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.
22. The mixer assembly of claim 16, wherein the exhaust gas upstream of the first flow guide element flows substantially parallel to the longitudinal axis of the tubular housing, wherein the exhaust gas exiting the mixer assembly is separated into two divided exhaust streams.
23. The mixer assembly of claim 22, wherein the two divided exhaust streams swirl in opposite directions to one another.
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 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.
[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
2 Housing
[0063] 2.1 Tubular wall
2.2 Mid-axis
[0064] 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
[0065] 7 Corrugated base
8 Cone, ramp, flow guide element
9.1 Blade of Ex
9.2 Blade of Ax
[0066] 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
[0067] L1 Longitudinal axis of S1
L2 Longitudinal axis of S2
Q Profile of 2
[0068] 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