Exhaust aftertreatment system having mixer assembly
10711677 ยท 2020-07-14
Assignee
Inventors
- Lawrence J. Noren, IV (Springport, MI, US)
- Daniel J. Owen (Parma, MI, US)
- Jeffrey W. Denton (Jackson, MI, US)
- Attila KOVACS (Karlsruhe, DE)
- Eric A. Hein (Neustadt an der Weinstrasse, DE)
- Meng-Huang Lu (Ann Arbor, MI, US)
- Manoj K. Sampath (Ann Arbor, MI, US)
Cpc classification
B01F2025/931
PERFORMING OPERATIONS; TRANSPORTING
F01N2470/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/10
PERFORMING OPERATIONS; TRANSPORTING
F01N3/2892
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/4521
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
International classification
F01N3/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A mixer assembly for mixing an injected reductant with an exhaust gas output from a combustion engine comprises a mixer housing including a wall defining an exhaust passageway having a longitudinal axis. A tubular swirling device housing extends along a first axis substantially transverse to the longitudinal axis. The tubular swirling device includes a plurality of openings through which exhaust gas enters. The exhaust gas within the tubular swirling device swirls about the first axis and exits at an outlet end of the tubular swirling device. A mixing plate is positioned immediately downstream of the tubular swirling device. The mixing plate swirls the exhaust about a second axis extending parallel to the longitudinal axis.
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 enters the housing; a diversion plate positioned within the housing downstream of the exhaust gas inlet and the reductant inlet and being intersected by the longitudinal axis, the diversion plate urging a first portion of the exhaust gas in a first transverse direction and a second portion of the exhaust gas in a second and opposite transverse direction, wherein the first and second portions of the exhaust gas are urged toward the reductant inlet; and a mixing plate positioned within the housing immediately downstream of the diversion plate, the mixing plate including a surface shaped to swirl the exhaust gas and the reductant about an axis extending parallel to the longitudinal axis.
2. The mixer assembly of claim 1, further including a shield fixed to the diversion plate to block the exhaust gas from directly flowing toward the injected reductant.
3. The mixer assembly of claim 2, wherein the shield is fixed to an outer wall of the housing.
4. The mixer assembly of claim 1, wherein the mixing plate includes apertures of different size and shape to allow mixed exhaust gas and injected reductant to pass therethrough.
5. The mixer assembly of claim 1, further including an injector mount fixed to an outer wall of the housing and the reductant inlet.
6. The mixer assembly of claim 1, wherein the reductant inlet is positioned on a side of the tubular housing.
7. 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; an upstream mixing element including a convex portion positioned between a first recess and a second recess, the recesses being shaped to direct the exhaust gas through apertures extending through the upstream mixing element at positions closer to the reductant inlet than an opposite side of the tubular housing, wherein a downstream face of upstream mixing element at least partially defines a reductant receiving duct that extends transversely across the tubular housing; and a downstream mixing element positioned immediately downstream from the upstream mixing element, the downstream mixing element including an upstream surface at least partially defining the reductant receiving duct, the downstream mixing element including curved surfaces having spaced apart exit ducts supplying mixed exhaust gas and injected reductant to the housing exhaust gas outlet.
8. The mixer assembly of claim 7, wherein the exit ducts are positioned to impart a swirling motion to the exhaust gas.
9. The mixer assembly of claim 7, wherein the downstream mixing element includes apertures of different size, wherein at least one of the apertures is bounded by a louver to change the direction of exhaust gas flow.
Description
DRAWINGS
(1) The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
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(13) Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
DETAILED DESCRIPTION
(14) Example embodiments will now be described more fully with reference to the accompanying drawings.
(15) Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.
(16) The terminology used herein is for the purpose of describing particular example embodiments only and is not intended to be limiting. As used herein, the singular forms a, an, and the may be intended to include the plural forms as well, unless the context clearly indicates otherwise. The terms comprises, comprising, including, and having, are inclusive and therefore specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof. The method steps, processes, and operations described herein are not to be construed as necessarily requiring their performance in the particular order discussed or illustrated, unless specifically identified as an order of performance. It is also to be understood that additional or alternative steps may be employed.
(17) When an element or layer is referred to as being on, engaged to, connected to, or coupled to another element or layer, it may be directly on, engaged, connected or coupled to the other element or layer, or intervening elements or layers may be present. In contrast, when an element is referred to as being directly on, directly engaged to, directly connected to, or directly coupled to another element or layer, there may be no intervening elements or layers present. Other words used to describe the relationship between elements should be interpreted in a like fashion (e.g., between versus directly between, adjacent versus directly adjacent, etc.). As used herein, the term and/or includes any and all combinations of one or more of the associated listed items.
(18) Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as first, second, and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
(19) Spatially relative terms, such as inner, outer, beneath, below, lower, above, upper, and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures. Spatially relative terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as below or beneath other elements or features would then be oriented above the other elements or features. Thus, the example term below can encompass both an orientation of above and below. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.
(20) With reference to
(21) A hydrocarbon (HC) injector 24 may be disposed at least partially within the exhaust gas passageway 14 upstream of the DOC 16. The HC injector 24 may receive hydrocarbon fuel from a fuel source 26 and may inject into the fuel into the stream of exhaust gas upstream of the DOC 16. A burner (not shown) may be disposed at least partially within the exhaust gas passageway 14 upstream of the DOC 16 at or adjacent the HC injector 24. The burner may ignite the fuel injected by the HC injector 24 to regenerate the DOC 16 and/or the filter 18.
(22) A reductant injector 28 may be disposed adjacent to or partially within the mixer assembly 20 upstream of the SCR catalyst 22. The reductant injector 28 may receive a reductant (e.g., urea) from a reductant tank 30 and inject the reductant into an exhaust stream in the mixer assembly 20. As will be described in more detail below, reductant may mix with exhaust gas within the mixer assembly 20 prior to flowing through the SCR catalyst 22.
(23) Referring now to
(24) The injector housing 34 may be an annular member including a flange 46, a generally cylindrical portion 48, and a generally frustoconical portion 50. As shown in
(25) The mixing bowl 36 may be a generally bowl-shaped structure that may be stamped and/or otherwise formed from sheet metal, for example. It will be appreciated that the mixing bowl could be formed by any suitable process and from any suitable material. The mixing bowl 36 may include an upstream end portion 66, a collar portion 68, a step or flange portion 70 and a downstream rim 72 that cooperate to define a mixing chamber 74. The flange portion 70 may be disposed between the upstream end portion 66 and the collar portion 68 and may include the aperture 64 through which the injector housing 34 extends. An outer diametrical surface of the rim 72 can be welded, fastener or pressed into engagement with the inner diametrical surface of the mixer housing 32, for example.
(26) As shown in
(27) As shown in
(28) The first mixing plate 38 may include a plurality of louvers 84 and apertures 86 through which the mixture of reductant and exhaust gas may flow. The second mixing plate 40 may include a plurality of apertures 88 through which the mixture of reductant and exhaust gas may flow. The first and second mixing plates 38, 40 may increase the turbulence of the flow upstream of the SCR catalyst 22 to facilitate further mixing of the exhaust gas and the reductant prior to entering the SR catalyst 22. The mixing plates 38, 40 may also spread the mixture of reductant and exhaust gas over a larger cross-sectional area so that the mixture will flow into the SCR catalyst 22 over a larger cross-sectional area. It will be appreciated that the mixer assembly 20 could include any number of mixing plates and/or static mixers configured in any desired manner. In some embodiments, the contours of the mixing bowl and/or the shape and position of one or more mixing plates 38, 40 may direct the mixture of exhaust gas and reductant away from a lower portion (from the frame of reference of
(29) While the mixer assembly 20 is described above as mixing exhaust gas with reductant from the reductant injector 28 and providing the mixture to the SCR catalyst 22, it will be appreciated that the mixer assembly 20 could be used in conjunction with the HC injector 24 rather than the reductant injector 28. That is, the mixer assembly 20 could be provided upstream of the DOC 16, and the HC injector 24 could inject fuel into the injector housing 34 and mixing chamber 74 to be mixed with the exhaust gas prior to being ignited.
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(31) Additionally or alternatively, apertures and louvers could be formed in the exterior surface 76 between the recesses 82. Additionally or alternatively, one or more bypass apertures or passages could be formed in the mixing bowl 36 at or near the aperture 64 and/or at or near the rim 72 so that relatively small amounts of exhaust gas can bypass the injector housing 34. Additionally or alternatively, one or more bypass apertures or passages could be formed in the inner diametrical surface of the mixer housing 32 so that relatively small amounts of exhaust gas can bypass the injector housing 34 and the mixing chamber 74.
(32) While the mixer assemblies 20 shown in
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(35) Mixing bowl 236 is substantially similar to previously described mixing bowl 236 and the alternate configurations depicted in
(36) First mixing plate 238 includes a stepped shape when viewed from the side such that a first portion 243 is positioned axially closer to injector housing 234 than a second portion 245. An intermediate portion 251 interconnects first portion 243 and second portion 245. Intermediate portion 251 is spaced apart from a collar portion 268 of mixing bowl 236 to define a pinch point or orifice therebetween. The orifice generates a region of increased gas velocity to entrain the smaller droplets of reductant and urge these droplets toward second portion 245 positioned on the same side of pipe as the injector. First portion 243 includes a plurality of louvers 284 and apertures 286 through which the mixture of reductant and exhaust gas may flow. Second portion 245 includes a plurality of substantially cylindrically-shaped apertures 249 provided to allow reductant and exhaust gas to flow therethrough. Louvers 284 are substantially crescent shaped and arranged in an arc to create a swirling exhaust gas motion. As larger droplets of reductant attempt to increase their distance from the injector, the swirling exhaust gas pattern generated by louvers 284 urges the droplets toward the injector such that they evaporate near the center of the pipe 232.
(37) Second mixing plate 240 may include a plurality of apertures 288 through which the mixture of reductant and exhaust gas may flow. The shape, size, and position of various apertures 288 are defined to further mix the exhaust gas and reductant prior to entering a downstream catalyst. Mixing plates 238, 240 may distribute the mixture of reductant and exhaust gas over a desired inlet area of the downstream catalyst to optimize efficiency of catalyst operation.
(38) The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.