• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    Arrangement for introducing a liquid medium into exhaust gases from a combustion engine: an exhaust gas line (2), an injection chamber (3) bounded in radial directions by a tubular wall (8), an injector (13) injects the liquid medium into the injection chamber; a mixing duct (14) to which the injection chamber has an outlet (10) for delivering exhaust gases; a bypass duct (15) which has an outlet (17) via which it is connected to the mixing duct, and an endwall (7) at the injection chamber's downstream end and demarcating the chamber from the mixing duct, such that the chamber's outlet is situated at the periphery of the endwall. The outlet of the bypass duct is close to the outlet of the injection chamber so that the exhaust gases which flow into the mixing duct via the chamber's outlet will collide with the exhaust gases which flow into the mixing duct via the outlet of the bypass duct.
    公开号:SE1051099A1
    申请号:SE1051099
    申请日:2010-10-22
    公开日:2012-04-23
    发明作者:Peter Loman
    申请人:Scania Cv Abp；
    IPC主号:
    专利说明:

    When urea is used as a reducing agent, it is injected into the exhaust line in the form of a liquid urea solution by means of an injection means. The injection means comprises a nozzle via which the urea solution under pressure is injected into the exhaust line in atomized form as a spray. During large parts of a diesel engine's operating condition, the exhaust gases have a sufficiently high temperature to be able to evaporate the urea solution so that ammonia is formed. However, it is difficult to avoid that part of the added urea solution comes into contact with and adheres to the inner wall surface of the exhaust line in an undisturbed state. When an internal combustion engine is operated in a uniform manner over a period of time, i.e. under a stationary operating condition, no appreciable variations of the exhaust gas flow occur and the urea solution injected into the exhaust gases will therefore hit substantially the same area of the exhaust line during this entire period. Under the action of the relatively cool urea solution, the temperature can be lowered locally in this area of the exhaust line to a temperature lower than 100 ° C, which in turn can lead to the formation of a film of urea solution in this area which is then drawn with of the exhaust gas flow. After this film has been moved a certain distance in the exhaust line, the water in the urea solution will boil away under the action of the hot exhaust gases.
    What remains is solid urea which is slowly evaporated by the heat in the exhaust line. If the supply of solid urea is greater than the evaporation, a solid urea accumulates in the exhaust line. If the layer of urea becomes sufficiently thick, the urea and its decomposition products will react with each other to form primitive polymers on urea base, so-called urea lumps. Such lumps of urea can eventually block an exhaust line.
    In order to facilitate the evaporation of the injected urea solution, an evaporation means can be arranged in the exhaust line downstream of the injection site. This evaporating means can in its simplest form consist of a metal plate heated by the exhaust gases, on which reducing agent droplets are intended to adhere and evaporate. The evaporator may comprise catalytic material to accelerate the evaporation of the reducing agent or lack such material.
    OBJECT OF THE INVENTION The object of the present invention is to provide a further development of an arrangement of the type described above in order to provide an arrangement with a design which in at least some aspect offers an advantage over this.
    SUMMARY OF THE INVENTION According to the present invention, said object is achieved by means of an arrangement having the features defined in claim 1.
    The arrangement according to the invention comprises: - a line intended to be flowed through by exhaust gases, - an injection chamber with an upstream end and a downstream end, the injection chamber being delimited in the radial direction of a tubular wall and at its upstream end having an inlet for receiving - an injection means for injecting the liquid medium into the injection chamber, - a mixing channel included in the line, which is arranged downstream of the injection chamber, the injection chamber having at its downstream end an outlet for discharging exhaust gases to the mixing channel, and - a bypass channel; in the line upstream of the mixing channel and has an outlet, via which the bypass channel is connected to the mixing channel. The inlet of the injection chamber is arranged to divert a part of the exhaust gases flowing through the line to allow these diverted exhaust gases to flow into the injection chamber and then into the mixing channel via the outlet of the injection chamber, while the bypass channel is arranged to pass another part of the exhaust gases through the line. into the mixing duct to be mixed there with said derived exhaust gases. At its downstream end, the injection chamber has an end wall, the injection chamber being delimited from the mixing channel by this end wall and the outlet of the injection chamber being arranged at the periphery of the end wall. Furthermore, the outlet of the bypass duct is arranged in the vicinity of the outlet of the injection chamber in such a way that the exhaust gases flowing into the mixing duct via the outlet of the injection chamber will collide with the exhaust gases flowing into the mixing duct via the outlet of the bypass duct.
    Drops of the injected liquid medium which have not hit the tubular wall of the injection chamber and which have not evaporated on their passage through the injection chamber will hit the end wall at the downstream end of the injection chamber. A part of the liquid medium which hits the end wall will evaporate under the action of the hot exhaust gases, while the remaining part of this liquid medium, i.e. the part which does not have time to evaporate after hitting the end wall, flows along the end wall to finally swept along by the exhaust gas flow out through the injection chamber outlet. In the mixing duct, this exhaust gas flow collides with the exhaust gas flow from the bypass duct outlet. A turbulent flow occurs where these exhaust gases collide with each other, which helps to disperse the liquid medium in the exhaust gases. The turbulent flow also helps to break up the droplets of the liquid medium into smaller droplets that evaporate faster.
    According to an embodiment of the invention, the bypass channel surrounds the injection chamber and is delimited therefrom by the tubular wall of the injection chamber. The exhaust gases flowing through the bypass duct will give off heat to this tubular wall, the inside of which forms an internal wall surface of the injection chamber. This counteracts a cooling of this inner wall surface of the injection chamber, which in turn prevents the injected medium from sticking to this inner wall surface without evaporating.
    According to another embodiment of the invention, the exhaust gases from the bypass duct are arranged to flow into the mixing duct in a substantially radial direction towards the center axis of the mixing duct via the outlet of the bypass duct, while the exhaust gases from the injection chamber are arranged to flow into the mixing duct substantially outlet. As a result, the exhaust gas flow from the outlet of the injection chamber collides at a steep angle with the exhaust gas flow from the outlet of the bypass duct, which contributes to a very turbulent flow where these exhaust gas flows collide with each other.
    According to another embodiment of the invention, the outlet of the injection chamber is designed to restrict the exhaust gas flow so that the exhaust gases flowing through the injection chamber are subjected to an acceleration during their passage through this outlet. This ensures a high velocity of the exhaust gas flow from the outlet of the injection chamber, which contributes to a very turbulent flow where this exhaust gas flow collides with the exhaust gas flow from the outlet of the bypass duct. Due to their mass, the droplets of the liquid medium show a greater inertia than the surrounding exhaust gases, which means that the exhaust gases are accelerated faster than the droplets when passing through the outlet of the injection chamber and thereby temporarily obtain a higher speed than the droplets. This obtained velocity difference between the exhaust gases and said droplets helps to decompose the droplets into smaller droplets which evaporate faster. The speed difference also contributes to increased transfer of heat from the exhaust gases to the droplets.
    According to another embodiment of the invention, the outlet of the bypass duct is designed to restrict the exhaust gas flow so that the exhaust gases flowing through the bypass duct are subjected to an acceleration during their passage through this outlet. This ensures a high speed of the exhaust gas flow from the bypass duct outlet, which contributes to a very turbulent flow where this exhaust gas flow collides with the exhaust gas flow from the injection chamber outlet.
    According to another embodiment of the invention, the side of the end wall facing the injection chamber has a convex shape. As a result, the liquid medium hitting the end wall will be pressed radially outwards in the direction of the periphery of the end wall and thereby in the direction of the outlet of the injection chamber of the exhaust gas flow towards the end wall.
    Other advantageous features of the arrangement according to the invention appear from the dependent claims and the following description.
    BRIEF DESCRIPTION OF THE DRAWING The invention will be described in more detail below with the aid of exemplary embodiments, with reference to the accompanying drawing.
    It is shown in: Fig. 1 a schematic longitudinal section through an arrangement according to an embodiment of the present invention.
    DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION Fig. 1 illustrates an arrangement 1 according to the present invention for introducing a liquid medium into exhaust gases from an internal combustion engine. The arrangement may, for example, be arranged in an exhaust line upstream of an SCR catalyst for introducing a liquid reducing agent in the form of urea or ammonia into the exhaust line upstream of the SCR catalyst, or be arranged in an exhaust aftertreatment device for introducing a liquid reducing agent into the form of a liquid reducing agent. or ammonia upstream of an SCR catalyst included in the exhaust aftertreatment device.
    The arrangement 1 comprises a line 2 which is intended to receive exhaust gases from an internal combustion engine and pass these exhaust gases further in the direction of an exhaust after-treatment unit, for example in the form of an SCR catalyst. The arrangement 1 further comprises an injection chamber 3 with an upstream end 4 and a downstream end 5. The injection chamber 3 is delimited in the axial direction by a first end wall 6 at its upstream end 4 and by a second end wall 7 at its downstream end 5. the injection chamber 3 is further delimited in the radial direction by a tubular wall 8 extending between the upstream end 4 of the injection chamber and the downstream end 5. The injection chamber 3 has an inlet 9 for receiving exhaust gases at its upstream end and an outlet for discharging exhaust gases at its downstream end. The outlet 10 is arranged at the periphery of the second end wall 7, preferably between the periphery of the second end wall and the tubular wall 8. The outlet 10 is suitably annular and arranged to extend around the second end wall 7 and around the central axis 12 of the injection chamber. the inlet 9 is suitably annular and arranged to extend around the central axis 12 of the injection chamber.
    The side of the second end wall 7 facing the injection chamber 3 suitably has a convex shape, as illustrated in Fig. 1. In the illustrated example, the second end wall 7 is cup-shaped.
    An injection means 13 for injecting the liquid medium is arranged in the center of the upstream end 4 of the injection chamber for injecting the liquid medium towards the downstream end 5 of the injection chamber. In the illustrated example, the injection means 13 extends into the injection chamber through said first end wall 6. The injection means 13, which may for instance comprise an injection nozzle, is arranged to inject the liquid medium under pressure into the injection chamber 3 in finely divided form as a spray. The injection chamber 3 is connected via its outlet 10 to a mixing channel 14 included in the line 2, which is arranged downstream of the injection chamber 3. The injection chamber 3 is delimited from the mixing channel 14 by the above-mentioned second end wall 7.
    A bypass duct 15 is provided in the conduit 2 upstream of the mixing duct 14 for guiding exhaust gases into the mixing duct without passage through the injection chamber 3. The bypass duct 15 has an inlet 16 for receiving exhaust gases at its upstream end and an outlet 17 for discharging exhaust gases at its downstream end. Via the outlet 17, the bypass channel 15 is connected to the mixing channel 14. The outlet 17 is suitably annular and arranged to extend around the central axis 18 of the mixing channel.
    In the illustrated example, the bypass channel 15 surrounds the injection chamber 3 and is delimited therefrom by the above-mentioned tubular wall 8, which is arranged between the bypass channel and the injection chamber. The bypass channel surrounds the tubular wall 8 and extends along the outside thereof. In this case, the bypass channel 15 is thus annular, seen in a cross section through the bypass channel. In the illustrated example, the inlet 16 inlet of the bypass duct is annular and arranged externally about the inlet of the injection chamber 9. The inlet 9 of the injection chamber is arranged to divert a part of the exhaust gases flowing through the line 2 to allow these discharged exhaust gases to flow into the injection chamber. the mixing duct 14 via the outlet 10 of the injection chamber, while the bypass duct 15 is arranged to lead another part of the exhaust gases flowing through the line 2 directly into the mixing duct 14 for mixing there with said diverted exhaust gases.
    The spray of liquid medium which is injected into the injection chamber 3 via the injection means 13 comes into the injection chamber 3 in contact with exhaust gases which flow into the injection chamber 9 via the injection chamber inlet in a substantially symmetrical flow around this spray. The exhaust gases flowing into the injection chamber 3 carry the liquid medium downstream into the injection chamber. During its movement downstream in the injection chamber 3, the liquid medium is dispersed into the exhaust gases and a part of it evaporates under the action of the heat of the exhaust gases. Liquid medium which has not evaporated in the injection chamber 3 strikes the end wall 7 at the downstream end of the injection chamber. A part of the liquid medium hitting this end wall 7 will evaporate under the action of the hot exhaust gases, while the remaining part of this liquid medium flows along the end wall 7 to be finally swept away by the exhaust gas flow out through the injection chamber. outlet 10 and further into the mixing channel 14, where the liquid medium is dispersed in the exhaust gases and evaporates under the action of the heat of the exhaust gases.
    The bypass duct outlet 17 is arranged in the vicinity of the inlet chamber outlet 10, just downstream thereof, so that the exhaust gases flowing into the mixing duct 14 via the inlet chamber outlet 10 will collide with the exhaust gases flowing into the mixing duct 14 via the bypass duct outlet 17 forming a turbulent exhaust gas flow in the mixing channel. The geometry adjacent the bypass duct outlet 17 is such that the exhaust gases from the bypass duct 15 are caused to flow into the mixing duct 14 in a substantially radial direction towards the center axis 18 of the mixing duct via the bypass duct outlet 17, and the geometry adjacent the injection chamber 10 is the injection chamber 10. that the exhaust gases from the injection chamber 3 are caused to flow into the mixing channel 14 in a substantially axial direction via the outlet 10 of the injection chamber 10. the outlet chamber 10 is designed to restrict the exhaust flow of the exhaust gases flowing through the injection chamber 3 so that these exhaust gases are subjected to acceleration. its passage through this outlet 10. In addition, the outlet 17 of the bypass duct is designed to restrict the exhaust flow of the exhaust gases flowing through the bypass duct 15 so that these exhaust gases are subjected to an acceleration during their passage through this outlet 17.
    In the embodiment illustrated in Fig. 1, the arrangement 1 comprises a bulging part 20 which extends into the conduit 2 and whose upper side forms the above-mentioned first end wall 6 of the injection chamber 3. Upstream of the inlet of the injection chamber 9 the conduit 2 has an annular space 21 which extends around the bulging part 20. the inlet 9 of the injection chamber and the inlet 16 of the bypass channel are both connected to this annular space 21. In the illustrated example the inlet 9 of the injection chamber is arranged between the bulging part 20 and the tubular wall 8.
    The arrangement according to the invention is particularly intended for use in a heavy motor vehicle, such as for instance a bus, a towing vehicle or a truck.
    The invention is of course in no way limited to the embodiments described above, but a number of possibilities for modifications thereof should be obvious to a person skilled in the art, without this for that reason deviating from the basic idea of the invention as defined in the appended claims. .
    权利要求:
    Claims (6)
    [1]
    Arrangement for introducing a liquid medium, for example urea, into exhaust gases from an internal combustion engine, which arrangement (1) comprises: - a line (2) intended to be passed through by exhaust gases, - a injection chamber (3) with an upstream end (4) and a downstream end (5), the injection chamber being delimited in the radial direction by a tubular wall (8) and having an inlet (9) for receiving exhaust gases at its upstream end, - an injection means (13) for injecting the liquid medium into the injection chamber (3), - a mixing channel (14) included in the line (2), which is arranged downstream of the injection chamber (3), the injection chamber at its downstream end ( 5) has an outlet (10) for discharging exhaust gases to the mixing channel, and - a bypass channel (15) which is arranged in the line (2) upstream of the mixing channel (14) and has an outlet (17), via which the bypass channel is connected to, among others, - ningskana wherein the inlet (9) of the injection chamber is arranged to divert a part of the exhaust gases flowing through the line (2) to allow these discharged exhaust gases to flow into the injection chamber (3) and then into the mixing channel (14) via inlet - the outlet (10) of the spray chamber, while the bypass duct (15) is arranged to lead another part of the exhaust gases flowing through the duct (2) into the mixing duct (14) for mixing therewith with said diverted exhaust gases, characterized therefrom: - that the injection chamber (3) has at its downstream end (5) an end wall (7), the injection chamber being delimited from the mixing channel (14) by this end wall (7), - that the outlet (10) of the injection chamber is arranged at the periphery of said end wall (7), and - that the outlet (17) of the bypass duct is arranged in the vicinity of the outlet (10) of the injection chamber in such a way that the exhaust gases flowing into the mixing duct (14) via the injection chamber outlet (10) will collide with the exhaust gases flowing into the mixing duct (14) via the bypass duct outlet (17).
    [2]
    Arrangement according to claim 1, characterized in that the outlet (10) of the injection chamber is arranged between said tubular wall (8) and the periphery of said end wall (7).
    [3]
    Arrangement according to claim 1 or 2, characterized in that the bypass channel (15) surrounds the injection chamber (3) and is delimited therefrom by said tubular wall (8).
    [4]
    4.. Arrangement according to one of Claims 1 to 3, characterized in that: - the exhaust gases from the bypass duct (15) are arranged to flow into the mixing duct (14) in a substantially radial direction towards the center axis (18) of the mixing duct via the bypass duct (17), and - that the exhaust gases from the injection chamber (3) are arranged to flow into the mixing channel (14) in a substantially axial direction via the outlet (10) of the injection chamber.
    [5]
    Arrangement according to one of Claims 1 to 4, characterized in that the outlet (10) of the injection chamber is designed to restrict the exhaust gas flow so that the exhaust gases flowing through the injection chamber (3) are subjected to an acceleration during their passage through this outlet (10).
    [6]
    Arrangement according to one of Claims 1 to 5, characterized in that the outlet (17) of the bypass duct is designed to restrict the exhaust gas flow so that the exhaust gases flowing through the bypass duct (15) are subjected to an acceleration during their passage through this outlet. (17). Arrangement according to one of Claims 1 to 6, characterized in that the side of the end wall (7) which faces the injection chamber (3) has a convex shape. Arrangement according to one of Claims 1 to 7, characterized in that the outlet (10) of the injection chamber is annular and extends around the end wall (7). . Arrangement according to one of Claims 1 to 8, characterized in that the outlet (17) of the bypass channel is annular and extends around the central axis (18) of the mixing channel. Arrangement according to one of Claims 1 to 9, characterized in that the injection means (13) is arranged in the center of the upstream end (4) of the injection chamber and is arranged to inject the liquid medium in the direction of the downstream end (5) of the injection chamber. Arrangement according to one of Claims 1 to 10, characterized in that the inlet (9) of the injection chamber is annular and extends around the central axis (12) of the injection chamber.
    类似技术:
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    同族专利:
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    CN103168155A|2013-06-19|
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    SE535235C2|2012-06-05|
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    CN103168155B|2015-07-08|
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    US20130305696A1|2013-11-21|
    US8915069B2|2014-12-23|
    EP2630350B1|2017-03-29|
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    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    SE1051099A|SE535235C2|2010-10-22|2010-10-22|Arrangement for introducing a liquid medium into exhaust gases from an internal combustion engine|SE1051099A| SE535235C2|2010-10-22|2010-10-22|Arrangement for introducing a liquid medium into exhaust gases from an internal combustion engine|
    KR1020137013126A| KR20130140028A|2010-10-22|2011-10-13|Arrangement for introducing a liquid medium into exhaust gases from a combustion engine|
    JP2013534857A| JP5650846B2|2010-10-22|2011-10-13|Device for introducing a liquid medium into exhaust gas from a combustion engine|
    EP11834717.8A| EP2630350B1|2010-10-22|2011-10-13|Arrangement for introducing a liquid medium into exhaust gases from a combustion engine|
    BR112013008310A| BR112013008310A2|2010-10-22|2011-10-13|arrangement for introducing a liquid medium into exhaust gases from a combustion engine|
    US13/877,526| US8915069B2|2010-10-22|2011-10-13|Arrangement for introducing a liquid medium into exhaust gases from a combustion engine|
    RU2013123134/06A| RU2536466C1|2010-10-22|2011-10-13|Device for injection of liquid medium into exhaust gases of internal combustion engine|
    CN201180050460.XA| CN103168155B|2010-10-22|2011-10-13|Arrangement for introducing a liquid medium into exhaust gases from a combustion engine|
    PCT/SE2011/051222| WO2012053960A1|2010-10-22|2011-10-13|Arrangement for introducing a liquid medium into exhaust gases from a combustion engine|
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