CN201043748Y - Gas burner of producer - Google Patents
Gas burner of producer Download PDFInfo
- Publication number
- CN201043748Y CN201043748Y CNU200720047239XU CN200720047239U CN201043748Y CN 201043748 Y CN201043748 Y CN 201043748Y CN U200720047239X U CNU200720047239X U CN U200720047239XU CN 200720047239 U CN200720047239 U CN 200720047239U CN 201043748 Y CN201043748 Y CN 201043748Y
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- China
- Prior art keywords
- combustion
- burner
- shower nozzle
- air flow
- spinning disk
- Prior art date
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- Expired - Fee Related
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- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Abstract
The utility model provides a gas burner for generator and belongs to the technical field of burner. The burner consists of a burner shell, a shell cover, an air inlet joint, a lance core, a swirl plate, a nozzle and a mixed tube. Combustion-supporting wind respectively forms whirl air flow and circular air flow after getting through the whirl plate, fuel gas flow fractionized by a nozzle excircle and a group of uniformly distributed small holes on an inclined cone, fuel gas sprayed out from a central hole of the nozzle and whirl air flow and circular air flow of combustion-supporting wind intersect in the range of 0 to 90-degree angle, therefore, the utility model can prevent fuel gas which is just sprayed out from fully mixing with combustion-supporting air flow and combustion, local high temperature can be generated, and combustion can be flushed in combustion interval. The utility model mainly used for ceramics furnace and other fuel gas heating equipments.
Description
Technical field
The utility model belongs to technical field of burner, especially is applicable to a kind of producer gas burner of fuel gas buring equipment such as ceramic post sintering kiln such as roller kilns, tunnel cave, shuttle kiln.
Background technology
At present, its gas spray head design of the producer gas burner of domestic use is unreasonable, gas-flow is not carried out comprehensive thin stock stream, make combustion air to the undercompounding of gas-flow, inhomogeneous, influenced burning velocity, it is low to reduce ignition temperature, the heat loss due to incomplete combustion is big, the easy coking of shower nozzle makes the harmful substance in the coal gas be difficult to decompose not environmental protection simultaneously.In addition, gas-flow is concentrated ejection, forms localized hyperthermia easily, burns out parts such as spinning disk, shower nozzle, mixing tube, makes the NOx product increase simultaneously.
Summary of the invention
The utility model provides a kind of producer gas burner, it is unreasonable to solve the gas spray head design, producing localized hyperthermia makes the NOx product increase, burn out the technical problem of burner part, gas-flow is carried out omnibearing thin stock stream, combustion air and gas-flow are mixed, fully, the order burning is evenly tiling on burner interval, improves burning quality and efficient.
The technical scheme in the invention for solving the above technical problem is: a kind of producer gas burner, it is by the burner shell, casing cover, inlet suction port, the rifle core, spinning disk, shower nozzle, mixing tube is formed, combustion air is via the burner shell, casing cover, mixing tube, the passage ejection that spinning disk is formed, be characterized in that a combustion air part is equally distributed on the spinning disk cylindrical, become the skewed slot ejection of a α angle with flame ejection central shaft, form swirling eddy, the aperture ejection of another part one group of evenly distributed axis and central axes on the spinning disk end face forms annular flow.Combustion gas from inlet suction port enter, through the passage that rifle core, spinning disk, shower nozzle are formed, a part is by one group of equally distributed aperture ejection on shower nozzle cylindrical, the oblique cone, a part is sprayed by the shower nozzle centre bore.Shower nozzle is threaded with spinning disk, gas-flow and combustion air swirling eddy, annular flow intersect in the scope at 0-90 ° of angle, so just prevent that combustion gas from just just having sprayed and combustion air current mixed combustion cmpletely, produce localized hyperthermia, burning can evenly be tiled on burner interval.One group of equally distributed aperture has segmented gas-flow on shower nozzle cylindrical, the oblique cone, makes it more full and uniform with mixing of combustion air current, and it is more stable to burn, and has reduced the heat loss due to incomplete combustion.
Compared with prior art, the utlity model has following beneficial effect: use the situation of mixing that the utility model can improve combustion air and combustion gas, avoid producing the phenomenon that localized hyperthermia increases the NOx product, the order burning is evenly tiling on burner interval, burning rapidly, the combustion space calorific intensity is big, combustion thermal efficiency height, environmental protection.
Description of drawings
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is the profilograph of an embodiment of the present utility model.
Fig. 2 is the installation diagram of facing of spinning disk and valve.
Fig. 3 is that full sectional view is looked on the right side of Fig. 2.
Fig. 4 is the right view of Fig. 2.
1. inlet suction ports among the figure, 2. casing cover, 3. rifle core, 4. combustion air air inlet, 5. shell, 6. mixing tube, 7. spinning disk, 8. shower nozzle, 9. spinning disk cylindrical skewed slot, 10. spinning disk end face aperture 11. shower nozzle cylindrical apertures, 12. shower nozzle scalene cone apertures, 13. shower nozzle centre bores.
The specific embodiment
Now be further elaborated with regard to an embodiment of the present utility model in conjunction with the accompanying drawings.
Combustion air enters from combustion air air inlet 4 in the accompanying drawings, passage through casing cover 2, shell 5, mixing tube 6, spinning disk 7 compositions, spinning disk cylindrical skewed slot 9 and 10 ejections of spinning disk end face aperture by uniform arrangement on the spinning disk 7, wherein through spinning disk cylindrical skewed slot 9 ejection be swirling eddy, through 10 ejections of spinning disk end face aperture are annular flows.With the burner central shaft is axle, spinning disk cylindrical skewed slot 9 and spinning disk end face aperture 10 are made swirling eddy passage and the annular flow passage that circumference array forms spinning disk 7 respectively, the quantity of spinning disk cylindrical skewed slot 9 is no less than 16, the quantity of spinning disk end face aperture 10 is no less than 8, the distribution circle diameter of aperture is greater than the diameter of shower nozzle, skewed slot becomes a α angle with central shaft, aperture 10 axis and central axes.The passage that combustion gas is formed through inlet suction port 1, rifle core 3, spinning disk 7, shower nozzle 8 is by shower nozzle cylindrical aperture 11 evenly distributed on the shower nozzle external cylindrical surface, on the scalene cone, shower nozzle scalene cone aperture 12 and 13 ejections of shower nozzle centre bore.Shower nozzle 8 is threaded with spinning disk 7.The axis of shower nozzle centre bore 13 and burner central axes.With the burner central shaft is axle, and shower nozzle cylindrical aperture 11, shower nozzle scalene cone aperture 12 form equally distributed thin strand of combustion gas ejection passage as circumference array respectively, and the circumferential arrangement quantity of shower nozzle cylindrical aperture 11, shower nozzle scalene cone aperture 12 is no less than 6.Shower nozzle cylindrical aperture 11 is arranged in two rows on the face of cylinder, do between the every row of aperture of circumference array the arrangement that interlaces on axial section of angle with 180 °/n, and wherein n is the little hole number of a circumference array.The aperture of shower nozzle cylindrical aperture 11, shower nozzle scalene cone aperture 12 is selected between the 6mm at 4mm, and the cone angle of shower nozzle oblique cone is selected between 80 ° to 110 °. and the aperture of shower nozzle centre bore 13 is selected between the 10mm at 8mm.Gas-flow and combustion air swirling eddy, annular flow intersect in the scope at 0-90 ° of angle, make burned flame that a suitable length, uniformity of temperature profile, flameholding be arranged.
Claims (1)
1. producer gas burner, it is by the burner shell, casing cover, inlet suction port, the rifle core, spinning disk, shower nozzle, mixing tube is formed, described burner shell, casing cover, mixing tube, spinning disk is formed the combustion air passage, described inlet suction port, the rifle core, spinning disk, shower nozzle is formed blast tube, it is characterized in that: described shower nozzle is made up of the cylinder and the cone of hollow, the cone angle of cone is selected between 80 ° to 110 °, be distributed with two rows on the external cylindrical surface, be distributed with the evenly distributed number of the arrangement of a row on the scalene cone and be no less than 6 combustion gas ejection aperture, hole diameter is selected between the 6mm at 4mm, between every row with the arrangement that on axial section, interlaces of the angle of 180 °/n, wherein n is the little hole number of a circumference array, the shower nozzle center drilling, the diameter of centre bore is selected between the 10mm at 8mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU200720047239XU CN201043748Y (en) | 2007-01-12 | 2007-01-12 | Gas burner of producer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU200720047239XU CN201043748Y (en) | 2007-01-12 | 2007-01-12 | Gas burner of producer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201043748Y true CN201043748Y (en) | 2008-04-02 |
Family
ID=39258642
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU200720047239XU Expired - Fee Related CN201043748Y (en) | 2007-01-12 | 2007-01-12 | Gas burner of producer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201043748Y (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102226522A (en) * | 2011-06-01 | 2011-10-26 | 中国科学院广州能源研究所 | Gas burner |
| CN105605578A (en) * | 2016-01-31 | 2016-05-25 | 参化（上海）能源科技有限公司 | Combustor |
| CN106500096A (en) * | 2016-12-14 | 2017-03-15 | 北京京诚凤凰工业炉工程技术有限公司 | gas burner |
| CN107763622A (en) * | 2017-11-14 | 2018-03-06 | 丁光学 | Kiln burner |
| CN108758635A (en) * | 2018-07-06 | 2018-11-06 | 广东科达洁能股份有限公司 | A kind of kiln whirlwind sheet |
| CN109595554A (en) * | 2019-01-23 | 2019-04-09 | 四川福蓉科技股份公司 | A kind of burner and the heating device with burner |
| CN109813103A (en) * | 2017-11-22 | 2019-05-28 | 中国瑞林工程技术股份有限公司 | Tuyere device and its application for side-blown converter |
| CN110513688A (en) * | 2019-09-18 | 2019-11-29 | 安德森热能科技（苏州）有限责任公司 | A kind of low nitrogen air heating turbulent burner |
| CN111121005A (en) * | 2019-12-02 | 2020-05-08 | 中国科学院过程工程研究所 | Decoupling gas burner and using method thereof |
| CN110513688B (en) * | 2019-09-18 | 2024-07-16 | 安德森热能科技（苏州）有限责任公司 | Low nitrogen air heating cyclone burner |
-
2007
- 2007-01-12 CN CNU200720047239XU patent/CN201043748Y/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102226522A (en) * | 2011-06-01 | 2011-10-26 | 中国科学院广州能源研究所 | Gas burner |
| CN105605578A (en) * | 2016-01-31 | 2016-05-25 | 参化（上海）能源科技有限公司 | Combustor |
| CN106500096A (en) * | 2016-12-14 | 2017-03-15 | 北京京诚凤凰工业炉工程技术有限公司 | gas burner |
| CN107763622A (en) * | 2017-11-14 | 2018-03-06 | 丁光学 | Kiln burner |
| CN109813103A (en) * | 2017-11-22 | 2019-05-28 | 中国瑞林工程技术股份有限公司 | Tuyere device and its application for side-blown converter |
| CN108758635A (en) * | 2018-07-06 | 2018-11-06 | 广东科达洁能股份有限公司 | A kind of kiln whirlwind sheet |
| CN108758635B (en) * | 2018-07-06 | 2024-03-12 | 佛山市科达机电有限公司 | Kiln cyclone sheet |
| CN109595554A (en) * | 2019-01-23 | 2019-04-09 | 四川福蓉科技股份公司 | A kind of burner and the heating device with burner |
| CN110513688A (en) * | 2019-09-18 | 2019-11-29 | 安德森热能科技（苏州）有限责任公司 | A kind of low nitrogen air heating turbulent burner |
| CN110513688B (en) * | 2019-09-18 | 2024-07-16 | 安德森热能科技（苏州）有限责任公司 | Low nitrogen air heating cyclone burner |
| CN111121005A (en) * | 2019-12-02 | 2020-05-08 | 中国科学院过程工程研究所 | Decoupling gas burner and using method thereof |
| CN111121005B (en) * | 2019-12-02 | 2021-04-09 | 中国科学院过程工程研究所 | Decoupling gas burner and using method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080402 Termination date: 20150112 |
|
| EXPY | Termination of patent right or utility model |