CN109945178B - Jet-flow type burner - Google Patents
Jet-flow type burner Download PDFInfo
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- CN109945178B CN109945178B CN201711384919.5A CN201711384919A CN109945178B CN 109945178 B CN109945178 B CN 109945178B CN 201711384919 A CN201711384919 A CN 201711384919A CN 109945178 B CN109945178 B CN 109945178B
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Abstract
The jet flow type burner of the invention basically comprises: the air blower is arranged at the rear section of the combustion chamber body of the combustion unit; the combustion unit is provided with a fuel barrel for storing fuel, a tubular combustion chamber body, at least one nozzle is arranged inside the combustion chamber body, at least one fuel pipe connected with the fuel barrel is arranged at each nozzle, at least one jet pipe is arranged at the front end of the combustion chamber body, the pipe diameter of each jet pipe is relatively smaller than the inner diameter of the combustion chamber body, the combustion detention time of the fuel inside the combustion chamber body can be prolonged under the action of the jet pipe, and the purpose of improving the combustion heat energy of the fuel is achieved.
Description
Technical Field
The invention relates to a burner, and mainly provides a jet flow type burner capable of effectively improving the combustion efficiency of fuel.
Background
The structure of the burner is basically as shown in fig. 1, and the burner is provided with a combustion chamber 12 connected with a fan 11, and a plurality of nozzles 13 connected with an oil supply device (not shown) are arranged in the combustion chamber 12, and the fan 11 mainly generates accelerated airflow in the combustion chamber 12, so that fuel oil injected into the combustion chamber 12 is ignited and then matched with the airflow in the combustion chamber 12, and flame can be ejected from the front end of the combustion chamber 12 for combustion.
The fuel used by the traditional burner mostly takes diesel oil with good ignition performance as the main part, at present, the heavy oil can be heated to 110 ℃ by a heater and then conveyed to an ignition position by a high-pressure pump matched with a pipeline, and the heavy oil is used as the fuel; the current combustion engine is mostly applied by directly connecting the applied thermal mechanical or heat exchange device with the front end of the combustion chamber 12, so the efficiency that can be improved by the combustion engine is completely dependent on the combustion efficiency of the fuel and the flame action range of the front end of the combustion chamber 12.
Although the air flow can be accelerated by using a fan like a conventional burner; however, in actual operation, the fuel injected into the combustion chamber may be blown out of the combustion chamber in an incompletely combusted state due to excessive acceleration of the air flow, so that the desired combustion efficiency of the combustor cannot be achieved.
Disclosure of Invention
The invention provides a jet flow type combustor which can effectively improve the combustion efficiency of fuel.
The invention relates to a jet flow type burner, which comprises: a combustion unit, a blower, a high pressure gas supply unit; wherein: the combustion unit is provided with a fuel barrel for storing fuel and a tubular combustion chamber body, wherein at least one nozzle is arranged in the combustion chamber body, at least one fuel pipe connected with the fuel barrel is arranged at each nozzle, at least one jet pipe is arranged at the front end of the combustion chamber body, and the pipe diameter of each jet pipe is relatively smaller than the inner diameter of the combustion chamber body; the blower is arranged at the rear end of the combustion chamber body in a state that the air outlet direction of the blower is parallel to the axis of the combustion chamber body.
Therefore, the jet flow type combustor can prolong the combustion residence time of fuel in the combustion chamber body under the action of the jet flow pipe, and achieves the purpose of improving the combustion efficiency of the fuel.
According to the technical characteristics, the jet flow type combustor further comprises a high-pressure gas supply unit; the high-pressure gas supply unit is provided with a gas storage barrel for storing high-pressure gas, and each nozzle is provided with a high-pressure pipe connected with the gas storage barrel.
According to the technical characteristics, the jet flow type combustor further comprises an air speed auxiliary unit; the wind speed auxiliary unit is provided with a wind speed cylinder at least covering the outside of the blower, the front end and the rear end of the wind speed cylinder are open, a gap for airflow to pass through is formed between the wind speed cylinder and the blower, and the rear end of the wind speed cylinder is provided with a blade and a motor for driving the blade to rotate.
According to the technical characteristics, the jet flow type burner further comprises a control unit; the control unit is provided with a control circuit, an igniter relatively positioned in the combustion chamber body and a fuel pump connected with a fuel pipe of each nozzle, wherein the control circuit is at least electrically connected with the igniter, the fuel pump and the blower.
According to the technical characteristics, the jet flow type burner further comprises the high-pressure gas supply unit and the wind speed auxiliary unit; the high-pressure gas supply unit is provided with a gas storage barrel for storing high-pressure gas, and each nozzle is provided with a high-pressure pipe connected with the gas storage barrel; the wind speed auxiliary unit is provided with the wind speed cylinder which is coated outside the blower, the front end and the rear end of the wind speed cylinder are open, a gap for airflow to pass through is formed between the wind speed cylinder and the blower, and the rear end of the wind speed cylinder is provided with the blade and the motor which drives the blade to rotate.
According to the technical characteristics, the jet flow type burner further comprises the high-pressure gas supply unit and the control unit; the high-pressure gas supply unit is provided with a gas storage barrel for storing high-pressure gas, and each nozzle is provided with a high-pressure pipe connected with the gas storage barrel; the control unit is provided with the control circuit, the igniter relatively positioned in the combustion chamber body, the fuel pump connected with the fuel pipe of each nozzle and a throttle valve connected with the high-pressure pipe of each nozzle, and the control circuit is at least electrically connected with the igniter, the fuel pump, the throttle valve and the blower.
According to the technical characteristics, the jet flow type burner further comprises the wind speed auxiliary unit and the control unit; the wind speed auxiliary unit is provided with a wind speed cylinder which is coated outside the blower, the front end and the rear end of the wind speed cylinder are open, a gap for airflow to pass through is formed between the wind speed cylinder and the blower, and the rear end of the wind speed cylinder is provided with the blade and the motor for driving the blade to rotate; the control unit is provided with the control circuit, the igniter relatively positioned in the combustion chamber body and the fuel pump connected with the fuel pipe of each nozzle, and the control circuit is at least electrically connected with the igniter, the fuel pump, the blower and the motor of the wind speed auxiliary unit.
According to the technical characteristics, the jet flow type burner further comprises the high-pressure gas supply unit, the wind speed auxiliary unit and the control unit; the high-pressure gas supply unit is provided with a gas storage barrel for storing high-pressure gas, and each nozzle is provided with a high-pressure pipe connected with the gas storage barrel; the wind speed auxiliary unit is provided with a wind speed cylinder which is coated outside the blower, the front end and the rear end of the wind speed cylinder are open, a gap for airflow to pass through is formed between the wind speed cylinder and the blower, and the rear end of the wind speed cylinder is provided with the blade and the motor for driving the blade to rotate; the control unit is provided with the control circuit, the igniter relatively positioned in the combustion chamber body, the fuel pump connected with the fuel pipe of each nozzle and the throttle valve connected with the high-pressure pipe of each nozzle, and the control circuit is at least electrically connected with the igniter, the fuel pump, the throttle valve, the blower and the motor of the wind speed auxiliary unit.
This wind speed auxiliary unit is equipped with this lubricating oil barrel that supplies to store lubricating oil, and position department is established to the pivot axle that has an at least this lubricating oil union coupling in this lubricating oil barrel and this motor in addition.
The wind speed auxiliary unit is provided with at least one cabin cover capable of being opened and closed at the cylinder wall of the wind speed cylinder.
The wind speed auxiliary unit is provided with a lubricating oil barrel for storing lubricating oil, at least one lubricating oil pipe is connected to the lubricating oil barrel and a rotating shaft of the motor, and at least one cabin cover capable of being opened and closed is arranged on the barrel wall of the wind speed barrel.
The high-pressure gas supply unit is further provided with an air compressor connected with the gas storage barrel, and the air compressor is electrically connected with the control circuit of the control unit.
The high-pressure gas supply unit is further provided with an air compressor connected with the gas storage barrel, and the air compressor is electrically connected with the control circuit of the control unit; and the wind speed auxiliary unit is provided with the lubricating oil barrel for storing lubricating oil, and at least one lubricating oil pipe is connected to the rotating shaft of the lubricating oil barrel and the motor at the position.
The high-pressure gas supply unit is further provided with an air compressor connected with the gas storage barrel, and the air compressor is electrically connected with the control circuit of the control unit; and the wind speed auxiliary unit is provided with at least one cabin cover which can be opened and closed at the cylinder wall of the wind speed cylinder.
The high-pressure gas supply unit is further provided with an air compressor connected with the gas storage barrel, and the air compressor is electrically connected with the control circuit of the control unit; the wind speed auxiliary unit is provided with a lubricating oil barrel for storing lubricating oil, at least one lubricating oil pipe is connected to the lubricating oil barrel and a rotating shaft of the motor, and at least one cabin cover capable of being opened and closed is arranged on the barrel wall of the wind speed barrel.
The jet flow type combustor disclosed by the invention mainly prolongs the combustion time of fuel in the combustion chamber body under the action of the jet flow pipe so as to achieve the purpose of improving the combustion efficiency of the fuel, can utilize the high-pressure gas supply unit to accelerate the fuel entering the nozzle, improves the atomization effect of the fuel after passing through the nozzle, and simultaneously provides the air flow entering the combustion chamber body so as to improve the combustion efficiency of the fuel; even more, under the effect of this wind speed auxiliary unit, can promote the velocity of flow and the flow of acceleration air current, promote the combustion efficiency and the efficiency of fuel with the more positive, reliable means relatively, avoid relevant unit to receive the high temperature influence, except can effectively reduce the pollution that diesel oil, heavy oil burning produced, more be favorable to taking alcohols as fuel, and can use in indoor environment such as restaurant, office, school.
Drawings
Fig. 1 is a schematic view of a conventional burner.
Fig. 2 is a schematic diagram of the basic structure of a jet flow combustor according to a first embodiment of the present invention.
Fig. 3 is an external perspective view of the front end view of the combustion chamber body according to the present invention.
Fig. 4 is a sectional view showing a structure of a combustion chamber body according to the present invention.
Fig. 5 is a sectional view showing the structure of a jet type burner according to a first embodiment of the present invention.
FIG. 6 is a schematic diagram of the operation of the jet combustor of the present invention.
Fig. 7 is an external perspective view of the combustion chamber body and the wind speed auxiliary unit according to the first embodiment of the present invention.
FIG. 8 is a schematic view of the operation of the wind speed assisting unit according to the present invention.
Fig. 9 is an external perspective view of a combustion chamber body and an air velocity assisting unit according to a second embodiment of the present invention.
Description of the figure numbers:
Prior Art
11 blower fan
12 combustion chamber
13 nozzle
The invention
20 burner unit
21 fuel tank
22 combustion chamber body
23 nozzle
24 Fuel pipe
25 high-pressure pipe
26 jet pipe
30 blower
40 wind speed auxiliary unit
41 wind speed cylinder
411 Hatch cover
42 blade
43 Motor
44 lubricating oil barrel
45 lubricating oil pipe
50 control unit
51 control circuit
52 igniter
53 fuel pump
54 throttle valve
60 high-pressure gas supply unit
61 gas storage barrel
62 air compressor.
Detailed Description
The present invention mainly provides a jet-type combustor capable of effectively improving fuel combustion efficiency, as shown in fig. 2 to 5, the jet-type combustor of the present invention basically comprises: a combustion unit 20 and a blower 30; wherein: the combustion unit 20 is provided with a fuel tank 21 for storing fuel, a tubular combustion chamber body 22, at least one nozzle 23 disposed inside the combustion chamber body 22, at least one fuel pipe 24 connected to the fuel tank 21 disposed at each nozzle 23, at least one jet pipe 26 disposed at the front end of the combustion chamber body 22, and the diameter of each jet pipe 26 being relatively smaller than the inner diameter of the combustion chamber body 22.
The blower 30 is connected to the combustion chamber main body 22, and the air flow can be supplied to the combustion chamber main body 22 after being pressurized by the blower 30. In one embodiment, the blower 30 is disposed at the rear end of the combustion chamber body 22 in a state that the air outlet direction thereof is substantially parallel to the axis of the combustion chamber body 22; alternatively, in another embodiment, the blower 30 is connected to the combustion chamber body 22 by a pipe (not shown) that connects the blower 30 and the combustion chamber body 22, so that the air flow can be pressurized by the blower 30 and then provided to the combustion chamber body 22. In practice, the blower 30 is preferably disposed on the axis of the combustion chamber main body 22.
In principle, the jet-flow type combustion engine of the present invention can extend the combustion residence time of the fuel in the combustion chamber body 22 (as shown in fig. 6) under the action of the jet pipes 26 during operation, so as to achieve the purpose of improving the combustion efficiency of the fuel.
Moreover, the jet flow type burner of the present invention, when implemented, may further include a high pressure gas supply unit 60; the high pressure gas supply unit 60 is provided with a gas storage barrel 61 for storing high pressure gas, and a high pressure pipe 25 connected with the gas storage barrel 61 is arranged at each nozzle 23; in practice, the high pressure air supply unit 60 may further include an air compressor 62 connected to the air tank 61, and the air compressor 62 may be operated to continuously supply high pressure air.
Referring to fig. 5, fig. 7 and fig. 8, the jet burner of the present invention may further include an auxiliary wind speed unit 40; the wind speed auxiliary unit 40 is provided with a wind speed cylinder 41 at least covering the outside of the blower 30, the front and rear ends of the wind speed cylinder 41 are open, a gap for air flow to pass through is formed between the wind speed cylinder 41 and the blower 30, a blade 42 and a motor 43 for driving the blade 42 to rotate are arranged at the rear end of the wind speed cylinder 41, and a ventilation net with a net structure is arranged at the rear end of the wind speed cylinder 41.
Accordingly, the flow rate of the intake air of the blower 30 can be increased by the operation of the blades 42 of the wind speed auxiliary unit 40 (as shown in fig. 7), so that not only the flow rate and flow rate of the accelerated airflow can be effectively increased, but also a part of the airflow can be accelerated through the gap between the wind speed cylinder 41 and the blower 30, and the waste heat discharge rate of the blower 30 and the motor 43 can be increased, thereby avoiding the influence of high temperature on the relevant units by relatively more positive and reliable means.
It should be noted that, because the jet burner of the present invention can increase and accelerate the flow velocity and flow rate of the air flow under the action of the auxiliary wind speed unit 40, the size of the fan can be reduced, and even through the design of the blower 30 on-line with the axis of the combustion chamber body 22, the shapes of the combustion chamber body 22, the blower 30 and the auxiliary wind speed unit 40 can be integrated, which is more conducive to the development of the burner toward miniaturization and compactness.
The jet flow type burner of the present invention, when implemented, may further comprise a control unit 50; the control unit 50 is provided with a control circuit 51, an igniter 52 located inside the combustion chamber body 22, and a fuel pump 53 connected to the fuel pipe 24 of each nozzle 23, wherein the control circuit 51 is electrically connected to at least the igniter 52, the fuel pump 53, and the blower 30.
Accordingly, the control circuit 51 of the control unit 50 can be loaded or set with related work items and parameters, and the control circuit 51 controls the operation of the igniter 52, the fuel pump 53 and the blower 30 according to the selected or set work items and parameters, thereby achieving the purpose of automatic operation.
When the jet flow type burner of the present invention is implemented, the jet flow type burner further includes the high pressure gas supply unit 60 and the wind speed auxiliary unit 40; the high pressure gas supply unit 60 is provided with the gas storage barrel 61 for storing high pressure gas, and the high pressure pipe 25 connected with the gas storage barrel 61 is arranged at each nozzle 23; the wind speed auxiliary unit 40 is provided with the wind speed cylinder 41 covering the outside of the blower 30, the front and rear ends of the wind speed cylinder 41 are open, a gap through which an air current can pass is formed between the wind speed cylinder 41 and the blower 30, and the rear end of the wind speed cylinder 41 is provided with the blade 42 and the motor 43 for driving the blade 42 to rotate.
When the jet flow type burner of the present invention is implemented, the jet flow type burner further includes the high pressure gas supply unit 60 and the control unit 50; the high pressure gas supply unit 60 is provided with the gas storage barrel 61 for storing high pressure gas, and the high pressure pipe 25 connected with the gas storage barrel 61 is arranged at each nozzle 23; the control unit 50 is provided with the control circuit 51, the igniter 52 located in the combustion chamber main body 22, the fuel pump 53 connected to the fuel pipe 24 of each nozzle 23, and a throttle valve 54 connected to the high-pressure pipe 25 of each nozzle 23, and the control circuit 51 is electrically connected to at least the igniter 52, the fuel pump 53, the throttle valve 54, and the blower 30.
When the jet flow type burner of the present invention is implemented, the jet flow type burner further comprises the wind speed auxiliary unit 40 and the control unit 50; the wind speed auxiliary unit 40 is provided with the wind speed cylinder 41 covering the outside of the blower 30, the front and rear ends of the wind speed cylinder 41 are open, a gap through which air can pass is formed between the wind speed cylinder 41 and the blower 30, and the rear end of the wind speed cylinder 41 is provided with the blade 42 and the motor 43 driving the blade 42 to rotate; the control unit 50 is provided with the control circuit 51, the igniter 52 located in the combustion chamber main body 22, and the fuel pump 53 connected to the fuel pipe 24 of each nozzle 23, and the control circuit 51 is electrically connected to at least the igniter 52, the fuel pump 53, the blower 30, and the motor 43 of the wind speed auxiliary unit 40.
Of course, the jet flow type combustion engine of the present invention, when implemented, may further include the high pressure gas supply unit 60, the wind speed auxiliary unit 40 and the control unit 50; the high pressure gas supply unit 60 is provided with the gas storage barrel 61 for storing high pressure gas, and the high pressure pipe 25 connected with the gas storage barrel 61 is arranged at each nozzle 23; the wind speed auxiliary unit 40 is provided with the wind speed cylinder 41 covering the outside of the blower 30, the front and rear ends of the wind speed cylinder 41 are open, a gap through which air can pass is formed between the wind speed cylinder 41 and the blower 30, and the rear end of the wind speed cylinder 41 is provided with the blade 42 and the motor 43 driving the blade 42 to rotate; the control unit 50 is provided with the control circuit 51, the igniter 52 located in the combustion chamber main body 22, the fuel pump 53 connected to the fuel pipe 24 of each nozzle 23, and the throttle valve 54 connected to the high-pressure pipe 25 of each nozzle 23, and the control circuit 51 is electrically connected to at least the igniter 52, the fuel pump 53, the throttle valve 54, the blower 30, and the motor 43 of the wind speed auxiliary unit 40.
In various possible embodiments of the present invention, the wind speed auxiliary unit 40 may further include a lubricant barrel 44 (as shown in fig. 5) for storing lubricant, and at least one lubricant pipe 45 is connected to the lubricant barrel and the shaft position (bearing) of the motor 43, so that lubricant can be supplied to the shaft position of the motor 43 through the normal state of the lubricant barrel 44 and the lubricant pipe 45, thereby ensuring smooth operation of the motor 43 and improving the operation efficiency of the whole jet burner.
Referring to fig. 9, in the wind speed auxiliary unit 40, at least one hatch 411 capable of being opened and closed is disposed on the wall of the wind speed cylinder 41, and the design of the hatch 411 can be utilized to achieve the purpose of facilitating the installation and maintenance of the related units.
Of course, as shown in fig. 5 and 9, the wind speed auxiliary unit 40 is preferably further provided with the lubricating oil barrel 44 for storing lubricating oil, at least one lubricating oil pipe 45 is connected to the lubricating oil barrel and the rotating shaft axial position (bearing) of the motor 43, and at least one hatch 411 capable of being opened and closed is arranged on the wall of the wind speed barrel 41.
In the embodiment of the present invention further including the control unit 50, the high pressure air supply unit 60, and the air compressor 62 connected to the gas tank 61, the air compressor 62 is electrically connected to the control circuit 51 of the control unit 50, and the high pressure air can be continuously supplied by the operation of the air compressor 62.
In the embodiment of the present invention further including the control unit 50, the high pressure gas supply unit 60, and further having the air compressor 62 connected to the gas storage barrel 61, wherein the air compressor 62 is electrically connected to the control circuit 51 of the control unit 50, the wind speed auxiliary unit 40 may further have the lubricating oil barrel 44 for storing lubricating oil, and at least one lubricating oil pipe 45 is connected to the rotating shaft of the lubricating oil barrel 44 and the motor 43 at a position (bearing).
In the embodiment of the present invention, the control unit 50, the high pressure gas supply unit 60, and the air compressor 62 connected to the gas storage barrel 61 are further provided, and the air compressor 62 is electrically connected to the control circuit 51 of the control unit 50, and the wind speed auxiliary unit 40 can also be provided with at least one hatch 411 for opening and closing at the wall of the wind speed cylinder 41.
Of course, in the embodiment of the present invention further including the control unit 50, the high pressure gas supply unit 60, and further having the air compressor 62 connected to the gas storage barrel 61, wherein the air compressor 62 is electrically connected to the control circuit 51 of the control unit 50, the wind speed auxiliary unit 40 further has the lubricating oil barrel 44 for storing lubricating oil, at least one lubricating oil pipe 45 is connected to the rotating shaft of the lubricating oil barrel 44 and the motor 43 at the position (bearing), and the cabin cover 411 is provided at the wall of the wind speed barrel 41 for opening and closing.
Compared with the traditional conventional technology, the jet flow type combustor disclosed by the invention has the advantages that the combustion residence time of fuel in the combustion chamber body is prolonged under the action of the jet flow pipe, so that the purpose of improving the combustion efficiency of the fuel is achieved, and the high-pressure gas supply unit can be utilized to generate micro-atomization acceleration effect on the fuel entering the nozzle, so that fuel molecules are more refined, the combustion is more complete, and the purpose of improving the combustion efficiency of the fuel is achieved; further under the effect of this forced draught blower, increase the inflow of air of this combustion chamber body for burning more completely reaches fuel combustion efficiency and promotes, even, can promote the velocity of flow and the flow of accelerating the air current under the effect of this wind speed auxiliary unit, promote combustion efficiency and the efficiency of fuel with the relatively more positive, reliable means, avoid relevant unit to receive the high temperature influence, except can effectively reducing the pollution that diesel oil, heavy oil burning produced, more favorable as fuel with alcohols, and can use in indoor environment such as restaurant, office, school.
Claims (7)
1. A jet combustor, comprising: a combustion unit (20) and a blower (30); the method is characterized in that:
the combustion unit (20) is provided with a fuel barrel (21) for storing fuel and a tubular combustion chamber body (22), at least one nozzle (23) is arranged in the combustion chamber body (22), at least one fuel pipe (24) connected with the fuel barrel (21) is arranged at each nozzle (23), at least one jet pipe (26) is arranged at the front end of the combustion chamber body (22), and the pipe diameter of each jet pipe (26) is relatively smaller than the inner diameter of the combustion chamber body (22); the blower (30) is connected with the combustion chamber body (22);
the blower (30) is arranged at the rear end of the combustion chamber body (22) in a state that the air outlet direction of the blower is parallel to the axis of the combustion chamber body (22), the blower (30) is arranged on the axis of the combustion chamber body (22) on line, and airflow can be provided to the combustion chamber body (22) after being pressurized by the blower (30); the jet flow type burner comprises an air speed auxiliary unit (40); the wind speed auxiliary unit (40) is provided with a wind speed cylinder (41) at least covering the outside of the blower (30), the front end and the rear end of the wind speed cylinder (41) are open, a gap for airflow to pass is formed between the wind speed cylinder (41) and the blower (30), the rear end of the wind speed cylinder (41) is provided with a blade (42) and a motor (43) for driving the blade (42) to rotate, the wind speed auxiliary unit (40) is provided with at least one cabin cover (411) for opening and closing at the cylinder wall of the wind speed cylinder (41); and a ventilation net having a net structure, the ventilation net being disposed at a rear end of the wind speed cylinder (41).
2. A jet combustor as claimed in claim 1, wherein the jet combustor includes a high pressure gas supply assembly (60); the high-pressure gas supply unit (60) is provided with a gas storage barrel (61) for storing high-pressure gas, and a high-pressure pipe (25) connected with the gas storage barrel (61) is arranged at each nozzle (23).
3. A jet combustor as claimed in claim 1, wherein the jet combustor includes a control unit (50); the control unit (50) is provided with a control circuit (51), an igniter (52) which is relatively positioned in the combustion chamber body (22), and a fuel pump (53) which is connected with the fuel pipe (24) of each nozzle (23), wherein the control circuit (51) is at least electrically connected with the igniter (52), the fuel pump (53) and the blower (30).
4. The jet combustor of claim 1, comprising a high pressure gas supply unit (60) and a control unit (50); the high-pressure gas supply unit (60) is provided with a gas storage barrel (61) for storing high-pressure gas, and a high-pressure pipe (25) connected with the gas storage barrel (61) is arranged at each nozzle (23); the control unit (50) is provided with a control circuit (51), an igniter (52) which is relatively positioned in the combustion chamber body (22), a fuel pump (53) which is connected with the fuel pipe (24) of each nozzle (23), and a throttle valve (54) which is connected with the high-pressure pipe (25) of each nozzle (23), wherein the control circuit (51) is at least electrically connected with the igniter (52), the fuel pump (53), the throttle valve (54) and the blower (30).
5. A jet burner as in claim 1 or 2 or 3 or 4 wherein the air velocity assist unit (40) has a lubricant tank (44) for storing lubricant, and at least one lubricant pipe (45) is connected to the lubricant tank (44) and the motor (43) at the axial location of the rotational axis.
6. The jet burner of claim 4, wherein the high pressure gas supply unit (60) is provided with an air compressor (62) connected to the gas receiver (61), the air compressor (62) being electrically connected to the control circuit (51) of the control unit (50).
7. The jet combustor of claim 4, wherein the high pressure gas supply unit (60) is provided with an air compressor (62) connected to the gas receiver (61), the air compressor (62) being electrically connected to the control circuit (51) of the control unit (50); and the wind speed auxiliary unit (40) is provided with a lubricating oil barrel (44) for storing lubricating oil, and at least one lubricating oil pipe (45) is connected to the rotating shaft of the lubricating oil barrel (44) and the motor (43) at a position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711384919.5A CN109945178B (en) | 2017-12-20 | 2017-12-20 | Jet-flow type burner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711384919.5A CN109945178B (en) | 2017-12-20 | 2017-12-20 | Jet-flow type burner |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109945178A CN109945178A (en) | 2019-06-28 |
| CN109945178B true CN109945178B (en) | 2021-04-02 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711384919.5A Active CN109945178B (en) | 2017-12-20 | 2017-12-20 | Jet-flow type burner |
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| CN (1) | CN109945178B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101033752A (en) * | 2007-04-04 | 2007-09-12 | 陈泽民 | Couple-stage axial-flow fans |
| CN201827100U (en) * | 2010-09-20 | 2011-05-11 | 陈文满 | Axial flow fan |
| CN103953926A (en) * | 2014-05-15 | 2014-07-30 | 中国轻工业陶瓷研究所 | Ceramic kiln combustion system taking biological alcohol oil as fuel and combustion control method of ceramic kiln combustion system |
| CN104197327A (en) * | 2014-09-02 | 2014-12-10 | 李良君 | Alcohol group combustor |
| CN105386989A (en) * | 2015-12-01 | 2016-03-09 | 江苏兆胜空调有限公司 | High-temperature-resistant axial flow ventilator for ship |
| CN206386927U (en) * | 2017-01-04 | 2017-08-08 | 河北金景达新能源科技股份有限公司 | A kind of alcohol-based fuel burner of energy-conserving and environment-protective |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4161926B2 (en) * | 2004-03-31 | 2008-10-08 | Ｊｆｅスチール株式会社 | Tubular flame burner |
| CN2723841Y (en) * | 2004-08-12 | 2005-09-07 | 周惠欣 | Small rotary cup type burner |
| CN207661765U (en) * | 2017-12-20 | 2018-07-27 | 洁醇事业股份有限公司 | Jet flow combustor |
-
2017
- 2017-12-20 CN CN201711384919.5A patent/CN109945178B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101033752A (en) * | 2007-04-04 | 2007-09-12 | 陈泽民 | Couple-stage axial-flow fans |
| CN201827100U (en) * | 2010-09-20 | 2011-05-11 | 陈文满 | Axial flow fan |
| CN103953926A (en) * | 2014-05-15 | 2014-07-30 | 中国轻工业陶瓷研究所 | Ceramic kiln combustion system taking biological alcohol oil as fuel and combustion control method of ceramic kiln combustion system |
| CN104197327A (en) * | 2014-09-02 | 2014-12-10 | 李良君 | Alcohol group combustor |
| CN105386989A (en) * | 2015-12-01 | 2016-03-09 | 江苏兆胜空调有限公司 | High-temperature-resistant axial flow ventilator for ship |
| CN206386927U (en) * | 2017-01-04 | 2017-08-08 | 河北金景达新能源科技股份有限公司 | A kind of alcohol-based fuel burner of energy-conserving and environment-protective |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109945178A (en) | 2019-06-28 |
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