CN115143478A - Tail gas treatment method - Google Patents
Tail gas treatment method Download PDFInfo
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- CN115143478A CN115143478A CN202210827164.6A CN202210827164A CN115143478A CN 115143478 A CN115143478 A CN 115143478A CN 202210827164 A CN202210827164 A CN 202210827164A CN 115143478 A CN115143478 A CN 115143478A
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- tail gas
- pipe
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- combustion
- gas
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- 238000000034 method Methods 0.000 title claims abstract description 12
- 239000007789 gas Substances 0.000 claims abstract description 145
- 238000002485 combustion reaction Methods 0.000 claims abstract description 68
- 239000002737 fuel gas Substances 0.000 claims description 6
- 238000006864 oxidative decomposition reaction Methods 0.000 claims description 4
- GNFTZDOKVXKIBK-UHFFFAOYSA-N 3-(2-methoxyethoxy)benzohydrazide Chemical compound COCCOC1=CC=CC(C(=O)NN)=C1 GNFTZDOKVXKIBK-UHFFFAOYSA-N 0.000 claims description 3
- FGUUSXIOTUKUDN-IBGZPJMESA-N C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 Chemical compound C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 FGUUSXIOTUKUDN-IBGZPJMESA-N 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 3
- 239000002912 waste gas Substances 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims description 2
- 239000000126 substance Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000011345 viscous material Substances 0.000 description 1
- 239000002918 waste heat Substances 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G7/00—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
- F23G7/06—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases
- F23G7/061—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases with supplementary heating
- F23G7/065—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases with supplementary heating using gaseous or liquid fuel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G5/00—Incineration of waste; Incinerator constructions; Details, accessories or control therefor
- F23G5/44—Details; Accessories
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES
- F23J15/00—Arrangements of devices for treating smoke or fumes
- F23J15/02—Arrangements of devices for treating smoke or fumes of purifiers, e.g. for removing noxious material
- F23J15/022—Arrangements of devices for treating smoke or fumes of purifiers, e.g. for removing noxious material for removing solid particulate material from the gasflow
- F23J15/025—Arrangements of devices for treating smoke or fumes of purifiers, e.g. for removing noxious material for removing solid particulate material from the gasflow using filters
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G2204/00—Supplementary heating arrangements
- F23G2204/10—Supplementary heating arrangements using auxiliary fuel
- F23G2204/103—Supplementary heating arrangements using auxiliary fuel gaseous or liquid fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
- F23G2209/00—Specific waste
- F23G2209/14—Gaseous waste or fumes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES
- F23J2217/00—Intercepting solids
- F23J2217/10—Intercepting solids by filters
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Environmental & Geological Engineering (AREA)
- Incineration Of Waste (AREA)
Abstract
The invention relates to a tail gas treatment method, which is based on a novel tail gas incinerator, and comprises an incineration component, wherein the incineration component comprises: a tail gas pipe; the first slip ring is slidably arranged on the tail gas pipe; the second slip ring is slidably arranged on the tail gas pipe; the combustion plates are circumferentially arrayed at the tail end of the tail gas pipe, and the inner sides of the combustion plates are hinged with the first sliding ring; two ends of the connecting rod are hinged with the combustion plate and the second sliding ring respectively; and the gas pipe is communicated with the combustion plate. The novel tail gas incinerator can effectively increase the supply amount of fresh air in the incinerator body, the size, the position, the direction and the diffusivity of formed incineration flame are adjustable, targeted adjustment can be performed on different tail gases, and the incineration efficiency of the tail gas incinerator is improved.
Description
Technical Field
The invention relates to the technical field of tail gas treatment, in particular to a tail gas treatment method.
Background
The tail gas incinerator utilizes the heat produced by combustion of auxiliary fuel to raise the temperature of combustible harmful gas to reaction temperature so as to produce oxidation decomposition. The tail gas incinerator is suitable for treating tail gas of spraying and drying equipment and purifying harmful gas emitted in petrochemical industry, medicine industry and other industries. The method has the advantages of purifying the gas containing water-soluble or viscous substances and high molecular substances in the organic tail gas. The requirements of environmental protection and labor protection are met, and meanwhile, heat exchange equipment is added, so that the purposes of waste heat recycling and energy saving are achieved.
The incinerator in the prior art often appears because the air input is not enough to lead to burning inadequately to influence tail gas incineration's efficiency, and to different tail gases, the size, shape and the position of the burning flame of incinerator all need to carry out the adjustment of pertinence, but the burning flame that the incinerator among the prior art formed only can carry out size control, and flame shape and position can't be adjusted, has also influenced the incineration efficiency to different tail gases.
Disclosure of Invention
In order to solve the technical problems in the background art, the invention provides a tail gas treatment method, which is based on a novel tail gas incinerator, can effectively increase the supply amount of fresh air in the incinerator body, and the size, position, direction and diffusivity of formed incineration flame can be adjusted, and the incineration efficiency of the tail gas incinerator can be improved by performing targeted adjustment on different tail gases.
The technical scheme adopted by the invention for solving the technical problem is as follows:
a new-type tail gas burns burning furnace, includes the subassembly of burning, burns the subassembly and includes:
a tail gas pipe;
the first slip ring is slidably arranged on the tail gas pipe;
the second slip ring is slidably arranged on the tail gas pipe;
the combustion plates are circumferentially arrayed at the tail end of the tail gas pipe, and the inner sides of the combustion plates are hinged with the first sliding ring;
two ends of the connecting rod are respectively hinged with the combustion plate and the second slip ring;
and the gas pipe is communicated with the combustion plate.
Further, still include the air intake assembly, the air intake assembly includes:
the first air inlet pipe is communicated with the outside;
the second air inlet pipe is communicated with the furnace body;
the air inlet cavity is arranged between the first air inlet pipe and the second air inlet pipe;
the air inlet turbine is rotatably arranged in the air inlet cavity;
the first exhaust pipe is communicated with the furnace body;
the second exhaust pipe is communicated with the outside;
the exhaust cavity is arranged between the first exhaust pipe and the second exhaust pipe;
and the exhaust turbine is rotatably arranged in the exhaust cavity and is in transmission connection with the air inlet turbine.
Further, the incineration assembly further comprises:
the fixing table is arranged on the tail gas pipe;
the first driving ring is arranged on the tail gas pipe in a sliding mode and fixed with the first sliding ring through a first connecting shaft;
the second driving ring is arranged on the tail gas pipe in a sliding mode and is fixed with the second sliding ring through a second connecting shaft;
the first electric cylinder is arranged between the fixed platform and the first driving ring;
and the second electric cylinder is arranged between the fixed table and the second driving ring.
Further, the lower end of the furnace body is provided with a gas distribution ring which is communicated with the gas pipe; the gas hole that corresponds with the combustion plate is seted up to the gas ring upper end, and the gas hole passes through gas hose and combustion plate intercommunication.
Further, the combustion plate is of a cavity structure, a plurality of combustion holes are formed in one side, facing the tail gas pipe, of the combustion plate, and the combustion holes are inclined towards the same horizontal direction.
Furthermore, the second exhaust pipe and the tail gas pipe are provided with filters.
A working method of a novel tail gas incinerator comprises the following steps:
a. tail gas enters the furnace body through a tail gas pipe;
b. the fuel gas enters the combustion plate through the fuel gas pipe, the gas distribution ring and the fuel gas hose and is sprayed out and combusted through the combustion holes;
c. the gas sprayed out of the combustion holes is combusted and heated, so that the tail gas sprayed out of the tail gas pipe is subjected to oxidative decomposition reaction;
d. the combusted waste gas is exhausted through the first exhaust pipe, the exhaust cavity and the second exhaust pipe;
e. when the waste gas is discharged, the exhaust turbine in the exhaust cavity is driven to rotate, the air inlet turbine and the exhaust turbine rotate synchronously, the rotating air inlet turbine promotes the external air to enter the furnace body through the first air inlet pipe, the air inlet cavity and the second air inlet pipe, and the air supply amount in the furnace body is effectively increased.
f. The first electric cylinder drives the inner end of the combustion plate to move along the axial direction of the tail gas pipe through a first driving ring, a first connecting shaft and a first slip ring;
g. the second electric cylinder drives the outer end of the combustion plate to move along the axial direction of the tail gas pipe through a second driving ring, a second connecting shaft and a second slip ring;
h. combining step f and step g, can adjusting the position and the angle of opening and shutting of combustion plate relative to the tail gas pipe to adjust the position and the direction of gas flame on the combustion plate, thereby realize different tail gas combustion effects.
The invention has the beneficial effects that:
(1) The supply amount of air in the furnace body can be effectively increased through the air inlet assembly, and the incineration efficiency of the tail gas incinerator is improved.
(2) The size, the position, the direction and the diffusivity of incineration flame formed by the incineration assembly are adjustable, and the incineration efficiency of tail gas can be improved by pertinently adjusting different tail gases.
Drawings
The invention is further illustrated with reference to the following figures and examples.
FIG. 1 is a cross-sectional view of the present invention;
FIG. 2 is a schematic structural view of an incineration assembly according to the invention;
FIG. 3 is a schematic view of the construction of an incineration assembly according to the invention;
FIG. 4 is a schematic structural view of the air intake assembly of the present invention;
fig. 5 is a schematic structural diagram of the present invention.
In the figure:
1. the gas stove comprises a tail gas pipe, 2 a fixed platform, 3 a first electric cylinder, 4 a second electric cylinder, 5 a gas pipe, 6 a gas distribution ring, 7 a stove body, 8 a gas hose, 9 a combustion plate, 10 a first exhaust pipe, 11 an exhaust cavity, 12 an exhaust turbine, 13 an air inlet cavity, 14 an air inlet turbine, 15 a first air inlet pipe, 16 a second air inlet pipe, 17 a second exhaust pipe, 18 a connecting rod, 19 a first sliding ring, 20 a second sliding ring, 21 a first driving ring, 22 a second driving ring, 23 a first connecting shaft, 24 a second connecting shaft and 101 an air outlet part.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
As shown in fig. 1-3, a novel tail gas incinerator comprises an incineration assembly, wherein the incineration assembly comprises: a tail gas pipe 1; the tail gas pipe 1 is sleeved with a first slip ring 19 and a second slip ring 20, and the first slip ring 19 and the second slip ring 20 can slide on the tail gas pipe 1 along the axial direction of the tail gas pipe; a plurality of combustion plates 9 are circumferentially arrayed on the periphery of the upper end of the tail gas pipe 1, and the inner sides of the combustion plates 9 are hinged with a first sliding ring 19; a connecting rod 18 is arranged on the outer side of the combustion plate 9, and two ends of the connecting rod 18 are respectively hinged with the combustion plate 9 and a second sliding ring 20; the combustion plate 9 is of a cavity structure, a plurality of combustion holes are formed in one side, facing the tail gas pipe 1, of the combustion plate 9, and the combustion holes are inclined towards the same horizontal direction and communicated with the combustion plate 9. The lower end of the furnace body 7 is provided with a gas distribution ring 6, and the gas distribution ring 6 is communicated with the gas pipe 5; the gas hole that corresponds with combustion plate 9 is seted up to the 6 upper ends of gas ring, and the gas hole passes through gas hose 8 and combustion plate 9 intercommunication. The gas enters the gas distribution ring 6 through the gas pipe 5, the gas in the gas distribution ring 6 enters the cavity of the combustion plate 9 through the gas hoses 8, and then is sprayed out through the combustion holes to form combustion flame.
For driving the first and second slip rings 19, 20, the incineration assembly further comprises: the fixed station 2 is fixedly arranged at the lower end of the tail gas pipe 1; the first driving ring 21 is sleeved on the tail gas pipe 1, the first driving ring 21 can slide along the axial direction of the tail gas pipe 1, and the first driving ring 21 is fixedly connected with the first sliding ring 19 through a first connecting shaft 23; the second driving ring 22 is sleeved on the exhaust pipe 1, the second driving ring 22 can slide along the axial direction of the exhaust pipe 1, and the second driving ring 22 is fixed with the second slip ring 20 through the second connecting shaft 24. In order to ensure that the mechanisms can operate independently and do not generate interference, the first connecting shaft 23 and the second connecting shaft 24 are arranged at intervals in a staggered mode, a through hole for the second connecting shaft 24 to penetrate through is formed in the first driving ring 21, and a through hole for the first connecting shaft 23 to penetrate through is formed in the second sliding ring 20.
Furthermore, the first driving ring 21 is driven by the first electric cylinder 3, the first electric cylinder 3 is arranged between the fixed table 2 and the first driving ring 21, the cylinder end of the first electric cylinder 3 is fixedly connected with the fixed table 2, and the cylinder end of the first electric cylinder 3 is fixedly connected with the first driving ring 21; the second driving ring 22 is driven by a second electric cylinder 4, the second electric cylinder 4 is arranged between the fixed table 2 and the second driving ring 22, the cylinder end of the second electric cylinder 4 is fixedly connected with the fixed table 2, and the cylinder end of the second electric cylinder 4 is fixedly connected with the second driving ring 22. Both the first electric cylinder 3 and the second electric cylinder 4 are controlled by their respective controllers.
As shown in fig. 4, in order to increase the air intake amount and improve the incineration efficiency of the new-type tail gas incinerator, the device further comprises an air intake assembly, wherein the air intake assembly comprises: a first intake pipe 15 communicating with the outside; a second air inlet pipe 16 communicated with the furnace body 7; an intake chamber 13 provided between the first intake pipe 15 and the second intake pipe 16; a rotatable air inlet turbine 14 is arranged in the air inlet cavity 13, and the rotation of the air inlet turbine 14 can accelerate the air in the first air inlet pipe 15 into the second air inlet pipe 16; the furnace also comprises a first exhaust pipe 10 communicated with the furnace body 7; a second exhaust pipe 17 communicating with the outside; an exhaust chamber 11 provided between the first exhaust pipe 10 and the second exhaust pipe 17; the exhaust cavity 11 is internally provided with a rotatable exhaust turbine 12, when gas in the first exhaust pipe 10 enters the second exhaust pipe 17 through the exhaust cavity 11, the exhaust turbine 12 can be driven to rotate, the exhaust turbine 12 is coaxially connected with the air inlet turbine 14, and the rotation of the exhaust turbine 12 can drive the air inlet turbine 14 to synchronously rotate. The burned gas in the furnace body 7 is discharged through the first exhaust pipe 10, the exhaust chamber 11, and the second exhaust pipe 17, and the outside gas can be promoted to enter the furnace body 7 through the first intake pipe 15, the intake chamber 13, and the second intake pipe 16. The increase in the intake air amount can effectively promote combustion in the furnace body 7.
Further, the second exhaust pipe 17 and the exhaust pipe 1 are provided with a filter for purifying the fine dust of the gas in the second exhaust pipe 17 and the exhaust pipe 1.
The specific working method comprises the following steps:
a. the tail gas enters the furnace body 1 through the tail gas pipe 1 and is sprayed out from the gas outlet part 101 at the upper end of the tail gas pipe 1.
b. The gas enters the combustion plate 9 through the gas pipe 6, the gas distribution ring 6 and the gas hose 6 and is sprayed out and combusted through the combustion holes, and the combustion holes are inclined towards the same horizontal direction, so that the distributed flames formed by all the combustion holes can form spiral main flames. And the combustion of tail gas is more facilitated.
c. The temperature of the gas sprayed from the combustion holes is raised, so that the tail gas sprayed from the tail gas pipe 1 is subjected to oxidative decomposition reaction, and harmful substances in the tail gas are subjected to oxidative decomposition.
d. The burned exhaust gas is discharged via the first exhaust pipe 10, the exhaust chamber 11, and the second exhaust pipe 17.
e. When the exhaust gas is exhausted, the exhaust turbine 12 in the exhaust cavity 11 is driven to rotate, the air inlet turbine 14 and the exhaust turbine 12 rotate synchronously, the rotating air inlet turbine 14 promotes the outside air to enter the furnace body 7 through the first air inlet pipe 15, the air inlet cavity 13 and the second air inlet pipe 16, the air supply amount in the furnace body 7 is effectively increased, and the combustion efficiency is improved.
f. The first electric cylinder 3 drives the inner end of the combustion plate 9 to move in the axial direction of the tail gas pipe 1 through the first driving ring 21, the first connecting shaft 23 and the first slip ring 19.
g. The second electric cylinder 4 drives the outer end of the combustion plate 9 to move along the axial direction of the tail gas pipe 1 through a second driving ring 22, a second connecting shaft 24 and a second slip ring 20.
h. And (e) the combined movement of the step f and the step g can adjust the position and the opening and closing angle of the combustion plate 9 relative to the tail gas pipe 1, so that the position and the direction of gas flame on the combustion plate 9 can be adjusted, and different tail gas combustion effects can be realized.
In light of the foregoing description of the preferred embodiment of the present invention, many modifications and variations will be apparent to those skilled in the art without departing from the spirit and scope of the invention. The technical scope of the present invention is not limited to the content of the specification, and must be determined according to the scope of the claims.
Claims (3)
1. A tail gas treatment method is based on a tail gas incinerator, which comprises an incineration component and an air inlet component,
the incineration assembly comprises:
a tail gas pipe (1);
the first slip ring (19) is arranged on the tail gas pipe (1) in a sliding manner;
the second slip ring (20) is slidably arranged on the tail gas pipe (1);
the combustion plates (9) are circumferentially arrayed at the tail end of the tail gas pipe (1), the inner sides of the combustion plates (9) are hinged to the first sliding ring (19), the combustion plates (9) are of cavity structures, a plurality of combustion holes are formed in one side, facing the tail gas pipe (1), of each combustion plate (9), and the combustion holes are inclined towards the same horizontal direction;
the two ends of the connecting rod (18) are respectively hinged with the combustion plate (9) and the second sliding ring (20);
the gas pipe (5) is communicated with the combustion plate (9);
the fixed platform (2) is arranged on the tail gas pipe (1);
the first driving ring (21) is arranged on the tail gas pipe (1) in a sliding mode, and the first driving ring (21) is fixed with the first sliding ring (19) through a first connecting shaft (23);
the second driving ring (22) is arranged on the tail gas pipe (1) in a sliding mode, and the second driving ring (22) is fixed with the second sliding ring (20) through a second connecting shaft (24);
a first electric cylinder (3) provided between the fixed table (2) and the first drive ring (21);
a second electric cylinder (4) provided between the fixed table (2) and the second drive ring (22);
the air intake assembly includes:
a first intake pipe (15) communicating with the outside;
the second air inlet pipe (16) is communicated with the furnace body (7);
the air inlet cavity (13) is arranged between the first air inlet pipe (15) and the second air inlet pipe (16);
the air inlet turbine (14) is rotatably arranged in the air inlet cavity (13);
the first exhaust pipe (10) is communicated with the furnace body (7);
a second exhaust pipe (17) communicating with the outside;
an exhaust chamber (11) provided between the first exhaust pipe (10) and the second exhaust pipe (17);
the exhaust turbine (12) is rotatably arranged in the exhaust cavity (11), and the exhaust turbine (12) is in transmission connection with the air inlet turbine (14);
the lower end of the furnace body (7) is provided with a gas distribution ring (6), and the gas distribution ring (6) is communicated with the gas pipe (5); the upper end of the gas distribution ring (6) is provided with a gas hole corresponding to the combustion plate (9), and the gas hole is communicated with the combustion plate (9) through a gas hose (8);
the method is characterized by comprising the following steps:
a. tail gas enters the furnace body (7) through the tail gas pipe (1);
b. the fuel gas enters the combustion plate (9) through the fuel gas pipe (5), the gas distribution ring (6) and the fuel gas hose (8) and is sprayed out through the combustion holes for combustion;
c. the gas sprayed out of the combustion holes is combusted and heated, so that the tail gas sprayed out of the tail gas pipe (1) is subjected to oxidative decomposition reaction;
d. the combusted waste gas is exhausted through a first exhaust pipe (10), an exhaust cavity (11) and a second exhaust pipe (17);
e. the exhaust turbine (12) in the exhaust cavity (11) is driven to rotate while exhaust gas is exhausted, the air inlet turbine (14) and the exhaust turbine (12) rotate synchronously, the rotating air inlet turbine (14) promotes external air to enter the furnace body (7) through the first air inlet pipe (15), the air inlet cavity (13) and the second air inlet pipe (16), and the air supply amount in the furnace body (7) is effectively increased.
2. The exhaust gas treatment method according to claim 1, comprising the steps of:
f. the first electric cylinder (3) drives the inner end of the combustion plate (9) to move along the axial direction of the tail gas pipe (1) through a first driving ring (21), a first connecting shaft (23) and a first sliding ring (19);
g. the second electric cylinder (4) drives the outer end of the combustion plate (9) to move along the axial direction of the tail gas pipe (1) through a second driving ring (22), a second connecting shaft (24) and a second slip ring (20);
h. combining step f and step g, can adjusting the position and the angle that opens and shuts of burning board (9) for tail gas pipe (1) to adjust burning board (9) and go up the position and the direction of gas flame, thereby realize different tail gas combustion effects.
3. The exhaust gas treatment method according to claim 1, characterized in that:
and the second exhaust pipe (17) and the tail gas pipe (1) are provided with filters.
Priority Applications (1)
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CN202210827164.6A CN115143478B (en) | 2020-07-03 | 2020-07-03 | Tail gas treatment method |
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CN202210827164.6A CN115143478B (en) | 2020-07-03 | 2020-07-03 | Tail gas treatment method |
CN202010634844.7A CN111750368B (en) | 2020-07-03 | 2020-07-03 | Tail gas incinerator |
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CN202010634844.7A Division CN111750368B (en) | 2020-07-03 | 2020-07-03 | Tail gas incinerator |
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CN115143478A true CN115143478A (en) | 2022-10-04 |
CN115143478B CN115143478B (en) | 2024-04-19 |
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CN202010634844.7A Active CN111750368B (en) | 2020-07-03 | 2020-07-03 | Tail gas incinerator |
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CN112944327B (en) * | 2021-01-30 | 2022-07-05 | 淄博能源研究院 | Lotus petal type full-automatic biomass combustion furnace |
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JP5490956B1 (en) * | 2013-10-25 | 2014-05-14 | ▲たか▼男 上嶋 | Incinerator |
CN208871646U (en) * | 2018-09-25 | 2019-05-17 | 洛阳瑞昌环境工程有限公司 | A kind of sulfur recovery facility tail gas burning furnace |
CN110887051A (en) * | 2019-11-22 | 2020-03-17 | 深圳市群卜鸿科技有限公司 | A waste gas burns burning furnace that burning is abundant for environmental protection engineering |
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CN111750368B (en) | 2022-06-17 |
CN115143478B (en) | 2024-04-19 |
CN111750368A (en) | 2020-10-09 |
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