EXHAUST GAS REDUCTION UNIT FOR INTERNAL COMBUSTIOIN ENGINE
20170241319 · 2017-08-24
Assignee
Inventors
Cpc classification
Y02A50/20
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
B01F25/4331
PERFORMING OPERATIONS; TRANSPORTING
B01F2101/2204
PERFORMING OPERATIONS; TRANSPORTING
F01N2410/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2892
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2240/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B01F25/431972
PERFORMING OPERATIONS; TRANSPORTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F01N2610/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2610/1453
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/2066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2260/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2260/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01N3/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Unit for reduction of exhaust gases for an IC engine. The unit has a cylindrical housing with gas inlet and outlet openings and injector for a reducing substance. A helicoid is coaxially arranged inside the housing. A channel conveys the exhaust gases, has a substantially quadrangular cross-section, and helicoidally develops inside the unit. The helix is generated by the intersection between the inner surface of the housing and the helicoid has an inclination angle (β) relative to planes perpendicular to the generatrices of the cylindrical housing ranging from 0° to 30°. The unit includes a coaxial stiffening and stabilization sleeve located at the center of the helicoid passing axially throughout the helicoid and axially over a length at least equal to the axial length of the helicoid. The sleeve cooperates with the inner surface of the housing and with the opposite surfaces of the helicoid to define the helicoidal channel.
Claims
1. Unit (11) for the reduction of exhaust gases for an IC engine, comprising: a cylindrical housing (13) having a gas inlet opening (15), a gas outlet opening (17) and an injector (19) for a reducing substance; a helicoid (21) coaxially arranged inside the housing (13); a channel (25) aimed at conveying the exhaust gases and having a substantially quadrangular cross-section, said channel helicoidally developing inside the unit (11); characterized in that the helix generated by the intersection between the inner surface of the housing (13) and the helicoid (21) has an inclination angle (β) relative to the planes perpendicular to the generatrices of the cylindrical housing ranging from 0° to 30° and in that it comprises a coaxial sleeve (23) for stiffening and stabilization, said sleeve being located at the center of the helicoid and passing axially throughout the helicoid (21) and axially extending over a length at least equal to the axial length of the helicoid (21), said sleeve (23) cooperating with the inner surface of the housing (13) and with the opposite surfaces of the helicoid (21) in order to define the helicoidal channel (25) for conveying the exhaust gases.
2. Unit according to claim 1, wherein said inclination angle (β) is smaller than 20°.
3. Unit according to claim 1, wherein the surface of the helicoid (21) comprises at least one hole (29a,29b).
4. Unit according to claim 3, wherein the surface of the helicoid (21) comprises a plurality of holes (29a,29b).
5. Unit according claim 1, wherein the helicoid (21) has opposite corrugated surfaces.
6. Unit according to claim 1, wherein the injector (19) is radially arranged in the housing (13) and opens into the helicoidally developing channel (25).
7. Unit according to claim 1, wherein the sleeve (23) is open at its both ends and defines a by-pass conduit with respect to the helicoidal channel (25).
8. Unit according to claim 7, wherein the area of the cross-section of the by-pass conduit is approximately 1/25 of the area of the transverse surface of the helicoidally developing channel (25).
9. Unit according to claim 1, wherein the diameter (d) of the sleeve (23) is at least one fifth of the diameter (D) of the helicoid (21).
10. Unit according to claim 1, wherein the sleeve (23) extends on both sides with respect to the axial length of the helicoid (21) over a length at least equal to the pitch (p) of the helicoid (21).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0015] Some preferred embodiments of the invention will be described by way of non-limiting example with reference to the accompanying drawings, in which same or functionally equivalent parts are designated with the same reference numerals:
[0016]
[0017]
[0018]
[0019]
DESCRIPTION OF PREFERRED EMBODIMENTS
[0020] Referring to
[0021] According to the invention, a helicoid 21 is arranged inside the housing 13. The helicoid 21 is coaxially arranged inside the housing and defines a channel 25 for conveying the exhaust gases. The channel 25 has a preferably quadrangular, substantially square or rectangular, cross-section, with a radial extension smaller than the axial one. Preferably, the pitch “p” of the helicoid 21 is constant. In addition, each generatrix of the housing 13 is tangent to the helicoid 21 in at least two points. The helix generated by the intersection between the inner surface of the housing 13 and the helicoid 21 has an inclination angle β with respect to the planes perpendicular to the generatrices of the cylindrical housing preferably ranging from 0° to 30°. Even more preferably, said angle β is smaller than 20°. According to the invention, there is provided a sleeve 23 coaxial to the center of the helicoid 21. The sleeve passes axially throughout the helicoid. The housing 13, the helicoid 21 and the sleeve 23 are preferably coaxial to the axis X-X.
[0022] The sleeve 23 has a function of stiffening and stabilization of the helicoid 21 inside the housing 13 and cooperates with the inner surface of the housing 13 and with the opposite surfaces of the helicoid 21 in order to define said channel 25 with helicoidal development.
[0023] According to the invention, the diameter “d” of the sleeve 23 is preferably at least one fifth of the diameter “D” of the helicoid 21. According to a variant of embodiment of the invention, the sleeve 23 has a length greater than the axial development of the helicoid and said sleeve 23 extends on one side, or even more preferably on both sides, with respect to the axial length of the helicoid 21, over a length at least equal to the pitch “p” of the helicoid 21.
[0024] Preferably, the sleeve 23 is hollow and closed at its upstream end by a plug 27. Alternatively, the sleeve 23 is hollow and open at its both ends and defines an axial by-pass conduit with respect to the helicoidal channel 25. Preferably, the area of the cross-section of the by-pass conduit is approximately 1/25 of the area of the cross-section of the helicoidally developing channel 25.
[0025] According to the invention, the surface of the helicoid 21 has one or both of its faces preferably corrugated, in order to promote passage of the gases and stiffen the structure of the helicoid 21.
[0026] Still according to the invention, the surface of the helicoid 21, which may be smooth or corrugated, preferably comprises at least one hole 29a,29b and more preferably a plurality of holes 29a,29b. The section of the holes 29a,29b can have various shapes, preferably a circular shape, holes numbered 29a, or a rectangular shape, holes numbered 29b. In the illustrated embodiment, both circular holes 29a and rectangular holes 29b are provided. Said holes are advantageously distributed according to a predetermined pattern in order to obtain the desired effects of reducing the pressure drop in the unit 11. Alternatively, the surface of the helicoid 21 may comprise a grid. The holes 29a,29b or the grid advantageously allow(s) passage of the exhaust gases in axial direction through the helicoid 21, thus reducing the pressure drop caused by the presence of the helicoidal channel 25.
[0027] The housing 13, the helicoid 21 and the sleeve 23 are preferably made of metal, preferably of steel sheet or aluminium sheet and joined together by welding along the helices generated by the intersection between the helicoid 21 and the generatrices of the sleeve 23 and the housing 13, respectively.
[0028] Referring to
[0029] In this embodiment of the invention, the injector 19 is arranged radially and protrudes through the housing 13 into the helicoidal channel 25, i.e. between the surfaces of the helicoid 21. This radial arrangement of the injector 19 is further compatible also with the first embodiment. Advantageously, the arrangement of the injector 19 in the channel 25, preferably not beyond half of the length of said channel 25, allows to obtain a more effective mixing action of the reducing substance with the exhaust gases by virtue of the helicoidal motion of the gases themselves. Still according to this second embodiment of the invention, it is also possible to provide the injector 19 arranged axially inside the housing 13, upstream of the helicoid 21, in the area of the housing 13 preceding said helicoid 21 in the direction of passage of the exhaust gases indicated by the arrows 31. This configuration may for instance be obtained by means of a portion of said housing 13 radially protruding inward of the housing.
[0030] The unit as described and illustrated may be subjected to several modifications falling within the same inventive principle.