CN209604124U - Swirl-flow devices are used in diesel emission post-processing - Google Patents
Swirl-flow devices are used in diesel emission post-processing Download PDFInfo
- Publication number
- CN209604124U CN209604124U CN201920391038.4U CN201920391038U CN209604124U CN 209604124 U CN209604124 U CN 209604124U CN 201920391038 U CN201920391038 U CN 201920391038U CN 209604124 U CN209604124 U CN 209604124U
- Authority
- CN
- China
- Prior art keywords
- partition
- air
- inlet pipe
- air inlet
- sleeve
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A50/00—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE in human health protection, e.g. against extreme weather
- Y02A50/20—Air quality improvement or preservation, e.g. vehicle emission control or emission reduction by using catalytic converters
Landscapes
- Exhaust Gas After Treatment (AREA)
Abstract
The utility model discloses a kind of diesel emission post-processing swirl-flow devices, including shell, SCR carrier is equipped in shell, housing downstream end is equipped with gas outlet, shell upstream end is equipped with end cap, end cap is connected with air inlet pipe, and housing central section is equipped at intervals with partition and diffuser plate in the axial direction, disperse hole is evenly distributed on diffuser plate；Level-one swirl vane is fixedly connected in air inlet pipe；The stream side surface of partition is fixedly connected with sleeve, and sleeve has been uniformly distributed circumferentially eddy flow air hole, and the partition at eddy flow air hole is connected with second level swirl vane, is evenly distributed with air inflow inlet in the air inlet pipe in sleeve；The main stomata of partition is evenly distributed on partition outside sleeve.The utility model ensure that the mixed uniformly effect of gas-liquid under lesser volume, can adapt to the installation space of most diesel oil engine vehicle, while air-flow entirety pressure drop control does not increase engine consumption in good level, has good market prospects.
Description
Technical field
The utility model relates to a kind of diesel emission post-processing technology fields.
Background technique
With the upgrading of emission regulation, diesel engine single use SCR(selective catalytic reduction) system or DPF(it is micro-
Grain trapping) system has been unable to meet regulation to NOx (nitrogen oxides), PM(particle) and PN(amounts of particles) limit value require, must
Must emission regulation limit value requirement be just able to satisfy using DPF system and SCR system simultaneously.It include shell, shell in existing SCR system
It is equipped with SCR carrier in vivo, tail gas is reacted and is purified when passing through shell.
But the DPF+SCR system of traditional structure is because overall volume is big caused by having independent mixed structure, length is long, it is general
Adaptive is poor.Especially under the requirement of stringenter environmental emission standard, reach the DPF+ of the traditional structure of new standard requirement
SCR system volume is bigger, is installed on many vehicles there is no enough spaces.Exhaust treatment system as vehicle accessory,
Need to meet the installation requirement of vehicle, the design of vehicle itself is difficult for some attachment and makes variation.
Meanwhile being distinctly claimed that " flow velocity is equal in " CAEPI 12-2017 " diesel engine exhausting after-treatment device " " of newest publication
Evenness, temperature uniformity and NH3The uniformity must not be lower than 0.95.And traditional gas-liquid mixed structure has been unable to meet above-mentioned want
It asks.
In short, in order to preferably be applicable in the market demand, it is necessary to which developing not only can guarantee gas-liquid mixed effect but also can reduce total
The vent gas treatment structure of volume.
Utility model content
The purpose of this utility model is to provide a kind of diesel emission post-processing swirl-flow devices.
To achieve the above object, the diesel emission post-processing swirl-flow devices of the utility model include shell, in shell
Equipped with SCR carrier, the axis direction of shell is the flow direction of air-flow entirety, using the direction of air-flow flowing as downstream direction, shell
Body downstream is equipped with gas outlet, and shell upstream end is equipped with end cap, and end cap is connected with air inlet pipe, and air inlet pipe is set with shell coaxial line
It sets,
The upstream end of air inlet pipe is located at hull outside and the downstream of air inlet pipe is located at enclosure interior；Housing central section is in axial direction
It is equipped at intervals with partition and diffuser plate on direction, disperse hole is evenly distributed on diffuser plate；
The peripheral edge edge of partition and the peripheral edge edge of diffuser plate are fixedly connected with inner walls；End cap updrift side into
It is intratracheally fixedly connected with level-one swirl vane, the air inlet tube cavity of level-one swirl vane downstream direction is first chamber；
Diffuser plate surrounds carrier chamber with shell downstream, and SCR carrier is located in carrier chamber；Partition and diffuser plate and two
Shell between person surrounds third chamber；The stream side surface of partition is fixedly connected with sleeve, and sleeve has been uniformly distributed circumferentially
Several eddy flow air holes, the partition outer surface at each eddy flow air hole are respectively connected with second level swirl vane, second level swirl vane with
The connection side of partition is parallel to shell axis, and plane where second level swirl vane is parallel to shell axis；
Air inlet pipe protrudes into sleeve, and has annular gap between the outer wall and sleeve lining of air inlet pipe；In sleeve into
Air inflow inlet is evenly distributed on tracheae；
Sleeve outer wall and end cap, shell and partition surround second chamber, and partition master is evenly distributed on the partition outside sleeve
Stomata；The air inlet pipe of end cap updrift side is equipped with nozzle mounting base, and the radial direction in nozzle mounting base along air inlet pipe is equipped with
For installing the mounting hole of atomizer；Nozzle mounting base be located at the downstream direction of level-one swirl vane and with level-one swirl vane
It is adjacent；
First chamber, air inflow inlet, air inlet pipe outer wall and sleeve lining between annular gap, eddy flow air hole, two
Grade swirl vane and the main stomatal limiting value of partition enter the first path of third chamber for mixed airflow.
Second level swirl vane is folded structure, including the first baffle plate and the second baffle plate, the first baffle plate and sleeve phase
It connects and connects while for benchmark, the angle of the tangent line of sleeve and the first baffle plate is α at true edge；Second baffle plate and second
Angle between baffle plate is β；α is more than or equal to 30 degree and less than or equal to 35 degree, and β is more than or equal to 135 degree and is less than or equal to 150
Degree.
Partition pair stomata is evenly distributed on partition in sleeve；The diameter of the main stomata of partition is the diameter of partition pair stomata
Three times more than；The diameter of partition is 1.5-2.5 times of the diameter of sleeve；
First chamber and partition pair stomatal limiting value enter the second path of third chamber for mixed airflow；
Air-flow is identical by pressure drop caused by the second path as air-flow by pressure drop caused by first path.
The width L1 of first baffle plate is 2-3 times of the width L2 between the second baffle plate, eddy flow air hole
Width is equal to L1+L2.
The upstream end of air inlet pipe is connected with flange.
The air inlet pipe of end cap updrift side is equipped with first sensor mounting base and second sensor mounting base, the first sensing
Device mounting base and second sensor mounting base are respectively positioned on the downstream direction of level-one swirl vane, and first sensor mounting base is equipped with
Along air inlet pipe radial direction be arranged be used for temperature sensor mounted mounting hole, second sensor mounting base be equipped with along into
The mounting hole for being used to install NOx sensor of the radial direction setting of tracheae.
The line in any three mutual adjacent and not air inflow inlet on the same line the centers of circle forms equilateral triangle.
Using the diesel emission post-processing swirl-flow devices of the utility model, by curved at two-stage eddy flow, second level eddy flow
The setting such as air flow path, two air flow paths is rolled over, the mixed uniformly effect of gas-liquid is ensure that under lesser volume, can adapt to
The installation space of most diesel oil engine vehicle, while air-flow entirety pressure drop control both can guarantee that gas-liquid was mixed in good level
Total volume can be reduced again by closing effect, not increased compared with it can reach the same uniformly existing mixed structure of the large volume of mixed-level
Engine consumption (existing mixed structure can not adapt to the lesser installation space of many vehicles because volume is big), has good
Market prospects.The diesel emission post-processing swirl-flow devices of the utility model effectively avoid the rebuffed pre-cooling of aqueous solution of urea simultaneously
The problem of crystallization.
The value of α is smaller, and eddy flow effect is better, and gas mixing effect is better；But the value of α is smaller simultaneously will also result in air-flow
Resistance it is also bigger.
If second level swirl vane is tabular, if to guarantee better eddy flow effect, the value of α cannot mistake
Greatly, it will lead to pressure drop when air-flow passes through in this way to increase, thus will increase the burden of engine, improve oil consumption.
The advantages of second level swirl vane is folded structure controls air-flow by the second baffle plate and passes through second level swirl vane
Eventually flowing to afterwards, thus the angle α need not be too small it is also ensured that eddy flow effect.The utility model is by setting the larger value for α
Reduce second level swirl vane to the resistance of air-flow to prevent from improving oil consumption, while the value by controlling β controls air-flow and leads to
It eventually flows to after crossing second level swirl vane and then ensure that eddy flow effect, while meeting eddy flow effect and control oil consumption two
A target.
On the one hand the setting in the second path can reduce gas-flow resistance, improve gas handling capacity, on the other hand improve
The uniformity coefficient of gas mixing.Air-flow passes through pressure drop caused by the second path by pressure drop caused by first path and air-flow
It is identical, gas can be made more uniformly to pass through partition, and improve the uniformity coefficient of gas mixing in third chamber.
The structure of second level swirl vane determine second level swirl vane need not other processing and fabricating, but can be on sleeve
When aperture, the sleeve wall of aperture segment is rotated upwards and is raised as rotating vane, on the one hand saves material cost in this way, separately
The sleeve wall part raised after one side aperture does not have to abandon, and reduces garbage disposal cost and the pollution to environment.
Under folded structure, the ratio between width L2 between the width L1 and the second baffle plate of the first baffle plate is got over
Small, then second level swirl vane is bigger to the resistance of air-flow on the whole, the easier oil consumption for increasing engine.Meanwhile first folding
The ratio between width L2 between the width L1 and the second baffle plate of flowing plate is bigger, then the second baffle plate makees the constraint of air-flow
With smaller, second level swirl vane is smaller to the cyclonic action of air-flow on the whole.The width of first baffle plate in the utility model
L1 is 2-3 times of the width L2 between the second baffle plate, while ensure that and minimize gas-flow resistance and guarantee eddy flow effect
Two targets.
If each air inflow inlet is in matrix arrangement, it is uniformly distributed although also belonging to, each air inflow inlet and its periphery phase
The distance of other adjacent air inflow inlets be it is inconsistent, just will appear air-flow when air-flow passes through in this way with respect to compact district, it is unfavorable
It is sufficiently mixed in gas, is also unfavorable for reducing gas-flow resistance.
The line in any three mutual adjacent and not air inflow inlet on the same line the centers of circle forms equilateral triangle,
Not only ensure that the uniformity of air inflow inlet distribution, and ensure that other adjacent with its periphery of any one air inflow inlet into
The distance of gas stomata is all identical, to eliminate air-flow with respect to compact district；Simultaneously under identical area compared to matrix arrangement into
More air inflow inlets can be arranged in gas stomata, reduce gas-flow resistance.
The diameter of partition is 1.5-2.5 times of the diameter of sleeve；The distribution area that ensure that the main stomata of partition is partition pair
The reasonable multiple of the distribution area of stomata is easy the gas-flow resistance of balance first path and the second path.
Detailed description of the invention
Fig. 1 is the schematic perspective view of the utility model after removing a part of shell and SCR carrier；
Fig. 2 is the sectional view of sleeve and second level swirl vane；
Fig. 3 is the structural schematic diagram of partition；
Fig. 4 is the structural schematic diagram of diffuser plate；
Fig. 5 is the structural schematic diagram of air inlet pipe after lost nozzle mounting base, the first and second sensor installation seats；
Fig. 6 is the schematic perspective view of sleeve and second level swirl vane.
Specific embodiment
As shown in Figures 1 to 6, the diesel emission post-processing swirl-flow devices of the utility model include shell 1, shell 1
Interior to be equipped with SCR carrier, the axis direction of shell 1 is the flow direction of air-flow entirety, using the direction of air-flow flowing as downstream direction,
1 downstream of shell is equipped with gas outlet, and 1 upstream end of shell is equipped with end cap 2, and end cap 2 is connected with air inlet pipe 3, air inlet pipe 3 and shell 1
It is coaxially set, the upstream end of air inlet pipe 3 is located at 1 outside of shell and the downstream of air inlet pipe 3 and is located inside shell 1；In shell 1
Portion is equipped at intervals with partition 4 and diffuser plate 5 in the axial direction, and disperse hole 6 is evenly distributed on diffuser plate 5；It is provided on shell
Port is routine techniques, gas outlet not shown.
The peripheral edge edge of partition 4 and the peripheral edge edge of diffuser plate 5 are fixedly connected with 1 inner wall of shell；2 updrift side of end cap
Air inlet pipe 3 in be fixedly connected with level-one swirl vane 7,3 inner cavity of air inlet pipe of 7 downstream direction of level-one swirl vane is the first chamber
Room 10；Level-one swirl vane 7 not can rotate with the fixation of second level swirl vane 8 hereafter；Level-one swirl vane 7 is in common
Fan it is lobate, figure be not shown in detail.
Diffuser plate 5 surrounds carrier chamber 9 with shell 1 downstream, and SCR carrier is located in carrier chamber 9；Partition 4 and diffuser plate 5
And shell 1 between the two surrounds third chamber 12；The stream side surface of partition 4 is fixedly connected with sleeve 13,13 edge of sleeve
Several eddy flow air holes 14 circumferentially are evenly distributed with, 4 outer surface of partition at each eddy flow air hole 14 is respectively connected with second level eddy flow
The connection side of blade 8, second level swirl vane 8 and partition 4 is parallel to 1 axis of shell, and 8 place plane of second level swirl vane is parallel to
1 axis of shell, can play good guide functions in this way；
Air inlet pipe 3 protrudes into sleeve 13, and has annular gap between 13 inner wall of the outer wall of air inlet pipe 3 and sleeve；Sleeve
Air inflow inlet 15 is evenly distributed in air inlet pipe 3 in 13；13 outer wall of sleeve and end cap 2, shell 1 and partition 4 surround the second chamber
Room 11 is evenly distributed with the main stomata 16 of partition on the partition 4 outside sleeve 13；The air inlet pipe 3 of 2 updrift side of end cap is equipped with nozzle
Mounting base 17；The mounting hole for installing atomizer is equipped with along the radial direction of air inlet pipe in nozzle mounting base；Nozzle installation
Seat 17 is located at the downstream direction of level-one swirl vane 7 and adjacent with level-one swirl vane 7；
Annular gap, eddy flow between first chamber 10,13 inner wall of air inflow inlet 15, the outer wall of air inlet pipe 3 and sleeve is saturating
Stomata 14, second level swirl vane 8 and the main stomata 16 of partition form the first path for entering third chamber 12 for mixed airflow.
Second level swirl vane 8 is folded structure, including the first baffle plate 21 and the second baffle plate 22, the first baffle plate 21 with
Sleeve 13 is connected and connects 23 while for benchmark, and the angle of the tangent line of sleeve 13 and the first baffle plate 21 is α at true edge 23；
Angle between second baffle plate 22 and the second baffle plate 22 is β；α is more than or equal to 30 degree and less than or equal to 35 degree, and β is more than or equal to
135 degree and be less than or equal to 150 degree.
The value of α is smaller, and eddy flow effect is better, and gas mixing effect is better；But the value of α is smaller simultaneously will also result in air-flow
Resistance it is also bigger.
If second level swirl vane 8 is tabular, if to guarantee better eddy flow effect, the value of α cannot mistake
Greatly, it will lead to pressure drop when air-flow passes through in this way to increase, thus will increase the burden of engine, improve oil consumption.
The advantages of second level swirl vane 8 is folded structure controls air-flow by the second baffle plate 22 and passes through second level eddy flow
It is eventually flowed to after blade 8, thus the angle α need not be too small it is also ensured that eddy flow effect.The utility model by by α be set as compared with
Big value reduces second level swirl vane 8 to the resistance of air-flow to prevent from improving oil consumption, while the value by controlling β controls gas
Stream by eventually flowing to after second level swirl vane 8, ensure that eddy flow effect, while meeting eddy flow effect and controlling oily
Consume two targets.
Partition pair stomata 24 is evenly distributed on partition 4 in sleeve 13；The diameter of the main stomata 16 of partition is partition pair gas
It is more than the three times of the diameter in hole 24；The diameter of partition 4 is 1.5-2.5 times of the diameter of sleeve 13；The diameter of partition 4 is preferably
2 times of the diameter of sleeve 13.
First chamber 10 and partition pair stomata 24 form the second path for entering third chamber 12 for mixed airflow；
Air-flow is identical by pressure drop caused by the second path as air-flow by pressure drop caused by first path.
On the one hand the setting in the second path can reduce gas-flow resistance, improve gas handling capacity, on the other hand improve
The uniformity coefficient of gas mixing.Air-flow passes through pressure drop caused by the second path by pressure drop caused by first path and air-flow
It is identical, gas can be made more uniformly to pass through partition 4, and improve the uniformity coefficient of gas mixing in third chamber 12.
The width L1 of first baffle plate 21 is 2-3 times of the width L2 between the second baffle plate 22 (comprising both ends
Value), the width of eddy flow air hole 14 is equal to L1+L2.
The structure of second level swirl vane 8 determine second level swirl vane 8 need not other processing and fabricating, but can be in sleeve
On 13 when aperture, 13 wall of sleeve of aperture segment is rotated upwards and is raised as rotating vane, on the one hand saves material in this way
Cost, 13 wall part of sleeve raised after another aspect aperture do not have to abandon, and reduce garbage disposal cost and the dirt to environment
Dye.
The ratio between width L2 under folded structure, between the width L1 of the first baffle plate 21 and the second baffle plate 22
Smaller, then second level swirl vane 8 is bigger to the resistance of air-flow on the whole, the easier oil consumption for increasing engine.Meanwhile first
The ratio between width L2 between the width L1 of baffle plate 21 and the second baffle plate 22 is bigger, then the second baffle plate 22 is to air-flow
Effect of contraction it is smaller, second level swirl vane 8 is smaller to the cyclonic action of air-flow on the whole.First baffling in the utility model
The width L1 of plate 21 is 2-3 times of the width L2 between the second baffle plate 22, at the same ensure that minimize gas-flow resistance with
Guarantee two targets of eddy flow effect.
The upstream end of air inlet pipe 3 is connected with flange 25, consequently facilitating the exhaust pipe with engine is connected.
The air inlet pipe 3 of 2 updrift side of end cap is equipped with first sensor mounting base 19 and second sensor mounting base 20, the
One sensor installation seat 19 and second sensor mounting base 20 are respectively positioned on the downstream direction of level-one swirl vane 7；
First sensor mounting base 19 is equipped with the radial direction setting along air inlet pipe for temperature sensor mounted
Mounting hole, second sensor mounting base 20 are equipped with the peace for being used to install NOx sensor being arranged along the radial direction of air inlet pipe
Fill hole.
The setting of first sensor mounting base 19 and second sensor mounting base 20, is easily installed temperature sensor and NOx
Sensor.
The line in any three mutual adjacent and not air inflow inlet 15 on the same line the centers of circle forms equilateral triangle
Shape.
If each air inflow inlet 15 is in matrix arrangement, it is uniformly distributed although also belonging to, each air inflow inlet 15 and its week
The distance of other adjacent air inflow inlets 15 of side be it is inconsistent, it is relatively intensive just to will appear air-flow when air-flow passes through in this way
Area, is unfavorable for gas and is sufficiently mixed, and is also unfavorable for reducing gas-flow resistance.
The line in any three mutual adjacent and not air inflow inlet 15 on the same line the centers of circle forms equilateral triangle
Shape not only ensure that the uniformity that air inflow inlet 15 is distributed, and ensure that any one air inflow inlet 15 is adjacent with its periphery
Other air inflow inlets 15 distance it is all identical, to eliminate air-flow with respect to compact district；Square is compared under identical area simultaneously
More air inflow inlets 15 can be arranged in configuration arrangement air inflow inlet 15, reduce gas-flow resistance.
SCR carrier preferably uses honeycomb ceramic carrier, especially cordierite honeycomb ceramic carrier.
In use, the diesel emission post-processing swirl-flow devices of the utility model are mounted on engines tail by flange 25
On gas delivery pipe, the atomizer for spraying into aqueous solution of urea is installed at nozzle mounting base 17, is pacified at the first mounting hole
Temperature sensor is filled, NOx sensor is installed at the second mounting hole.Temperature sensor and NOx sensor then pass through vehicle electronic circuit
Access vehicle-mounted ECU.
When diesel engine works, tail gas enters the air inlet pipe 3 of the utility model by tail gas discharging pipe, through level-one eddy flow
Blade 7 generates eddy flow and enters first chamber 10；Aqueous solution of urea is sprayed into first chamber 10 by atomizer, in eddy flow
Effect is lower to be mixed with air-flow；Mixed airflow moves downstream；Since the distribution area of the main stomata 16 of partition is partition pair gas
The reasonable multiple of the distribution area in hole 24, thus it is easy the gas-flow resistance of balance first path and the second path, keep air-flow uniform
Flowing.A part of air-flow enters third chamber 12 by first path, and another part air-flow enters third chamber by the second path
Room 12.It has passed through the commutation and the cyclonic action of the second swirl vane of air-flow by the air-flow of first path；Two parts air-flow warp
Collaborate once more after crossing shunting in third chamber 12, forms better even results.Air-flow in third chamber 12 is by more
Enter the SCR carrier in carrier chamber 9 after dissipating hole 6, nitrogen oxides is converted, the oxious component in tail gas is removed；After reaction
Tail gas be discharged into environment through gas outlet.
Above embodiments are only to illustrate rather than limit the technical solution of the utility model, although referring to above-described embodiment pair
The utility model is described in detail, those skilled in the art should understand that: still can to the utility model into
Row modification or equivalent replacement should all without departing from any modification or partial replacement of the spirit and scope of the utility model
Cover in the scope of the claims of the utility model.
Claims (7)
1. diesel emission post-processing swirl-flow devices, including shell, shell is interior to be equipped with SCR carrier, and the axis direction of shell is
The flow direction of air-flow entirety, using the direction of air-flow flowing as downstream direction, housing downstream end is equipped with gas outlet, shell upstream end
Equipped with end cap, end cap is connected with air inlet pipe, and air inlet pipe is coaxially set with shell, it is characterised in that:
The upstream end of air inlet pipe is located at hull outside and the downstream of air inlet pipe is located at enclosure interior；Housing central section is in the axial direction
On be equipped at intervals with partition and diffuser plate, disperse hole is evenly distributed on diffuser plate；
The peripheral edge edge of partition and the peripheral edge edge of diffuser plate are fixedly connected with inner walls；The air inlet pipe of end cap updrift side
It is inside fixedly connected with level-one swirl vane, the air inlet tube cavity of level-one swirl vane downstream direction is first chamber；
Diffuser plate surrounds carrier chamber with shell downstream, and SCR carrier is located in carrier chamber；Partition and diffuser plate and the two it
Between shell surround third chamber；The stream side surface of partition is fixedly connected with sleeve, and sleeve has been uniformly distributed circumferentially several
Eddy flow air hole, the partition outer surface at each eddy flow air hole are respectively connected with second level swirl vane, second level swirl vane and partition
Connection side be parallel to shell axis, plane where second level swirl vane is parallel to shell axis；
Air inlet pipe protrudes into sleeve, and has annular gap between the outer wall and sleeve lining of air inlet pipe；Air inlet pipe in sleeve
On be evenly distributed with air inflow inlet；
Sleeve outer wall and end cap, shell and partition surround second chamber, and the main stomata of partition is evenly distributed on the partition outside sleeve；
The air inlet pipe of end cap updrift side is equipped with nozzle mounting base, is equipped with along the radial direction of air inlet pipe for pacifying in nozzle mounting base
Fill the mounting hole of atomizer；Nozzle mounting base is located at the downstream direction of level-one swirl vane and adjacent with level-one swirl vane；
First chamber, air inflow inlet, air inlet pipe outer wall and sleeve lining between annular gap, eddy flow air hole, second level rotation
Stream blade and the main stomatal limiting value of partition enter the first path of third chamber for mixed airflow.
2. diesel emission according to claim 1 post-processing swirl-flow devices, it is characterised in that: second level swirl vane is
Folded structure, including the first baffle plate and the second baffle plate, the first baffle plate are connected with sleeve and connect while for benchmark, base
The angle of the tangent line of sleeve and the first baffle plate is α at quasi- side；Angle between second baffle plate and the second baffle plate is β；α is big
In equal to 30 degree and less than or equal to 35 degree, β is more than or equal to 135 degree and is less than or equal to 150 degree.
3. diesel emission post-processing swirl-flow devices according to claim 1, it is characterised in that: on the partition in sleeve
It is evenly distributed with partition pair stomata；The diameter of the main stomata of partition is the three times of the diameter of partition pair stomata or more；The diameter of partition
It is 1.5-2.5 times of the diameter of sleeve；
First chamber and partition pair stomatal limiting value enter the second path of third chamber for mixed airflow；
Air-flow is identical by pressure drop caused by the second path as air-flow by pressure drop caused by first path.
4. diesel emission post-processing swirl-flow devices according to claim 2, it is characterised in that: first baffle plate
Width L1 be 2-3 times of the width L2 between the second baffle plate, the width of eddy flow air hole is equal to L1+L2.
5. diesel emission post-processing swirl-flow devices according to any one of claim 1 to 3, it is characterised in that:
The upstream end of air inlet pipe is connected with flange.
6. diesel emission post-processing swirl-flow devices according to any one of claim 1 to 3, it is characterised in that: end
The air inlet pipe of lid updrift side be equipped with first sensor mounting base and second sensor mounting base, first sensor mounting base and
Second sensor mounting base is respectively positioned on the downstream direction of level-one swirl vane, and first sensor mounting base is equipped with along air inlet pipe
Radial direction setting is used for temperature sensor mounted mounting hole, and second sensor mounting base is equipped with the radial direction along air inlet pipe
The mounting hole for being used to install NOx sensor of direction setting.
7. diesel emission post-processing swirl-flow devices according to any one of claim 1 to 3, it is characterised in that: appoint
The line in three mutual adjacent and not air inflow inlet on the same line centers of circle of meaning forms equilateral triangle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920391038.4U CN209604124U (en) | 2019-03-26 | 2019-03-26 | Swirl-flow devices are used in diesel emission post-processing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920391038.4U CN209604124U (en) | 2019-03-26 | 2019-03-26 | Swirl-flow devices are used in diesel emission post-processing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209604124U true CN209604124U (en) | 2019-11-08 |
Family
ID=68405307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920391038.4U Active CN209604124U (en) | 2019-03-26 | 2019-03-26 | Swirl-flow devices are used in diesel emission post-processing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209604124U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109826697A (en) * | 2019-03-26 | 2019-05-31 | 平原滤清器有限公司 | Swirl-flow devices are used in diesel emission post-processing |
-
2019
- 2019-03-26 CN CN201920391038.4U patent/CN209604124U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109826697A (en) * | 2019-03-26 | 2019-05-31 | 平原滤清器有限公司 | Swirl-flow devices are used in diesel emission post-processing |
| CN109826697B (en) * | 2019-03-26 | 2024-01-19 | 平原滤清器有限公司 | Swirl device for diesel engine emission aftertreatment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106246303B (en) | Tail-gas after treatment apparatus | |
| CN104685177A (en) | Doser and mixer for a vehicle exhaust system | |
| WO2021189795A1 (en) | Diesel engine tail gas after treatment apparatus | |
| WO2016146015A1 (en) | Mixing tube and exhaust gas treatment device thereof | |
| WO2018006718A1 (en) | Tail gas aftertreatment device | |
| US11891937B2 (en) | Body mixing decomposition reactor | |
| CN110332035A (en) | SCR mixer and engine | |
| CN215109110U (en) | Mixer and engine exhaust aftertreatment system | |
| US20220184567A1 (en) | Mixer, Exhaust System and Mixing Method | |
| CN109826697A (en) | Swirl-flow devices are used in diesel emission post-processing | |
| CN209604124U (en) | Swirl-flow devices are used in diesel emission post-processing | |
| CN206987927U (en) | Exhaust aftertreatment mixing arrangement and its encapsulation | |
| CN209369905U (en) | A kind of close-coupled mixer assembly | |
| CN115135404A (en) | Mixer for use in an aftertreatment system | |
| CN109578120A (en) | Exhaust aftertreatment mixing arrangement | |
| CN112196646A (en) | Mixer assembly and exhaust aftertreatment package | |
| CN109356693B (en) | Compact mixer assembly | |
| WO2018006720A1 (en) | Mixing module | |
| CN218862709U (en) | Mixer assembly and exhaust aftertreatment package | |
| CN114278417B (en) | Exhaust aftertreatment urea mixing arrangement | |
| CN215633263U (en) | SCR mixer and have its engine | |
| WO2021189796A1 (en) | Mixing pipe assembly and tail gas aftertreatment device | |
| CN113431666A (en) | Mixing chamber subassembly and tail gas aftertreatment encapsulation | |
| WO2019140892A1 (en) | Exhaust aftertreatment apparatus | |
| WO2018095139A1 (en) | Exhaust aftertreatment device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |