NITROGEN OXIDES REDUCTION AGENT INJECTION ARRANGEMENT
20240384674 ยท 2024-11-21
Inventors
Cpc classification
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
F01N2560/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2610/1453
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2610/146
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1821
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/208
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1811
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2590/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2240/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A nitrogen oxides reduction agent injection arrangement for injecting a nitrogen oxides reduction agent, such as urea, into an exhaust conduit forming part of an exhaust system for an internal combustion engine system. The nitrogen oxides reduction agent injection arrangement comprises a nozzle that is adapted to inject the nitrogen oxides reduction agent into the interior of the exhaust conduit via a nozzle opening of the nozzle. The nozzle comprises a nozzle opening control portion made of a shape memory material whereby a size and/or a shape of the nozzle opening is dependent on at least a temperature of the nozzle opening control portion.
Claims
1. A nitrogen oxides reduction agent injection arrangement for injecting a nitrogen oxides reduction agent, such as urea, into an exhaust conduit forming part of an exhaust system for an internal combustion engine system, the nitrogen oxides reduction agent injection arrangement comprising a nozzle that is adapted to inject the nitrogen oxides reduction agent into the interior of the exhaust conduit via a nozzle opening of the nozzle, the nozzle comprising a nozzle opening control portion made of a shape memory material whereby a size and/or a shape of the nozzle opening is dependent on at least a temperature of the nozzle opening control portion.
2. The nitrogen oxides reduction agent injection arrangement of claim 1, wherein the nozzle opening control portion forms an integral part of the nozzle.
3. The nitrogen oxides reduction agent injection arrangement of claim 2, wherein the nozzle is made of the shape memory material.
4. The nitrogen oxides reduction agent injection arrangement of claim 1, further comprising a heating element at least thermally connected to the nozzle opening control portion.
5. The nitrogen oxides reduction agent injection arrangement of claim 4, wherein the heating element comprises an electric heating filament connected to the nozzle opening control portion.
6. The nitrogen oxides reduction agent injection arrangement of claim 4, further comprising a sensor for sensing exhaust gas information, indicative of at least one of the following: a temperature, a mixing pressure, and a flow speed, of an exhaust gas in the exhaust conduit upstream of the nozzle, the nitrogen oxides reduction agent injection arrangement further comprising a control unit adapted to receive the exhaust gas information and to control a heating of the heating element in response to the exhaust gas information.
7. The nitrogen oxides reduction agent injection arrangement of claim 1, further comprising a source of the nitrogen oxides reduction agent and a dosing unit for controlling a flow of the nitrogen oxides reduction agent from the source of the nitrogen oxides reduction agent to the nozzle opening.
8. The nitrogen oxides reduction agent injection arrangement of claim 1, wherein the shape memory material comprises an alloy comprising any one of the following metals: Nickel and Titanium; Nickel, Titanium and Iron; Nickel, Titanium and Niobium; Nickel, Titanium and Copper; Iron, Manganese and Silicon; Copper, Zinc and Aluminum, and Copper, Aluminum and Nickel.
9. The nitrogen oxides reduction agent injection arrangement of claim 1, wherein the nitrogen oxides reduction agent injection arrangement comprises a plurality of nozzles.
10. The nitrogen oxides reduction agent injection arrangement of claim 9, wherein the nozzles of the plurality of nozzles are adapted to be evenly distributed around a circumference of the exhaust conduit.
11. The nitrogen oxides reduction agent injection arrangement of claim 9, wherein the exhaust conduit has a cross section with a cross sectional center and wherein each nozzle of the plurality of nozzles is adapted to inject the nitrogen oxides reduction agent towards the cross sectional center.
12. An exhaust system for an internal combustion engine, the exhaust system comprising an exhaust conduit and the nitrogen oxides reduction agent injection arrangement of claim 1.
13. The exhaust system of claim 12, further comprising a selective catalytic reduction unit being adapted to receive exhaust gases from the exhaust conduit, the selective catalytic reduction unit being located downstream of the nitrogen oxides reduction agent injection arrangement as seen in a direction of flow of the exhaust gas.
14. An internal combustion engine system comprising an internal combustion engine and the nitrogen oxides reduction agent injection arrangement of claim 1.
15. A vehicle comprising the nitrogen oxides reduction agent injection arrangement of claim 1.
16. An internal combustion engine system comprising an internal combustion engine and the exhaust system of claim 12.
17. A vehicle comprising the exhaust system of claim 12.
18. A vehicle comprising the internal combustion engine system of claim 14.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0021] Examples are described in more detail below with reference to the appended drawings.
[0022]
[0023]
[0024]
[0025]
[0026]
[0027]
[0028]
[0029]
DETAILED DESCRIPTION
[0030] The detailed description set forth below provides information and examples of the disclosed technology with sufficient detail to enable those skilled in the art to practice the disclosure.
[0031]
[0032]
[0033] Furthermore, as a non-limiting example, the exhaust system 16 may comprise a selective catalytic reduction unit 24 which is adapted to receive exhaust gases from the exhaust conduit 18. As indicated in
[0034]
[0035] However, for every example of the nozzle opening control portion 30, the shape memory material may comprise an alloy comprising any one of the following metals: Nickel and Titanium; Nickel, Titanium and Iron; Nickel, Titanium and Niobium; Nickel, Titanium and Copper; Iron, Manganese and Silicon; Copper, Zinc and Aluminum, and Copper, Aluminum and Nickel.
[0036] Irrespective of the implementation of the nozzle opening control portion 30, as indicated the
[0037] Furthermore, as a non-limiting example, as indicated in each one of the
[0038]
[0039]
[0040]
[0041] Moreover, though purely by way of example, the control unit 44 may also be adapted to issue control information to the dosing unit 40 of the nitrogen oxides reduction agent injection arrangement 20.
[0042]
[0043]
[0044] It should be noted that the present disclosure may be presented in accordance with any one of the below Examples.
[0045] Example 1: A nitrogen oxides reduction agent injection arrangement 20 for injecting a nitrogen oxides reduction agent, such as urea, into an exhaust conduit 18 forming part of an exhaust system 16 for an internal combustion engine system 12, the nitrogen oxides reduction agent injection arrangement 20 comprising a nozzle 26 that is adapted to inject the nitrogen oxides reduction agent into the interior of the exhaust conduit 18 via a nozzle opening 28 of the nozzle 26, the nozzle 26 comprising a nozzle opening control portion 30 made of a shape memory material whereby a size and/or a shape of the nozzle opening 28 is dependent on at least a temperature of the nozzle opening control portion 30.
[0046] Example 2: The nitrogen oxides reduction agent injection arrangement 20 of Example 1, wherein the nozzle opening control portion 30 forms an integral part of the nozzle 26.
[0047] Example 3: The nitrogen oxides reduction agent injection arrangement 20 of Example 2, wherein the nozzle 26 is made of the shape memory material.
[0048] Example 4: The nitrogen oxides reduction agent injection arrangement 20 of any one of the preceding Examples, further comprising a heating element 34 at least thermally connected to the nozzle opening control portion 30.
[0049] Example 5: The nitrogen oxides reduction agent injection arrangement 20 of Example 4, wherein the heating element 34 comprises an electric heating filament 36 connected to the nozzle opening control portion 30.
[0050] Example 6: The nitrogen oxides reduction agent injection arrangement 20 of Example 4 or Example 5, further comprising a sensor 42 for sensing exhaust gas information, indicative of at least one of the following: a temperature, a mixing pressure and a flow speed, of an exhaust gas in the exhaust conduit 18 upstream of the nozzle 26, the nitrogen oxides reduction agent injection arrangement 20 further comprising a control unit 44 adapted to receive the exhaust gas information and to control a heating of the heating element 34 in response to the exhaust gas information.
[0051] Example 7: The nitrogen oxides reduction agent injection arrangement 20 of any one of the preceding Examples, further comprising a source 38 of the nitrogen oxides reduction agent and a dosing unit 40 for controlling a flow of the nitrogen oxides reduction agent from the source 38 of the nitrogen oxides reduction agent to the nozzle opening 28.
[0052] Example 8: The nitrogen oxides reduction agent injection arrangement 20 of any one of the preceding Examples, wherein the shape memory material comprises an alloy comprising any one of the following metals: Nickel and Titanium; Nickel, Titanium and Iron; Nickel, Titanium and Niobium; Nickel, Titanium and Copper; Iron, Manganese and Silicon; Copper, Zinc and Aluminum, and Copper, Aluminum and Nickel.
[0053] Example 9: The nitrogen oxides reduction agent injection arrangement 20 of any one of the preceding Examples, wherein the nitrogen oxides reduction agent injection arrangement 20 comprises a plurality of nozzles 26, 26, 26 in accordance with any one of the preceding Examples.
[0054] Example 10: The nitrogen oxides reduction agent injection arrangement 20 of Example 9, wherein the nozzles of the plurality of nozzles 26, 26, 26 are adapted to be evenly distributed around a circumference of the exhaust conduit 18.
[0055] Example 11: The nitrogen oxides reduction agent injection arrangement 20 of Example 9 or Example 10, wherein the exhaust conduit 18 has a cross section with a cross sectional center C and wherein each nozzle 26 of the plurality of nozzles 26, 26, 26 is adapted to inject the nitrogen oxides reduction agent towards the cross sectional center C.
[0056] Example 12: An exhaust system 16 for an internal combustion engine, the exhaust system 16 comprising an exhaust conduit 18 and a nitrogen oxides reduction agent injection arrangement 20 of any one of the preceding Examples.
[0057] Example 13: The exhaust system 16 of Example 12, further comprising a selective catalytic reduction unit 24 being adapted to receive exhaust gases from the exhaust conduit 18, the selective catalytic reduction unit 24 being located downstream of the nitrogen oxides reduction agent injection arrangement 20 as seen in a direction of flow of the exhaust gas.
[0058] Example 14: An internal combustion engine system 12 comprising an internal combustion engine 14 and a nitrogen oxides reduction agent injection arrangement 20 of any one of Examples 1-11 or an exhaust system 16 of any one of Examples 12-13.
[0059] Example 15: A vehicle 10 comprising a nitrogen oxides reduction agent injection arrangement 20 of any one of Examples 1-11 or an exhaust system 16 of any one of Examples 12-13 or an internal combustion engine system 12 of Example 14.
[0060] Example 16: A method for controlling injection of a nitrogen oxides reduction agent, such as urea, into an exhaust conduit 18 forming part of an exhaust system 16 for an internal combustion engine system 12, using a nitrogen oxides reduction agent injection arrangement 20, wherein the nitrogen oxides reduction agent injection arrangement 20 comprises a nozzle 26 that is adapted to inject the nitrogen oxides reduction agent into the interior of the exhaust conduit 18 via a nozzle opening 28 of the nozzle 26, the nozzle 26 comprising a nozzle opening control portion 30 made of a shape memory material whereby a size and/or a shape of the nozzle opening 28 is dependent on at least a temperature of the nozzle opening control portion 30, wherein the nitrogen oxides reduction agent injection arrangement 20 comprises a heating element 34 at least thermally connected to the nozzle opening control portion 30, wherein the method comprises sensing exhaust gas information, indicative of at least one of the following: a temperature, a mixing pressure and a flow speed, of an exhaust gas in the exhaust conduit 18 upstream of the nozzle 26, and controlling a heating of the heating element 34 in response to the exhaust gas information. It should be noted that the method may be carried out with any example of the nitrogen oxides reduction agent injection arrangement 20 as presented above or in the below appended claims.
[0061] It should be noted that, as used in the present application, gases NO and/or NO.sub.2 may also be referred to as nitric oxide. As such, as used in the present application, a nitrogen oxides reduction agent may also be referred to as a nitric oxide reduction agent. Alternatively, the term NO and/or NO.sub.2 reduction agent may be used. As may be realized from the above, as used in the present application, the terms nitrogen oxides reduction agent, nitric oxide reduction agent and NO and/or NO.sub.2 reduction agent are equivalent and can thus be used interchangeably.
[0062] The terminology used herein is for the purpose of describing particular aspects only and is not intended to be limiting of the disclosure. As used herein, the singular forms a, an, and the are intended to include the plural forms as well, unless the context clearly indicates otherwise. As used herein, the term and/or includes any and all combinations of one or more of the associated listed items. It will be further understood that the terms comprises, comprising, includes, and/or including when used herein specify the presence of stated features, integers, actions, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, actions, steps, operations, elements, components, and/or groups thereof.
[0063] It will be understood that, although the terms first, second, etc., may be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another. For example, a first element could be termed a second element, and, similarly, a second element could be termed a first element without departing from the scope of the present disclosure.
[0064] Relative terms such as below or above or upper or lower or horizontal or vertical may be used herein to describe a relationship of one element to another element as illustrated in the Figures. It will be understood that these terms and those discussed above are intended to encompass different orientations of the device in addition to the orientation depicted in the Figures. It will be understood that when an element is referred to as being connected or coupled to another element, it can be directly connected or coupled to the other element, or intervening elements may be present. In contrast, when an element is referred to as being directly connected or directly coupled to another element, there are no intervening elements present.
[0065] Unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this disclosure belongs. It will be further understood that terms used herein should be interpreted as having a meaning consistent with their meaning in the context of this specification and the relevant art and will not be interpreted in an idealized or overly formal sense unless expressly so defined herein.
[0066] It is to be understood that the present disclosure is not limited to the aspects described above and illustrated in the drawings; rather, the skilled person will recognize that many changes and modifications may be made within the scope of the present disclosure and appended claims. In the drawings and specification, there have been disclosed aspects for purposes of illustration only and not for purposes of limitation, the scope of the disclosure being set forth in the following claims.