CN201568162U - Flow-disturbing mixer - Google Patents
Flow-disturbing mixer Download PDFInfo
- Publication number
- CN201568162U CN201568162U CN2009202796566U CN200920279656U CN201568162U CN 201568162 U CN201568162 U CN 201568162U CN 2009202796566 U CN2009202796566 U CN 2009202796566U CN 200920279656 U CN200920279656 U CN 200920279656U CN 201568162 U CN201568162 U CN 201568162U
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- CN
- China
- Prior art keywords
- mixer
- air cavity
- injection pipe
- mixed air
- gas
- 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.)
- Expired - Lifetime
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/30—Use of alternative fuels, e.g. biofuels
Abstract
The utility model discloses a flow-disturbing mixer which comprises a mixer body, wherein a mixed air cavity is arranged in the mixer body, a gas distributing cavity which surrounds the mixed air cavity is arranged in the mixer body, the inner wall of the gas distributing cavity is fixed with a spray pipe which penetrates through the mixed air cavity, and an auxiliary gas jet orifice is arranged on the pipe wall of the spray pipe. Firstly, the spray pipe, which penetrates through the mixed air cavity, enables gas to be carried to the centermost of the mixed air cavity along the spray pipe, secondly, the inner wall of the gas distributing cavity is provided with jet orifices which are communicated with the gas distributing cavity, the jet orifices and the spray pipe enlarge the air and gas mixing area together, and air and gas are move thoroughly and evenly mixed. With the technical solution, the flow-disturbing mixer not only can lead the rare burning limit of combustion of the engine to be improved by 15%, but also can lower the gas consumption and exhaust temperature of the engine, and improves the operation economy of vehicles.
Description
Technical field
The utility model relates to a kind of gas engine technical field, relates in particular to a kind of gas mixing unit.
Background technique
Along with popularizing of developing of automobile industry and automobile consumption, the demand and the dependence of fuel oil become increasingly conspicuous, begun to cause people's attention through the automobile of repacking, combustion gas fuel.And China has abundant natural gas resource, and gas-fueled vehicles have become noticeable new generation of environment protection automobile.Fuel gas mixer on the automobile is that combustion gas and air are fully mixed formation inflammable mixture supply engine.Because the relative gasoline of energy that gas fuel combustion discharges is much smaller, when air and combustion gas mixing are inhomogeneous, can cause the burning lean flammability limit of motor car engine narrower, so, can mixer combustion gas and air fully, mix equably, and can be related to motor car engine normally stably move.
In the prior art, through long-term development, a lot of structure types has appearred in the engine gas mixer, sum up, technological scheme mainly is: combustion gas enters mixer cavity by the gas jet orifice on the mixer cavity wall, described gas jet orifice is circular and is distributed on the mixer cavity wall, remove this, on perpendicular to the direction of annulus, also be provided with double gas jet orifice, though can being combustion gas, these spray orifice settings spray into the mixer cavity from different angles, but, when air when an end of inner chamber enters the inner chamber, will dispel combustion gas near internal chamber wall, combustion gas can not enter into the central authorities of air stream, mixes with the full and uniform of combustion gas so can not realize air.
The model utility content
Technical problem to be solved in the utility model provides a kind of turbulence mixer that makes combustion gas and the well-mixed motor of air.
For solving the problems of the technologies described above, the technical solution of the utility model is: turbulence mixer, comprise the mixing body, be provided with mixed air cavity in the described mixing body, one end of described mixed air cavity is provided with air intlet, and the other end of described mixed air cavity is provided with mixed gas outlet, is provided with the combustion gas distribution chamber around described mixed air cavity in the described mixing body, the outer wall of described combustion gas distribution chamber is provided with fuel gas inlet, and the inwall of described combustion gas distribution chamber is provided with the main gas jet orifice that is communicated with described mixed air cavity; Be fixed with the injection pipe that runs through described mixed air cavity on the inwall of described combustion gas distribution chamber, the inner chamber of described injection pipe and described combustion gas distribution chamber are communicated with, and the tube wall of described injection pipe is provided with secondary gas jet orifice.
As a kind of embodiment, described mixing body comprises mixer case, and the inner chamber of described mixer case is cylindrical, and the inner chamber of described mixer case is socketed with trunnion, and described trunnion and described mixer case form described combustion gas distribution chamber.
As a kind of embodiment, described injection pipe passes the center of described mixed air cavity.
As a kind of embodiment, described secondary gas jet orifice is perpendicular to the air inlet direction.
As a kind of embodiment, at least two of described injection pipes, described injection pipe circumferentially is distributed on the described trunnion, and described injection pipe does not spatially intersect mutually.
As a kind of embodiment, the main gas jet orifice on the described trunnion wall is distributed on the described trunnion ringwise, and between described injection pipe.
As a kind of embodiment, described air intlet is the big inverted cone reducing in outer end, and the angle of inverted cone reducing is 30 °.
Adopt the beneficial effect of the technical program to be: at first, to run through the injection pipe of described mixed air cavity, make combustion gas be brought to the most central of mixed air cavity along injection pipe; Secondly, the inwall of described combustion gas distribution chamber is provided with spray orifice, and these spray orifices communicate with the combustion gas distribution chamber, and these spray orifices have strengthened the area of air and combustion gas mixing with injection pipe, and the mixing that makes both more fully and even; Adopt the technical program, not only can make the lean flammability limit of engine combustion improve 15%, can also reduce the gas consumption and the delivery temperature of motor, improve the Economy of vehicle operating.
Described injection pipe is provided with a lot of spray orifices, and the direction of these spray orifices is vertical with the flow direction of air, and the injection of combustion gas not only is not subjected to the influence of resistance of air, and air ground flows and can also be beneficial to combustion gas and spray in bigger scope.
Description of drawings
Below in conjunction with the drawings and specific embodiments the utility model is further described.
Fig. 1 is the utility model embodiment's a structure principle chart;
Fig. 2 is the right elevation of Fig. 1;
Among the figure: 1. mixer case, 2. trunnion, 3. air intlet, 4. fuel gas inlet, 5. mixed gas outlet, 6. mixed air cavity, 7. combustion gas distribution chamber, 8. injection pipe, 9. main gas jet orifice, 10. secondary gas jet orifice.
Embodiment
As shown in Figure 1, a kind of turbulence mixer, comprise the mixing body, be provided with mixed air cavity 6 in the described mixing body, an end of mixed air cavity 6 is provided with air intlet 3, air intlet 3 is the big inverted cone reducing in outer end, the reducing angle is 30 °, and the other end is provided with mixed gas outlet 5, mixes the combustion gas distribution chamber 7 that is provided with in the body around mixed air cavity 6, the outer wall of combustion gas distribution chamber 7 is provided with fuel gas inlet 4, and the inwall of combustion gas distribution chamber 7 also is provided with the main gas jet orifice 9 that is communicated with described mixed air cavity 6; Also be fixed with the injection pipe 8 that runs through mixed air cavity 6 on the inwall of described combustion gas distribution chamber 7, injection pipe 8 passes the center of mixed air cavity 6, and described injection pipe 8 is provided with two at least, and injection pipe 8 circumferentially is distributed on the trunnion 2, and injection pipe 8 does not spatially intersect mutually.The inner chamber of described injection pipe 8 and combustion gas distribution chamber 7 are communicated with, and are provided with secondary gas jet orifice 10 on the tube wall of injection pipe 8, and secondary gas jet orifice 10 is perpendicular to the air inlet direction.Mix body and comprise mixer case 1, the inner chamber of mixer case 1 is cylindrical, and is socketed with trunnion 2 at the inner chamber of mixer case 1, and trunnion 2 and mixer case 1 form foregoing combustion gas distribution chamber 7.As previously mentioned, the main gas jet orifice 9 on trunnion 2 walls is distributed on the trunnion 2 ringwise, and between two injection pipes 8.
During mixer work, be example with the rock gas, rock gas sprays into the combustion gas distribution chamber 7 from fuel gas inlet 4, and pressure is 7～9bar; Air enters the mixed air cavity 6 from air intlet 3, pressure is 1～2bar, at this moment, in combustion gas distribution chamber 7 and injection pipe 8, all contain rock gas, because there are the pressure difference of 5～8bar in rock gas and air, under this action of pressure, rock gas sprays into by main gas jet orifice 9 on the trunnion 2 and the secondary gas jet orifice 10 on the injection pipe 8 in the middle of the air in the mixed air cavity 6, forms mixed gas.Different with existing mixer, this mixer is provided with injection pipe 8 in mixed air cavity 6, article two, injection pipe 8 intersects the status in the inside of mixed air cavity 6 on direction, and all be provided with many secondary gas jet orifices 10 on the wall of every injection pipe 8, secondary gas jet orifice 10 runs through injection pipe 8 tube walls, and direction is vertical with air ground flow direction, like this, not only can make combustion gas can arrive the center of air draught by the inner chamber of injection pipe 8, flowing of air also can be accelerated the mixing velocity of air and rock gas.When the structure of injection pipe 8 and the secondary gas jet orifice on the injection pipe 8 10 strengthen rock gases and Air mixing degree, distribute, be arranged in rock gas that main gas jet orifices 9 in the middle of two injection pipes 8 also can make combustion gas distribution chamber 7 on trunnion 2 walls ringwise and spray into mixed air cavity 6 around the inwall of trunnion 2.Simultaneously, air intlet 3 is set to 30 ° inverted cone reducing, and injection pipe 8 places in mixed air cavity 6 can form Venturi effect, produce an area of low pressure herein, have accelerated air ground and have flowed.
In the technical program, by injection pipe 8 being set in mixed air cavity 6, being provided with etc. in the 30 degree reducings that secondary gas jet orifice 10 are set on the injection pipe 8, main gas jet orifice 9 and air intlet be set on mixed air cavity 6 walls, the good effect acting in conjunction of this several places design, make that the mixing of air and rock gas is more abundant, more even.
All are from design of the present utility model, and the structure conversion of having done without creative work all drops within the protection domain of the present utility model.
Claims (8)
1. turbulence mixer, comprise the mixing body, be provided with mixed air cavity in the described mixing body, one end of described mixed air cavity is provided with air intlet, the other end of described mixed air cavity is provided with mixed gas outlet, be provided with the combustion gas distribution chamber around described mixed air cavity in the described mixing body, the outer wall of described combustion gas distribution chamber is provided with fuel gas inlet, and the inwall of described combustion gas distribution chamber is provided with the main gas jet orifice that is communicated with described mixed air cavity; It is characterized in that:
Be fixed with the injection pipe that runs through described mixed air cavity on the inwall of described combustion gas distribution chamber, the inner chamber of described injection pipe and described combustion gas distribution chamber are communicated with, and the tube wall of described injection pipe is provided with secondary gas jet orifice.
2. turbulence mixer as claimed in claim 1, it is characterized in that: described mixing body comprises mixer case, the inner chamber of described mixer case is cylindrical, and the inner chamber of described mixer case is socketed with trunnion, and described trunnion and described mixer case form described combustion gas distribution chamber.
3. turbulence mixer as claimed in claim 2 is characterized in that: described injection pipe passes the center of described mixed air cavity.
4. turbulence mixer as claimed in claim 3 is characterized in that: described secondary gas jet orifice is perpendicular to the air inlet direction.
5. turbulence mixer as claimed in claim 3 is characterized in that: at least two of described injection pipes, described injection pipe circumferentially is distributed on the described trunnion, and described injection pipe does not spatially intersect mutually.
6. turbulence mixer as claimed in claim 5 is characterized in that: the main gas jet orifice on the described trunnion wall is distributed on the described trunnion ringwise, and between described injection pipe.
7. as the described turbulence mixer of the arbitrary claim of claim 1-6, it is characterized in that: described air intlet is the big inverted cone reducing in outer end.
8. turbulence mixer as claimed in claim 7 is characterized in that: described inverted cone reducing is 30 ° of inverted cone reducings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202796566U CN201568162U (en) | 2009-11-07 | 2009-11-07 | Flow-disturbing mixer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202796566U CN201568162U (en) | 2009-11-07 | 2009-11-07 | Flow-disturbing mixer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201568162U true CN201568162U (en) | 2010-09-01 |
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ID=42660447
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009202796566U Expired - Lifetime CN201568162U (en) | 2009-11-07 | 2009-11-07 | Flow-disturbing mixer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201568162U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106401802A (en) * | 2015-08-12 | 2017-02-15 | 上海海能汽车电子有限公司 | Mixer with cross-shaped core |
| CN111237094A (en) * | 2020-03-11 | 2020-06-05 | 广西玉柴机器股份有限公司 | Large-scale gas engine mixer |
-
2009
- 2009-11-07 CN CN2009202796566U patent/CN201568162U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106401802A (en) * | 2015-08-12 | 2017-02-15 | 上海海能汽车电子有限公司 | Mixer with cross-shaped core |
| CN111237094A (en) * | 2020-03-11 | 2020-06-05 | 广西玉柴机器股份有限公司 | Large-scale gas engine mixer |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: WEICHAI XIGANG NEW ENERGY POWER CO., LTD. Free format text: FORMER NAME: WEIFANG WEICHAI PEIXIN GAS ENGINE CO., LTD. |
|
| CP01 | Change in the name or title of a patent holder |
Address after: 261061 Shandong city in Weifang province Fu hi tech Industrial Development Zone, East Street No. 197 Patentee after: WEICHAI XIGANG NEW ENERGY POWER CO., LTD. Address before: 261061 Shandong city in Weifang province Fu hi tech Industrial Development Zone, East Street No. 197 Patentee before: Weichai Peterson Gas Diesel Engines Co., Ltd. |
|
| CX01 | Expiry of patent term |
Granted publication date: 20100901 |
|
| CX01 | Expiry of patent term |