SYSTEM FOR MIXING A LIQUID SPRAY INTO A GASEOUS FLOW AND EXHAUST AFTERTREATMENT DEVICE COMPRISING SAME

Abstract

The invention pertains to a spray/gas mixer, comprising: a main body having a circumferential wall with a first longitudinal axis (A) and extending from a first end to a second end, the first end defining an inlet opening, the second end defining an outlet opening; a divider baffle inside the interior; a swirl duct within the interior along a second longitudinal axis (B), having one end adjacent to the wall and a second end extending to the divider baffle; an injector orifice at the first end of the swirl duct; a swirl promoting means; and a restrictor arrangement. The swirl promoting means is arranged between the divider baffle and the restrictor arrangement, such that gas passing through the swirl promoting means is swirled around the first longitudinal axis (A) before passing through the restrictor. The restrictor arrangement is disposed between the swirl promoting means and the second end, forcing gas reaching it from an upstream side away from a peripheral region of the interior towards a center axis of the main body.

Claims

1. (canceled)

2. An exhaust aftertreatment system disposed within a conduit having a longitudinal axis, the exhaust aftertreatment system comprising: a divider baffle configured to be disposed within the conduit to separate the conduit into an upstream section and a downstream section, the divider baffle defining an aperture leading between the upstream and downstream sections; a swirl duct disposed in at least the upstream section, the swirl duct leading to the aperture at the divider baffle; and an impact surface disposed in the downstream section, the impact surface extending downstream from the divider baffle and being offset radially inward from an inner surface of the conduit by a gap, the impact surface intersecting a longitudinal axis of the swirl duct, the impact surface defining a plurality of openings leading to the gap.

3. The exhaust aftertreatment system of claim 2, wherein the gap is closed at a location downstream of the plurality of openings.

4. The exhaust aftertreatment system of claim 2, wherein the impact surface extends in parallel with the longitudinal axis of the conduit.

5. The exhaust aftertreatment system of claim 2, wherein the swirl duct extends through the aperture defined in the divider baffle and partially into the downstream section.

6. The exhaust aftertreatment system of claim 2, wherein the plurality of openings defined in the impact surface are disposed in alignment with the aperture defined through the divider baffle.

7. The exhaust aftertreatment system of claim 2, wherein the swirl duct includes louvered openings.

8. The exhaust aftertreatment system of claim 7, wherein the swirl duct has a perforated region offset from the louvered openings, the swirl duct defining perforations at the perforated region.

9. The exhaust aftertreatment system of claim 8, wherein the perforations of the perforated region are divided into two groups separated by oppositely disposed non-perforated sections.

10. The exhaust aftertreatment system of claim 2, further comprising a doser mounting location disposed at a first end of the swirl duct, wherein a second end of the swirl duct is located at the aperture through the divider baffle, the second end of the swirl duct being opposite the first end.

11. The exhaust aftertreatment system of claim 10, further comprising a spray path protection zone disposed at the swirl duct, the spray path protection zone being positioned to align with a nozzle of a doser mounted a the doser mounting location.

12. The exhaust aftertreatment system of claim 11, wherein the spray path protection zone is defined by a plurality of perforations.

13. The exhaust aftertreatment system of claim 12, wherein the perforations are defined by a conduit disposed within the swirl duct.

14. The exhaust aftertreatment system of claim 12, wherein the perforations are defined by the swirl duct.

15. The exhaust aftertreatment system of claim 11, wherein the spray path protection zone is defined by a first plurality of louvers disposed at the swirl duct, the louvers being offset along the swirl duct from a second plurality of louvers.

16. The exhaust aftertreatment system of claim 2, further comprising a restrictor arrangement disposed downstream of the divider baffle.

17. The exhaust aftertreatment system of claim 16, wherein the restrictor arrangement is spaced downstream from the impact surface.

18. The exhaust aftertreatment system of claim 16, further comprising a swirl plate disposed between the divider baffle and the restrictor arrangement.

19. The exhaust aftertreatment system of claim 2, wherein the impact surface is formed by an annular sleeve extending downstream from the divider baffle.

20. The exhaust aftertreatment system of claim 2, further comprising a substrate disposed in the downstream section and downstream of the impact surface.

21. The exhaust aftertreatment system of claim 16, further comprising: a first gas flow pathway extending through the swirl duct, through the aperture of the divider baffle, over the impact surface, towards the substrate; and a second gas flow pathway along the gap and through the openings defined in the impact surface.

Description

BRIEF DESCRIPTION OF THE FIGURES

[0050] These and other features and advantages of embodiments of the present invention will be described in more detail with reference to the attached drawings, in which:

[0051] FIG. 1 illustrates a system for mixing a liquid spray into a gaseous flow according to an embodiment of the present invention.

[0052] FIG. 2 presents an exploded view of the system of FIG. 1;

[0053] FIG. 3 presents a partly cut-away perspective of a variation of the central part of the system according to the present invention;

[0054] FIG. 4 presents a partly cut-away perspective of another embodiment of the system according to the present invention; and

[0055] FIG. 5 presents an exploded view of a divider baffle that may be used in embodiments of the present invention.

[0056] FIG. 6 is a longitudinal cross-sectional view of a second example dosing and mixing assembly including a conduit arrangement defining a spray path protection zone and mixing zone, in accordance with the principles of the present disclosure;

[0057] FIG. 7 is a longitudinal cross-sectional view of a third example dosing and mixing assembly including a swirl duct or conduit arrangement defining a spray path protection zone and mixing zone, in accordance with the principles of the present disclosure;

[0058] FIG. 8 is a longitudinal cross-sectional view of a fourth example dosing and mixing assembly including a conduit arrangement defining a spray path protection zone and mixing zone, in accordance with the principles of the present disclosure;

[0059] FIG. 9 is a perspective view of an alternative swirl duct similar to the swirl duct depicted in FIG. 7, for use in the third example dosing and mixing assembly of FIG. 7;

[0060] FIG. 10 is an axial end view of the swirl duct or first conduit of FIG. 9;

[0061] FIG. 11 is a perspective view of an example swirl duct (or first conduit) suitable for use in the fourth example dosing and mixing assembly, defining a mixing zone and a spray protection zone.

[0062] Throughout the figures, the same reference numerals have been used for the same or like elements.

DETAILED DESCRIPTION OF EMBODIMENTS

[0063] FIG. 1 illustrates a system for mixing a liquid spray into a gaseous flow according to an embodiment of the present invention. The system comprises a main body 100 having a circumferential wall 130 defining an interior 101 for accommodating the gaseous flow, substantially along a longitudinal axis A, in a downstream direction from a first end 110 to a second end 120. The first end 110 defines an inlet opening, and the second end 120 defines an outlet opening. On the side of the outlet opening, a reactive substrate or catalyst 160 may be provided in fluid communication with the interior 101. The circumferential wall 130 may be manufactured by joining to half shells together, for example by welding, to form a cylindrically shaped duct.

[0064] Inside the interior 101, a divider baffle 310 is disposed, effectively dividing the interior 101 into what will hereinafter be called an upstream portion and a downstream portion. Gas may pass from the upstream portion to the downstream portion through at least one orifice provided for that purpose. The divider baffle 310 is preferably arranged inside the interior in such a way that gas can only pass via said at least one orifice, because the interior is otherwise completely sealed off by the divider baffle 310. Most preferably, gas arriving from the upstream side can only pass through some or all of said at least one orifice after passing through a swirl duct 210 described below.

[0065] The swirl duct 210 and the divider baffle 310 may be configured to lead the larger part (e.g. more than 50%, i.e. the majority) of any gas flow reaching it from an upstream side towards a downstream side of said divider baffle 310 through the combination of the swirl duct 210 and the divider baffle 310, thus allowing only a smaller part (e.g. less than 50%, i.e. a minority) of said gas flow to bypass the combination of the swirl duct 210 and the divider baffle 310.

[0066] In the upstream portion, downstream of an optional substrate 165 (e.g. a DPF or DOC substrate), a swirl duct 210 (also referred to as a mixing tube) is disposed within the interior 101 along a second longitudinal axis B. The second longitudinal axis B may be at an angle with the first longitudinal axis A. In particular, the second longitudinal axis may be perpendicular or substantially perpendicular to the first longitudinal axis. More generally, the angle between the second longitudinal axis may also be in the preferred range of 70?-110?, or in the more preferred range of 80?-100?, or in the more preferred range of 85?-95?, which also result in a very compact arrangement.

[0067] The swirl duct 210 causes the exhaust gas to swirl about the second longitudinal axis B. In certain implementations, the swirl duct 210 defines slots through which the exhaust gas enters the swirl duct 210. In certain implementations, the swirl duct 210 includes louvers that direct the exhaust gas through the slots in a swirling flow along a circumferential direction, as described below.

[0068] The swirl duct 210 has a first end adjacent to the circumferential wall 130 and a second end extending to said divider baffle 310, as will be described in more detail below. The term adjacent to is meant to include an arrangement whereby the first end of the swirl duct 210 is in contact with or joined to the circumferential wall 130. In embodiments where an inner sleeve is provided inside the main body 100 (as will be described in more detail below in connection with FIG. 4), the first end of the swirl duct 210 may also be in contact with or joined to the inner sleeve, while still being considered adjacent to the circumferential wall 130. The swirl duct 210 receives the gaseous flow into its interior through openings in its outer wall. The swirl duct may for example be substantially cylindrical or frustoconical in shape. The outer wall of the swirl duct 210 may be provided with multiple protrusions at its second end, preferably in a regular pattern, to result in a castellated or saw-tooth appearance.

[0069] Depending on the arrangement of the openings in the swirl duct 210, the gas may enter from the upstream side and/or from the downstream side (after having been deflected by the divider baffle 320. The openings in the outer wall of the swirl duct 210 may be configured so as to impart a tangential component on the velocity of the gas entering the swirl duct 210, preferably a tangential component leading to a velocity vector at an angle relative to the axis of the swirl duct 210 in the range of 20?-40?, preferably 30?-35?. In view of obtaining that effect, some or all of the openings may be provided with louvers; in a particular embodiment, at least a 300 sector of the circumference does not have louvered openings.

[0070] An injector orifice 180 is disposed at the first end of the swirl duct 210 and configured to receive an injector to spray reactant into the gaseous flow so that the reactant mixes with the gaseous flow in the swirl duct 210. The injector orifice 180 may or may not extend through the circumferential wall 130. In the illustrated example, the injector orifice 180 is part of a doser seat, i.e. a structure that can be welded on the interior surface of the circumferential wall 130.

[0071] In the downstream portion, a restrictor arrangement 170 is disposed within the interior 101 between the divider baffle 310 and the second end 120, the restrictor arrangement 170 forcing gas reaching it from an upstream side away from a peripheral region of the interior 101 towards a center axis of the main body 100. This may be achieved by means of a restrictor arrangement 170 in the shape of a baffle plate that is substantially closed in in its peripheral area while having one or more orifices in its central area.

[0072] A swirl promoting means 320 is arranged between the divider baffle 310 and the restrictor arrangement 170, such that gas passing through the swirl promoting means 320 is swirled around the first longitudinal axis before passing through the restrictor arrangement 170 towards said second end 120. In this manner, the swirl promoting means 320 and the restrictor arrangement 170 cooperate to ensure maximal turbulence of the gaseous flow, and hence maximal mixing of the reactant in the gaseous flow prior to its reaching the reactive substrate or catalyst 160 that may be arranged downstream of the restrictor arrangement 170.

[0073] The swirl promoting means 320 may comprise a baffle plate defining a plurality of scoops, pipes, louvers, or other direction adjusting members.

[0074] One or more sheet metal surfaces (not illustrated) may be arranged so as to be substantially surrounded by a gaseous flow entering through said inlet opening 110, wherein the injector orifice 180 is configured so that an injection axis of any injector mounted therein intersects the one or more sheet metal surfaces. The one or more sheet metal surfaces may comprise a perforated plate 191 and a solid plate 192.

[0075] FIG. 2 presents an exploded view of the system of FIG. 1, without the main body 130. As can be seen in this figure, the axis of the swirl duct 210 (i.e., the second longitudinal axis B) coincides with an opening in a step portion of the divider baffle 310. In the assembled position, the second end of the swirl duct 210 extends to said divider baffle 310, so as to lead gas from the inside of the swirl duct 210 through the divider baffle 310 towards the downstream portion of the system 100. The second end of the swirl duct 210 may extend through the opening in the divider baffle 310. Alternatively, the second end of the swirl duct 210 may abut the step portion of the divider baffle 310, surrounding the opening. As a further alternative, a small gap may remain between the second end of the swirl duct 210 and the step portion of the divider baffle 310.

[0076] FIG. 3 presents a partly cut-away perspective of a variation of the central part of the system according to the present invention. As the point of view is from above (as referring to the orientation of the system in FIGS. 1 and 2), the illustrated portion of the illustrated elements corresponds to the lower portion. In this embodiment, the swirl duct 210 is a louvered tube that extends into an opening in the step portion of the divider baffle 310. The swirl promoting means 320 and the restrictor arrangement 170 are arranged downstream of the divider baffle 310. The embodiment of FIG. 3 is illustrative of the optional feature that a portion of the divider baffle 310 is shaped so as to be in contact with the swirl duct 210, thus forcing a larger portion of the gas flow into the swirl duct 210 by blocking flow around the swirl duct 210.

[0077] FIG. 4 presents a partly cut-away perspective of another embodiment of the system according to the present invention. In this embodiment, the system further comprises an inner sleeve 135 having an upstream end and a downstream end, whereby the upstream end is circumferentially joined to the divider baffle 310 and the downstream end is circumferentially joined to the swirl promoting means 320 or the restrictor arrangement 170 so as to leave an annular space between the inner sleeve and the circumferential wall 130. Preferably, the inner sleeve 135 is provided with at least one opening 139 ensuring fluid communication between the annular space and an inner volume enclosed by the inner sleeve 135. Thus, gas can flow both inside and around the sleeve (i.e., in the annular space between the circumferential wall 130 and the inner sleeve 135).

[0078] Optionally, at least one opening is disposed in the inner sleeve 135 in an area to be impacted by the reactant (as in the illustrated case, where the axis of the injector coincides with the longitudinal axis B of the swirl duct 210, which intersects the region provided with openings 139). Suitably arranged openings in the sleeve may thus provide a thermally stabilized grate (by convection) towards which the reactant is sprayed, thus providing a surface less prone to accumulation of solid reactant deposits than if the spray were directed to the inside of the circumferential wall 130. In the illustrated case, the swirl duct 210 (louvered tube) does not extend through the circumferential wall 130. In the illustrated case, the point of injection for the reactant spray lies inside mixer housing, so the injector orifice 180 does not extend through the outside wall. In this manner, the system can be made more compact.

[0079] FIG. 5 presents an exploded view of a divider baffle 310 that may be used in embodiments of the present invention. As shown in the figure, the divider baffle 310 may be constructed from multiple separate baffle portions. The bottom portion may consist of a suitably bent and perforated first plate-like element. The top portion may consist of a suitably bent second plate-like element. The separate baffle portions may be joined together in a fixed relationship. Alternatively, the separate baffle portions may retain a fixed relationship by virtue of being attached to a common structure.

[0080] In an alternative configuration (not shown in FIG. 5), the divider baffle 310 may be of a single piece, in particular it may be produced as a single suitably bent and perforated plate-like element.

[0081] Referring to FIGS. 6-11 further examples of dosing and mixing assembly are shown and explained, comprising a spray path protection zone.

[0082] The systems depicted in FIGS. 6-8 have been depicted in a schematic way, as they differ from the systems described in relation to FIGS. 1 and 4 only in that the swirl duct comprises a spray path protection zone. The variations with a spray path protection zone can be used in embodiments with and without the presence of an inner sleeve 135. Also, the restrictor arrangement 170 is not shown in detail.

[0083] Referring to FIG. 6, a second example dosing and mixing assembly is shown. In preferred embodiments, the spray path protection zone comprises a perforated conduit disposed within the swirl duct/first conduit adjacent to the injector orifice.

[0084] The spray protection zone comprises a perforated conduit 400 or spray path protector 400 disposed within the first conduit/swirl duct 210 at the injector orifice or injector mounting location 180. The spray path protector is positioned to surround a nozzle of the injector doser 500 disposed at the injector orifice 180. The spray protector 400 inhibits flow entering the first conduit 210 from opening the spray path of the reactant too quickly. In certain examples, the spray protector 400 blocks at least some of the swirling flow from reaching the nozzle of the doser 500. In certain examples, the spray protector 400 reduces swirling and/or other large-scale turbulence in exhaust flow that reaches the nozzle of the doser 500.

[0085] In certain implementations, the spray protector 400 includes a perforated conduit. The perforations of the spray protector 400 are sized to mitigate turbulence of exhaust passing through the perforations. In certain examples, each perforation has a cross-dimension (e.g., a diameter) of less than about 5 mm. In certain examples, each perforation has a cross-dimension of less than about 4 mm. In certain examples, each perforation has a cross-dimension of about 3 mm. In certain examples, each perforation has a cross-dimension of less than about 3 mm. In certain examples, each perforation has a cross-dimension of between 2 and 4 mm. In certain examples, each perforation has a cross-dimension of between 2.5 and 3.5 mm.

[0086] In some implementations, the perforated conduit 400 is cylindrical. In other implementations, the perforated conduit 400 can have other shapes. In certain implementations, the perforations of the spray protector 400 extend over at least a majority of a circumference of the perforated conduit. In certain examples, the perforations extend over the full circumference. In other examples, the perforated conduit may define one or more non-perforated circumferential sections. In certain examples, the perforated conduit defines two oppositely disposed non-perforated circumferential sections. In an example, a non-perforated circumferential section faces towards the inlet.

[0087] In some implementations, the perforated conduit is mounted to a doser mount that also holds the doser at the doser mounting location. In other implementations, the perforated conduit is mounted to the first conduit. In certain examples, the perforated conduit 400 extends partially across the swirl duct 210. In certain examples, the perforated conduit extends across less than a majority of an axial length of the swirl duct. In certain examples, the perforated conduit extends across between 25% and 50% of the swirl duct. In preferred embodiments, the perforated conduit is arranged concentrically with the swirl duct.

[0088] As described for FIG. 1 and FIG. 4, the swirl duct further comprises a mixing portion 420 or mixer comprising a first set of louvers 42.

[0089] Referring to FIG. 7, a third example dosing and mixing assembly is shown. the spray path protection zone comprises a protection portion of the swirl duct adjacent to the injector orifice, the protection portion comprising perforations.

[0090] The first conduit/swirl duct defines a spray path protection zone upstream of the mixing portion. The flow path protection zone is disposed at the doser mounting location/injector orifice to facilitate flow of reactant from the doser 500 without prematurely opening the spray path of the reactant from the doser. Opening the spray path too quickly can lead to deposits of the reactant, which can result in build-up of deposits and blockage of the exhaust flow within the system. For example, swirling exhaust flow around the reactant injection site can push reactant radially outwardly from the spray path towards the inner surface of the first conduit/swirl duct, thereby leading to deposition of reactant on the louvers of the mixing portion or around the nozzle of the doser.

[0091] In certain implementations, the protection zone is defined by a perforated region 401 of the first conduit/swirl duct 210 disposed between the injector mounting location and the mixing portion of the swirl duct 210. The perforations at the perforated region do not impart swirling onto exhaust entering the first conduit through the perforations. In certain examples, the perforations mitigate any swirling that was imparted on the exhaust (e.g., from the exhaust moving around the exterior of the first conduit) prior to the exhaust entering through the perforations. In certain examples, the perforations mitigate any large scale turbulence that was imparted on the exhaust prior to the exhaust passing through the perforations.

[0092] In certain implementations, the perforations of the perforated region are sized to inhibit swirling and/or other turbulence of the exhaust passing through the perforations. In certain examples, each perforation has a cross-dimension (e.g., a diameter) of less than about 5 mm. In certain examples, each perforation has a cross-dimension of less than about 4 mm. In certain examples, each perforation has a cross-dimension of about 3 mm. In certain examples, each perforation has a cross-dimension of less than about 3 mm. In certain examples, each perforation has a cross-dimension of between 2 and 4 mm. In certain examples, each perforation has a cross-dimension of between 2.5 and 3.5 mm.

[0093] As shown in FIG. 9, the perforations of the perforated region extend over at least a majority of the circumference of the first conduit 210. In certain examples, the perforations of the perforated region 401 may extend over a full circumference of the first conduit. In other examples, the perforations extend over less than a majority of the circumference of the first conduit. In certain implementations, the perforated region 360 includes one or more non-perforated sections (i.e., a circumferential section of the first conduit in which the adjacent perforations bounding the section are circumferentially spaced further from each other compared to the remainder of the adjacent perforations of the perforated region). In certain examples, the perforations of the perforated region 401 are divided into two groups separated by oppositely disposed non-perforated sections 4011, 4012. The inclusion of oppositely disposed non-perforated sections results in symmetrical flow through the protection zone. In certain examples, the non-perforated sections align with non-louvered sections 4201, 4202 of the mixing region/portion 420 comprising a first set of louvers 42.

[0094] According to preferred embodiments, at least some of the exhaust flow from the inlet enters the first conduit 210 through the perforated region 401 instead of through the mixing portion. In certain implementations, less flow enters through the perforated region 401 than through the mixing portion 420. In certain implementations, at least 15% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401. In certain implementations, at least 20% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401. In certain implementations, at least 25% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401. In certain implementations, at least 30% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401. In certain implementations, at least 35% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401. In certain implementations, between about 20% and 45% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401. In certain implementations, between about 25% and 40% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401. In certain implementations, between about 30% and 35% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401.

[0095] In certain implementations, no more than 80% of the exhaust from the inlet flows into the first conduit 210 through the mixing portion 420. In certain implementations, no more than 75% of the exhaust from the inlet flows into the first conduit 210 through the mixing portion 420. In certain implementations, no more than 70% of the exhaust from the inlet flows into the first conduit 210 through the mixing portion 420. In certain implementations, no more than 65% of the exhaust from the inlet flows into the first conduit 210 through the mixing portion 420. In certain implementations, no more than 60% of the exhaust from the inlet flows into the first conduit 210 through the mixing portion 420. In certain implementations, no more than 55% of the exhaust from the inlet flows into the first conduit 210 through the mixing portion 420. In certain implementations, between about 45% and 70% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401. In certain implementations, between about 55% and 65% of the exhaust from the inlet flows into the first conduit 210 through the perforated region 401.

[0096] The exhaust flow entering through the perforated region 401 carries the reactant towards the mixing portion with minimal effect on the spray path. The flow entering the first conduit 210 through the mixing portion initially swirls around the low or non-swirling flow from the perforated region 401. The flow from the mixing region 420 mixes with the exhaust flow from the perforated region 401 as the flows progress downstream through the first conduit 210, thereby creating a swirling flow of exhaust and reactant within the first conduit 210 downstream of the mixing region 420.

[0097] Referring to FIGS. 8 and 11, a fourth example dosing and mixing assembly is shown. The first conduit/swirl duct 210 defines a spray path protection zone upstream of the mixer portion on the swirl duct 210 (see FIG. 7). The spray path protection zone is disposed between the mixing portion 420 and the doser mounting location/injector orifice 180 to facilitate flow of reactant from the doser without prematurely opening the spray path of the reactant from the doser. Opening the spray path too quickly can lead to deposits of the reactant, which can result in build-up of deposits and blockage of the exhaust flow within the system. For example, swirling exhaust flow around the reactant injection site can push reactant radially outwardly from the spray path towards the inner surface of the first conduit 210, thereby leading to deposition of reactant on the louvers of the mixer portion 420 or around the nozzle of the doser.

[0098] In certain implementations, the protection zone is defined by a louvered section 402 of the swirl duct, comprising louvers 40, located upstream from the mixing portion/section 420. The louvered section is configured to impart swirl in an opposite direction than the mixing portion 420. A first part of the exhaust flow from the inlet will enter the first conduit 210 through the louvered section 402 while a second part of the exhaust flow from the inlet will enter the first conduit 210 through the mixing portion/mixer 420. The louvered section 402 will impart swirling in a first direction to the first part of the exhaust while the mixing portion 420 will impart swirling in a second, opposite direction to the second part of the exhaust. The interaction between these two swirling flows at the upstream end of the mixing portion 420 initially inhibits the swirling imparted by the mixing portion 420, thereby reducing the effect the mixing portion has on the spray path of the reactant dispensed from the injector doser.

[0099] In certain implementations, the louvers of the louvered section 402 are smaller (e.g., shorter along the conduit axis L) compared to the louvers of the mixing portion 420. Accordingly, less flow enters through the louvered section 402 than through the mixer 420. In certain implementations, the axial length (along the conduit axis L) of the louvers is less than half of the axial length of the mixer louvers. In certain implementations, the axial length of the louvers is between 10% and 40% of the axial length of the mixer louvers. In certain implementations, the axial length of the louvers is between 10% and 25% of the axial length of the mixer louvers. In certain implementations, the axial length of the louvers is between 15% and 20% of the axial length of the mixer louvers. In certain implementations, the total open area provided by the louvered section 402 is between about 15% and 55% of the total open area provided by the mixer/mixing portion. In certain examples, the total open area provided by the louvered section 402 is between about 25% and 45% of the total open area provided by the mixer/mixing portion.

[0100] The present invention also pertains to an exhaust treatment device for treating exhaust comprising the system for mixing a liquid spray into a gaseous flow described above, wherein an aftertreatment substrate is disposed downstream of the outlet 120, and wherein said the inlet 110 is adapted to receive an exhaust flow of an internal combustion engine.

[0101] The present invention also pertains to a motor vehicle comprising the exhaust treatment device described above.

[0102] The present invention also pertains to a motor-powered machine, in particular a diesel-powered motor vehicle, comprising the exhaust treatment device described above, arranged for the purpose of treating the exhaust produced by the vehicle's internal combustion engine.

[0103] While the invention has been described hereinabove with reference to particular embodiments, this was done to clarify and not to limit the invention, the scope of which is to be determined by reference to the accompanying claims. In particular, variations and elements which have only been described in the context of a particular embodiment, may be combined with the features of other embodiments to obtain the same technical effects.