CN206280162U - Engine nanometer air lattice - Google Patents
Engine nanometer air lattice Download PDFInfo
- Publication number
- CN206280162U CN206280162U CN201621236841.3U CN201621236841U CN206280162U CN 206280162 U CN206280162 U CN 206280162U CN 201621236841 U CN201621236841 U CN 201621236841U CN 206280162 U CN206280162 U CN 206280162U
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- China
- Prior art keywords
- combustion
- air
- supporting ring
- demarcation strip
- lattice
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Abstract
The utility model proposes engine nanometer air lattice, it is related to technical field of automobile engine, the engine nanometer air lattice include the first combustion-supporting ring, the second combustion-supporting ring and central aeration post, the first combustion-supporting ring is coaxially disposed with the second combustion-supporting ring, the center superposition of the first combustion-supporting ring, the second combustion-supporting ring and central aeration post, the first combustion-supporting ring and the second combustion-supporting ring are connected to central aeration post by air demarcation strip, and the air demarcation strip scattering device is between the first combustion-supporting ring and central aeration post or between the second combustion-supporting ring and central aeration post.The utility model constructs the nanometer air lattice for being arranged at motor head by the first combustion-supporting ring, the second combustion-supporting ring and central aeration post, engine nanometer air lattice enter into engine interior after can fully air molecule be broken up, the ratio of combustion of fuel in engine is improved, the power of engine is then improved.
Description
Technical field
The utility model is related to technical field of automobile engine, particularly guides and holds up a nanometer air lattice.
Background technology
Automobile engine（That is engine）At work, carburetor is by means of the external air provided in the cleaner unit interval
Fuel atomization, the oil molecule and air of atomization are blended burning and provide kinetic energy to engine by a certain percentage.And oil molecule and
Oxygen content in air causes engine power not enough often because mixing proportion is unstable, and oil consumption increases；Due to air-fuel mixture
It is irregular to cause incomplete combustion, a large amount of carbon distributions in cylinder are caused, increase the speed of cylinder body abrasion；Cause exhaust emissions serious simultaneously
Exceeded or even over-emitting black exhaust, severe contamination environment, virtually increased the potential safety hazard that vehicle exists under steam.
Utility model content
The purpose of this utility model is to solve the above problems and propose engine nanometer air lattice, and the utility model is by the
One combustion-supporting ring, the second combustion-supporting ring and central aeration post construct the nanometer air lattice for being arranged at motor head, the combustion-supporting gas
Engine interior is entered into after can fully air molecule be broken up, the ratio of combustion of fuel in engine is improved, hair is then improved
The power of motivation.
To achieve these goals, the technical scheme that the utility model is taken is as follows：
The utility model proposes engine nanometer air lattice, the nanometer air lattice include the first combustion-supporting ring, the second combustion-supporting ring
And central aeration post, the first combustion-supporting ring is coaxially disposed with the second combustion-supporting ring, the first combustion-supporting ring, the second combustion-supporting ring and in
The center superposition of heart ventilating column, the first combustion-supporting ring and the second combustion-supporting ring are connected to central aeration post by air demarcation strip,
The air demarcation strip scattering device between the first combustion-supporting ring and central aeration post or the second combustion-supporting ring and central aeration post it
Between.
Further, the air demarcation strip includes cuboid straight panel and transversal with the cuboid straight panel side edge
The curved arc in face, the air demarcation strip is obliquely installed between the first combustion-supporting ring and central aeration post or second is combustion-supporting
Between ring and central aeration post.
Further, the cross section of the central aeration post is in totally pentagram shape, and the central aeration post is provided with along its axle
To the center roof vent of insertion.
Further, border passage is provided with the inside of the described first combustion-supporting ring, the border passage is located at air point
On dividing plate and near the first combustion-supporting ring part.
Further, the border passage is in plum blossom-shaped.
Further, the described second combustion-supporting ring is arranged at the inner side of the first combustion-supporting ring, and the second combustion-supporting ring is divided equally described
Border passage, the first air demarcation strip is provided between the first combustion-supporting ring and the central aeration post, and described second is combustion-supporting
The second air demarcation strip is provided between ring and the central aeration post, the second air divider plate is arranged at first
Between air demarcation strip, the first air demarcation strip is arranged at same layer with the second air demarcation strip.
Further, the first air demarcation strip and the second air demarcation strip are 5.
Further, the described second combustion-supporting ring is arranged on the border passage, the height of the central aeration post
Equal to the first combustion-supporting ring and the height sum of the second combustion-supporting ring, is provided between the first combustion-supporting ring and the central aeration post
One air demarcation strip, the second air demarcation strip, described are provided between the second combustion-supporting ring and the central aeration post
Two air divider plates are arranged between the first air demarcation strip, and the first air demarcation strip separates with second air
Plate layering is set.
Further, the nanometer air lattice are in up-narrow and down-wide shape.
The beneficial effects of the utility model：
1. the utility model is used for the front end of engine, and air molecule first passes through nanometer air lattice of the present utility model and enters again
Enter to engine interior, when air molecule passes through nanometer air lattice, nanometer air lattice sufficiently can break up air molecule, improve
Air molecule and the mixing ratio of engine interior fuel, improve the ratio of combustion of fuel in engine, then improve the dynamic of engine
Power；
2. air demarcation strip is arranged to cuboid straight panel and the arc being connected with each other, and air demarcation strip is by nanometer air
The inner space of lattice is divided into some, and air first passes through cuboid straight panel, and cuboid straight panel separates air molecule breaks up,
In the effect by arc so that air molecule passes through speed increase during arc, intake velocity is improved, then improving has
Effect molecular weight, further improves the power of engine；
3. air demarcation strip is obliquely installed in the inside of nanometer air lattice so that air molecule is presented in nanometer air lattice
The characteristics of going out turbine type, improves the intake velocity of air；
4. nanometer air especially shape is presented shape with wide top and narrow bottom so that air admission hole is big and venthole is small so that air molecule from
Nanometer air lattice out after speed it is larger, subsequently into that can be sufficiently mixed with the fuel in engine after engine, enter
One step improves ratio of combustion.
Brief description of the drawings
Fig. 1 is the schematic perspective view of the utility model engine nanometer air lattice embodiment one；
Fig. 2 is the schematic perspective view of another angle of the utility model engine nanometer air lattice embodiment one；
Fig. 3 is the top view of the utility model engine nanometer air lattice embodiment one；
Fig. 4 is the upward view of the utility model engine nanometer air lattice embodiment one；
The schematic perspective view of Fig. 5 the utility model engine nanometer air lattice embodiment two；
Fig. 6 is the schematic perspective view of another angle of the utility model engine nanometer air lattice embodiment two；
Fig. 7 is the top view of the utility model engine nanometer air lattice embodiment two；
Fig. 8 is the upward view of the utility model engine nanometer air lattice embodiment two.
Wherein, the combustion-supporting rings of 1- first, the combustion-supporting rings of 2- second, 3- central aeration posts, 4- air demarcation strips, the ventilation of 5- borders
Hole, 31- center roof vents, 41- cuboid plates, 42- arcs, 43- the first air demarcation strips, 44- the second air demarcation strips.
Specific embodiment
Implementation method of the present utility model is described in detail referring now to accompanying drawing.It should be noted that following description is only to show
Example property, and it is not intended to limit the utility model.Additionally, in the following description, being indicated with like reference numerals adopting not
With the same or analogous part in accompanying drawing.Different characteristic in different embodiments described below, can be bonded to each other, with
Form the other embodiment in the range of the utility model.
As Figure 1-4, according to first embodiment of the present utility model, it is proposed that engine nanometer air lattice, this nanometer of sky
Gas lattice include the first combustion-supporting ring 1, the second combustion-supporting ring 2 and central aeration post 3, and the internal diameter of the second combustion-supporting ring 2 is less than the first combustion-supporting ring 1
Internal diameter, the first combustion-supporting ring 1 is coaxially disposed with the second combustion-supporting ring 2, and the first combustion-supporting ring 1, the second combustion-supporting ring 2 and central aeration post
On the one hand 3 center superposition, so enable to a nanometer air lattice to smooth on the whole attractive in appearance, on the other hand ensure that nanometer
The stabilization of the structure of air lattice, improves the service life of nanometer air lattice.
The cross section of above-mentioned central aeration post 3 is in totally pentagram shape, is provided with the inside of central aeration post 3 and is passed through along its axial direction
Logical center roof vent 31, totally pentagram shape because of its shape specification, on the one hand ensure that it is of the present utility model in structure
Stability, is on the other hand conducive to the connection between the combustion-supporting ring 1 of central aeration post 3 and first or the second combustion-supporting ring 2.Specifically connect
Connect mode as described below.
Fig. 1-2 is refer to, in the present embodiment, the separation of the first air is provided between the first combustion-supporting ring 1 and central aeration post 3
Plate 43, the first air demarcation strip 43 is 5, corresponds respectively to 5 angles of the central aeration post 3 of totally pentagram shape, specifically,
First combustion-supporting ring 1 is exactly to be connected at 5 jiaos of central aeration post 3 by 5 the first air demarcation strips 43, and now, first is combustion-supporting
Space between ring 1 and central aeration post 3 is divided into 5 small spaces, when air molecule passes through nanometer air lattice, is conducive to
Breaing up for air molecule, plays a part of activating air molecule.Helped on each first air demarcation strip 43 and near first
The part of combustion ring 1 is provided with border passage 5, and border passage 5 is in plum blossom-shaped, and border passage 5 is matched somebody with somebody with above-mentioned center roof vent 31
Close, improve effect of the air by nanometer air lattice.
In the present embodiment, the second combustion-supporting ring 2 is arranged at the inner side of the first combustion-supporting ring 1, and the second combustion-supporting ring 2 divides equally border
Passage 5, is provided with the second air demarcation strip 44 between the second combustion-supporting ring 2 and central aeration post 3, the second air demarcation strip 44 is 5
It is individual, 5 middle parts at angle of the central aeration post 3 of totally pentagram shape are corresponded respectively to, specifically, the second combustion-supporting ring 2 is just
5 jiaos that central aeration post 3 is connected to by 5 the second air demarcation strips 44 of middle part, now, the first combustion-supporting ring 1 or
Space between second combustion-supporting ring 2 and central aeration post 3 is further subdivided into 10 small spaces, further improves air molecule
Activation effect.
Refer to Fig. 1 or Fig. 2, air demarcation strip 4 include cuboid straight panel 41 and with the side edge of cuboid straight panel 41
The curved arc 42 in cross section.Air demarcation strip 4 is arranged to cuboid straight panel 41 and the arc 42 being connected with each other, empty
The inner space of nanometer air lattice is divided into some by qi leel dividing plate 4, and air first passes through cuboid straight panel 41, and cuboid is straight
Plate 41 separates air molecule to be broken up, in the effect by arc 42 so that air molecule passes through rate delivery during arc
Increase, improve intake velocity, then improve effective molecular weight, further improve the power of engine.
Air demarcation strip 4 is obliquely installed between the first combustion-supporting ring 1 and central aeration post 3 or the second combustion-supporting ring 2 and center
Between ventilating column 3, air demarcation strip 4 is obliquely installed in the inside of nanometer air lattice so that air molecule is in nanometer air lattice
The characteristics of showing turbine type, improves the intake velocity of air.
The second combustion-supporting ring 2 in the present embodiment is higher than the first combustion-supporting ring 1, as shown in figure 1, the first combustion-supporting ring 1 just at
Centre position on the height of second combustion-supporting ring 2, so that be arranged at the first sky between the first combustion-supporting ring 1 and central aeration post 3
Qi leel dividing plate 43 and the second air demarcation strip 44 being arranged between the second combustion-supporting ring 2 and central aeration post 3 are in same level
Face, i.e. the first air demarcation strip 43 and the second air demarcation strip 44 are set with layer.
In the present embodiment, nanometer air lattice are on the whole up-narrow and down-wide shape, specifically, the first combustion-supporting ring 1 and second
The internal diameter of combustion-supporting ring 2 is become larger with a lesser extent from top to bottom.The restriction of said structure causes to pass through when air molecule
During this nanometer of air lattice, air intlet is big, and gas outlet is small, improves intake velocity, effective air capacity increase.Of the present utility model
In other embodiment, a nanometer whole height for air lattice can also be increased by increasing the number of plies of nanometer air lattice so that receive
The size of the internal diameter of air inlet and the gas outlet of rice air lattice shows required difference, right under different use conditions to meet
The demand of intake velocity.
As viewed in figures 5-8, according to second embodiment of the present utility model, structure and the original of the present embodiment and first embodiment
Reason is essentially identical, and difference is that in the present embodiment, the second combustion-supporting ring 2 is set directly on border passage 5
So that nanometer air lattice show the combustion-supporting ring 1 of double-decker, i.e., first for bottom（Enter gas-bearing formation）, the second combustion-supporting ring 2 is top layer
（Go out gas-bearing formation）, due to double-decker so that the whole height of nanometer air lattice increases, so when air molecule passes through the present embodiment
Nanometer air lattice when, the intake velocity of air molecule is further lifted, be conducive to improve engine power.
In addition, refer to Fig. 5, when nanometer air lattice are set to double-layer structure, the height of central aeration post 3 is helped for first
The height sum of the combustion-supporting ring 2 of ring 1 and second is fired, now, the first air demarcation strip 43 is also corresponding with the second air demarcation strip 44
Become double-layer structure, when air molecule passes through nanometer air lattice, the air demarcation strip 4 of double-layer structure causes air molecule
Turbine effect becomes apparent from, and is more beneficial for the activation of air molecule.
The description to each implementation method of the utility model is that, in order to more fully understand the utility model, it is only to show above
Example property, and be not intended to limit the utility model.It should be noted that in the above description, for a kind of description of implementation method
And/or the feature for showing can be used in same or similar mode in one or more other embodiments, with other
Feature in implementation method is combined, or substitutes the feature in other embodiment.It will be understood by those skilled in the art that not
Depart from the various change that in the case that utility model of the present utility model conceives, is carried out for implementation method described above and
Modification, belongs in the range of the utility model.
Claims (9)
1. engine nanometer air lattice, it is characterised in that the nanometer air lattice include the first combustion-supporting ring（1）, the second combustion-supporting ring（2）
And central aeration post（3）, the first combustion-supporting ring（1）With the second combustion-supporting ring（2）It is coaxially disposed, the first combustion-supporting ring（1）,
Two combustion-supporting rings（2）And central aeration post（3）Center superposition, the first combustion-supporting ring（1）And the second combustion-supporting ring（2）By air
Demarcation strip（4）It is connected to central aeration post（3）, the air demarcation strip（4）Scattering device is in the first combustion-supporting ring（1）It is logical with center
Gas column（3）Between or the second combustion-supporting ring（2）With central aeration post（3）Between.
2. engine according to claim 1 nanometer air lattice, it is characterised in that the air demarcation strip（4）Including rectangular
Body straight panel（41）And with the cuboid straight panel（41）The curved arc in the cross section of side edge（42）, the air point
Dividing plate（4）It is obliquely installed in the first combustion-supporting ring（1）With central aeration post（3）Between or the second combustion-supporting ring（2）With central aeration post
（3）Between.
3. engine according to claim 1 nanometer air lattice, it is characterised in that the central aeration post（3）Cross section
In totally pentagram shape, the central aeration post（3）Be provided with along its axially through center roof vent（31）.
4. engine according to claim 1 nanometer air lattice, it is characterised in that the first combustion-supporting ring（1）Inner side set
There is border passage（5）, the border passage（5）Located at air demarcation strip（4）On and near the first combustion-supporting ring（1）It
Place.
5. engine according to claim 4 nanometer air lattice, it is characterised in that the border passage（5）In plum blossom-shaped.
6. engine according to claim 5 nanometer air lattice, it is characterised in that the second combustion-supporting ring（2）It is arranged at
One combustion-supporting ring（1）Inner side, the second combustion-supporting ring（2）The respectively border passage（5）, the first combustion-supporting ring（1）With
The central aeration post（3）Between be provided with the first air demarcation strip（43）, the second combustion-supporting ring（2）With the central aeration post
（3）Between be provided with the second air demarcation strip（44）, the second air demarcation strip（44）It is arranged at intervals at the first air point
Dividing plate（43）Between, the first air demarcation strip（43）With the second air demarcation strip（44）It is arranged at same layer.
7. engine according to claim 6 nanometer air lattice, it is characterised in that the first air demarcation strip（43）And the
Two air demarcation strips（44）It is 5.
8. engine according to claim 5 nanometer air lattice, it is characterised in that the second combustion-supporting ring（2）It is arranged at institute
State border passage（5）On, the central aeration post（3）Height be equal to the first combustion-supporting ring（1）With the second combustion-supporting ring（2）'s
Height sum, the first combustion-supporting ring（1）With the central aeration post（3）Between be provided with the first air demarcation strip（43）, it is described
Second combustion-supporting ring（2）With the central aeration post（3）Between be provided with the second air demarcation strip（44）, second air point
Dividing plate（44）It is arranged at intervals at the first air demarcation strip（43）Between, the first air demarcation strip（43）With second air
Demarcation strip（44）Layering is set.
9. engine nanometer air lattice according to any one of claim 1-8, it is characterised in that the nanometer air lattice are in
Up-narrow and down-wide shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621236841.3U CN206280162U (en) | 2016-11-18 | 2016-11-18 | Engine nanometer air lattice |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621236841.3U CN206280162U (en) | 2016-11-18 | 2016-11-18 | Engine nanometer air lattice |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206280162U true CN206280162U (en) | 2017-06-27 |
Family
ID=59083432
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621236841.3U Expired - Fee Related CN206280162U (en) | 2016-11-18 | 2016-11-18 | Engine nanometer air lattice |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206280162U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107061067A (en) * | 2016-11-18 | 2017-08-18 | 吕承哲 | Engine nanometer air lattice |
-
2016
- 2016-11-18 CN CN201621236841.3U patent/CN206280162U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107061067A (en) * | 2016-11-18 | 2017-08-18 | 吕承哲 | Engine nanometer air lattice |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170627 Termination date: 20181118 |