CN109945179B - Turbo-charged combustor - Google Patents
Turbo-charged combustor Download PDFInfo
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- CN109945179B CN109945179B CN201711386011.8A CN201711386011A CN109945179B CN 109945179 B CN109945179 B CN 109945179B CN 201711386011 A CN201711386011 A CN 201711386011A CN 109945179 B CN109945179 B CN 109945179B
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Abstract
The turbo-charged combustor of the present invention at least includes: a combustion unit and a turbocharger; the combustion unit is provided with a fuel barrel for storing fuel and a tubular combustion chamber body, at least one nozzle is arranged in the combustion chamber body, and at least one fuel pipe connected with the fuel barrel is arranged at each nozzle; and the turbocharger is connected with the combustion chamber body. According to under the effect of turbo charger, increase the air intake flow of combustion chamber body, promote the velocity of flow and the flow of accelerating gas flow for the burning more completely reaches the purpose that fuel combustion efficiency promotes.
Description
Technical Field
The invention relates to a combustor, and mainly provides a turbo-charged combustor capable of effectively improving combustion efficiency.
Background
The structure of a burner (or a 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 sprayed and combusted from the front end of the combustion chamber 12.
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 present combustion engine is mostly applied by directly connecting the applied thermal mechanical or heat exchange equipment with the front end of the combustion chamber 12, so the combustion efficiency of the fuel used by the combustion engine is completely determined by whether the air supply of the combustion chamber 12 is enough or not.
Although the air flow can be accelerated by using a fan like a conventional burner; however, in order to obtain sufficient air supply amount, the accelerated airflow generated by the fan 11 is completely introduced into the combustion chamber 12, and the size ratio of the fan 11 and the combustion chamber 12 is very different, so that the fan 11 and the combustion chamber 12 must be usually configured in parallel, which not only makes the related unit equipment susceptible to malfunction and damage caused by high operating temperature, but also severely limits the development of the combustor towards miniaturization and compactness under the condition that the shapes of the fan 11 and the combustion chamber 12 cannot be effectively integrated.
Disclosure of Invention
The invention provides a turbo-charged combustor capable of effectively improving combustion efficiency.
The turbo-charged combustor of the present invention at least includes: a combustion unit and a turbocharger; the combustion unit is provided with a fuel barrel for storing fuel and a tubular combustion chamber body, at least one nozzle is arranged in the combustion chamber body, and at least one fuel pipe connected with the fuel barrel is arranged at each nozzle; and the turbocharger is connected with the combustion chamber body.
According to the above technical feature, wherein the turbocharger is provided at the rear end of the combustion chamber body in a state where the air outlet direction thereof is parallel to the axis of the combustion chamber body; the wind speed auxiliary unit is provided with a wind speed cylinder at least covering the outside of the turbocharger, the front end and the rear end of the wind speed cylinder are open, a gap for air flow to pass through is formed between the wind speed cylinder and the turbocharger, and the rear end of the wind speed cylinder is provided with a blade and a motor driving the blade to rotate.
Therefore, under the action of the wind speed auxiliary unit, partial airflow can be accelerated to pass through the gap between the wind speed cylinder and the turbocharger, the waste heat discharge rate of the turbocharger and the motor is improved, and the relevant unit is prevented from being influenced by high temperature by a relatively more positive and reliable means.
According to the technical characteristics, the turbo-charged combustor 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 the fuel pipe of each nozzle, and the control circuit is at least electrically connected with the igniter, the fuel pump, the turbocharger and the motor of the wind speed auxiliary unit.
According to the technical characteristics, the turbo-charged combustor further comprises a 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 a high-pressure pipe connected with the gas storage barrel is arranged at each nozzle; 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, the turbocharger and the motor of the wind speed auxiliary unit.
According to the technical characteristics, the front end of the combustion chamber body of the combustion unit is provided with at least one jet pipe, and the pipe diameter of each jet pipe is relatively smaller than the inner diameter of the combustion chamber body.
According to the technical characteristics, the turbo-charged combustor further comprises the control unit; 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 turbocharger and the motor of the wind speed auxiliary unit; and the front end of the combustion chamber body of the combustion unit is provided with at least one jet pipe, and the pipe diameter of each jet pipe is relatively smaller than the inner diameter of the combustion chamber body.
According to the technical characteristics, the turbo-charged combustor 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 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 turbocharger and the motor of the wind speed auxiliary unit; and the front end of the combustion chamber body of the combustion unit is provided with at least one jet pipe, and the pipe diameter of each jet pipe is relatively smaller than the inner diameter of the combustion chamber body.
This wind speed auxiliary unit is equipped with a lubricating oil barrel that supplies to store lubricating oil, and position department is established to the pivot axle that has an at least 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 turbocharging type combustor disclosed by the invention is mainly used for increasing the air inlet flow of the combustion chamber body and improving the flow speed and flow of accelerated air flow under the action of the turbocharger, so that the combustion can be more completely improved to the fuel combustion efficiency; the turbocharging type combustor disclosed by the invention is mainly used for increasing the air inlet flow of the combustion chamber body and improving the flow speed and flow of accelerated air flow under the action of the turbocharger, so that the combustion can be more completely improved to the fuel combustion efficiency; even more, the design of the high-pressure gas supply unit and the jet pipe can be utilized to improve the combustion efficiency and heat energy of the fuel by a relatively more positive and reliable means, thereby not only effectively reducing the pollutants generated by the combustion of diesel oil and heavy oil, but also being more beneficial to taking alcohol as the fuel and being used in indoor environments such as restaurants, institutions, schools and the like.
Drawings
Fig. 1 is a schematic view of a conventional burner.
Fig. 2 is a schematic diagram of the basic component architecture of the turbocharged combustor according to the first embodiment of the present invention.
Fig. 3 is an external perspective view of the combustion chamber body and the wind speed auxiliary unit according to the present invention.
FIG. 4 is an exploded view of the wind speed auxiliary assembly according to the present invention.
Fig. 5 is a sectional view of the structure of the turbocharged combustor in the first embodiment of the present invention.
Fig. 6 is a schematic view of the operation of the turbocharged combustor according to the first embodiment of the present invention.
Fig. 7 is a sectional view of a structure of a turbocharged combustor in accordance with a second embodiment of the present invention.
Fig. 8 is an external perspective view of a combustion chamber body and an air velocity assisting unit according to a third 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 turbo charger
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 turbo-charged combustion engine capable of effectively increasing accelerated airflow and effectively avoiding the influence of high temperature on related units, as shown in fig. 2 to 5, the turbo-charged combustion engine of the present invention basically comprises at least: a combustion unit 20 and a turbocharger 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, and at least one fuel pipe 24 connected to the fuel tank 21 disposed at each nozzle 23. Preferably, a plurality of nozzles 23 are disposed inside the combustion chamber body 22.
The turbocharger 30 is coupled to the combustion chamber body 22 such that airflow is pressurized from the turbocharger 30 and provided to the combustion chamber body 22. In one embodiment, the turbocharger 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 turbocharger 30 is connected to the combustor body 22 by a conduit (not shown) that connects the turbocharger 30 to the combustor body 22 to allow for the pressurized flow of air from the turbocharger 30 to the combustor body 22. In practice, the turbocharger 30 is preferably disposed on the axis of the combustion chamber body 22.
Accordingly, the turbocharger 30 of the present invention can increase the intake air flow of the combustion chamber body 22, accelerate the flow rate of the air flow and increase the flow rate of the air flow, so as to achieve more complete combustion and achieve the effect of improving the combustion efficiency of the fuel.
The turbo-charged combustion engine further comprises an air speed auxiliary unit 40, the air speed auxiliary unit 40 is provided with an air speed cylinder 41 at least covering the outside of the turbo-charged 30, the front end and the rear end of the air speed cylinder 41 are open, a gap for air flow to pass through is formed between the air speed cylinder 41 and the turbo-charged 30, the rear end of the air speed cylinder 41 is provided with a blade 42 and a motor 43 for driving the blade 42 to rotate, and a ventilation net with a net-shaped structure is arranged at the rear end of the air speed cylinder 41.
In principle, the turbocharger combustion engine of the present invention can generate an accelerated airflow in the combustion chamber body 22 under the action of the turbocharger 30 during operation, so that after the fuel injected into the combustion chamber body 22 is ignited, as shown in fig. 6, the flame is ejected from the front end of the combustion chamber body 22 to be combusted in cooperation with the accelerated airflow in the combustion chamber body 22.
In particular, the flow rate of the intake air of the turbocharger 30 can be increased by the operation of the blades 42 of the wind speed auxiliary unit 40, which not only can effectively increase the flow speed and flow rate of the accelerated airflow, but also can accelerate part of the airflow through the gap between the wind speed cylinder 41 and the turbocharger 30, thereby increasing the waste heat discharge rate of the turbocharger 30 and the motor 43, and avoiding the relevant units from being affected by high temperature by relatively more positive and reliable means.
It should be noted that, because the turbo-charged combustion engine of the present invention can increase the flow velocity and flow rate of the accelerated airflow under the action of the wind speed auxiliary unit 40, the size of the fan can be reduced, and even through the design of the turbo-charger 30 disposed on the axial line of the combustion chamber body 22, the shapes of the combustion chamber body 22, the turbo-charger 30 and the wind speed auxiliary unit 40 can be integrated, which is more conducive to the development of the combustor towards miniaturization and compactness.
Moreover, the turbocharged combustion engine of the present invention may further include 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, the turbocharger 30, and the motor 43 of the wind speed auxiliary unit 40.
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, the turbocharger 30 and the motor 43 of the wind speed assisting unit 40 according to the selected or set work items and parameters, thereby achieving the purpose of automatic operation.
Referring to fig. 7, the turbocharged combustion engine of the present invention may further include a high pressure gas supply unit 60 and the control unit 50; the high pressure gas supply unit 60 is provided with a gas storage tank 61 for storing high pressure gas, and a high pressure pipe 25 connected to the gas storage tank 61 is provided at each nozzle 23. As for the control unit 50, the control circuit 51, the igniter 52 relatively located inside the combustion chamber 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 are provided, and the control circuit 51 is electrically connected to at least the igniter 52, the fuel pump 53, the throttle valve 54, the turbocharger 30, and the motor 43 of the wind speed assisting unit 40.
In this embodiment, the high-pressure gas provided by the high-pressure gas supply unit 60 can further accelerate the fuel entering the nozzle 23, so as to improve the atomization effect of the fuel after passing through the nozzle 23, and provide the air flow entering the combustion chamber main body 22, thereby achieving the purpose of improving the fuel combustion efficiency.
In the embodiment shown in fig. 7, the burner unit 20 further has at least one jet pipe 26 disposed at the front end of the combustion chamber body 22, and preferably a plurality of jet pipes 26 are disposed 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, so as to prolong the combustion time of the fuel in the combustion chamber body 22 and increase the flame spraying distance after the fuel is combusted under the action of the jet pipes 26, thereby achieving the purpose of increasing the combustion heat energy of the fuel.
The turbocharged combustion engine of the present invention, when implemented, can further include the control unit 50, the control unit 50 is provided with the control circuit 51, the igniter 52 located inside the combustion chamber body 22 relatively, and the fuel pump 53 connected to the fuel pipe 24 of each nozzle 23, the control circuit 51 is electrically connected to at least the igniter 52, the fuel pump 53, the turbocharger 30, and the motor 43 of the wind speed auxiliary unit 40, and the combustion unit 20 is provided with at least one jet pipe 26 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.
Of course, the turbocharged combustion engine of the present invention 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 tank 61 for storing high pressure gas, the high pressure pipe 25 connected to the gas tank 61 is provided at each nozzle 23, the control unit 50 is provided with the control circuit 51, the igniter 52 located inside the combustion chamber body 22 relatively, the fuel pump 53 connected to the fuel pipe 24 of each nozzle 23, the throttle valve 54 connected to the high pressure pipe 25 of each nozzle 23, the control circuit 51 is electrically connected to at least the igniter 52, the fuel pump 53, the throttle valve 54, the turbocharger 30 and the motor 43 of the wind speed auxiliary unit 40, and the combustion unit 20 is provided with at least one jet pipe 26 at the front end of the combustion chamber body 22, the diameter of each jet pipe 26 is preferably smaller than the inner diameter of the combustion chamber body 22.
In the present invention, in various possible implementation manners, the wind speed auxiliary unit 40 may further include a lubricant barrel 44 for storing lubricant, and at least one lubricant pipe 45 is connected to the lubricant barrel 44 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 entire turbo-charged combustion engine.
Referring to fig. 8, in the wind speed auxiliary unit 40, in various possible implementation modes, 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, 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 connected to the lubricating oil barrel and the rotating shaft of the motor 43 at the axial position (bearing), and the cabin cover 411 at least for opening and closing is provided at the barrel wall of the wind speed barrel 41.
And, in the embodiment of the present invention further comprising the control unit 50, the high pressure air supply unit 60 may further comprise an air compressor 62 connected to the air tank 61, wherein the air compressor 62 is electrically connected to the control circuit 51 of the control unit 50, and can continuously provide high pressure air under 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 tank 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 tank 44 for storing lubricating oil, and at least one lubricating oil pipe 45 is connected to the rotating shaft of the lubricating oil tank 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 position (bearing) where the lubricating oil barrel is axially arranged with the rotating shaft of the motor 43, and at least one cabin cover 411 capable of being opened and closed is arranged at the wall of the wind speed barrel 41.
Compared with the traditional conventional technology, the turbocharging type combustor disclosed by the invention has the advantages that the air inlet flow of the combustion chamber body is increased mainly under the action of the turbocharger, so that the combustion can be more completely improved in fuel combustion efficiency, and part of air flow can be accelerated to pass through the gap between the air speed cylinder and the turbocharger under the action of the air speed auxiliary unit, so that the flow speed and flow of the accelerated air flow are improved, and the relevant units are prevented from being influenced by high temperature; even more, the design of the high-pressure gas supply unit and the jet pipe can be utilized to improve the combustion efficiency and heat energy of the fuel by a relatively more positive and reliable means, thereby not only effectively reducing the pollutants generated by the combustion of diesel oil and heavy oil, but also being more beneficial to taking alcohol as the fuel and being used in indoor environments such as restaurants, offices, schools and the like.
Claims (14)
1. A turbocharged combustion engine, comprising at least: a combustion unit (20) and a turbocharger (30); 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), and at least one fuel pipe (24) connected with the fuel barrel (21) is arranged at each nozzle (23); the turbocharger (30) is arranged at the rear end of the combustion chamber body (22) in a state that the air outlet direction of the turbocharger (30) is parallel to the axis of the combustion chamber body (22), the turbocharger (30) is arranged on the axis of the combustion chamber body (22), and airflow can be provided to the combustion chamber body (22) after being pressurized by the turbocharger (30); the turbo-charged combustion engine comprises an air speed auxiliary unit (40), wherein the air speed auxiliary unit (40) is provided with an air speed cylinder (41) at least covering the outside of the turbo-charged combustion engine (30), the front end and the rear end of the air speed cylinder (41) are open, a gap for air flow to pass through is formed between the air speed cylinder (41) and the turbo-charged combustion engine (30), and the rear end of the air speed cylinder (41) is provided with a blade (42) and a motor (43) for driving the blade (42) to rotate; 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 turbocharged combustor according to claim 1, comprising 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), the turbocharger (30) and the motor (43) of the wind speed auxiliary unit (40).
3. The turbocharged 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 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 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), the turbocharger (30) and the motor of the wind speed auxiliary unit (40).
4. The turbocharged combustor of claim 1, wherein the combustor assembly (20) is provided with at least one injection pipe (26) at the front end of the combustor body (22), and the pipe diameter of each injection pipe (26) is relatively smaller than the inner diameter of the combustor body (22).
5. A turbocharged combustor according to claim 1, comprising 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), the turbocharger (30) and the motor (43) of the wind speed auxiliary unit (40); and the combustion unit (20) is provided with at least one jet pipe (26) 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).
6. The turbocharged 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 a fuel pipe (24) of each nozzle (23), and a throttle valve (54) which is connected with a high-pressure pipe 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), the turbocharger (30) and a motor (43) of the wind speed auxiliary unit (40); and the combustion unit (20) is provided with at least one jet pipe (26) 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).
7. The turbocharged combustor of any one of claims 1 to 6, wherein the wind speed assist unit (40) is provided with a lubricant tank (44) for storing lubricant, and further comprising at least one lubricant pipe (45) connected to the lubricant tank (44) and the shaft of the motor (43).
8. The turbocharged combustor as claimed in any one of claims 1 to 6, wherein the wind speed auxiliary unit (40) has at least one opening/closing hatch (411) at the wall of the wind speed cylinder (41).
9. The turbo-charged combustor according to any one of claims 1 to 6, wherein the wind speed auxiliary unit (40) has a lubricant tank (44) for storing lubricant, at least one lubricant pipe (45) is connected to the lubricant tank (44) and the rotational axis of the motor, and at least one hatch (411) for opening and closing is disposed on the wall of the wind speed cylinder (41).
10. A turbocharged combustion engine according to claim 3 or 6, wherein the high pressure gas supply unit (60) is provided with an air compressor connected to the gas storage tank, which air compressor is electrically connected to the control circuit (51) of the control unit (50).
11. The turbocharged combustor of claim 3 or 6, wherein the high pressure gas supply unit (60) is provided with an air compressor 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 for storing lubricating oil, and at least one lubricating oil pipe (45) is connected to the rotating shaft of the lubricating oil barrel and the motor.
12. The turbocharged combustor of claim 3 or 6, wherein the high pressure gas supply unit (60) is provided with an air compressor (62) connected to the gas receiver (61), the air compressor being electrically connected to the control circuit (51) of the control unit (50); and the wind speed auxiliary unit (40) is provided with at least one hatch cover (411) for opening and closing at the cylinder wall of the wind speed cylinder (41).
13. The turbocharged combustor of claim 3 or 6, 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); the wind speed auxiliary unit (40) is provided with a lubricating oil barrel (44) for storing lubricating oil, at least one lubricating oil pipe (45) is connected to the positions of the lubricating oil barrel (44) and the rotating shaft of the motor (43), and at least one cabin cover (411) for opening and closing is arranged on the barrel wall of the wind speed barrel (41).
14. The turbocharged combustor of claim 1, wherein the turbocharger (30) is piped to the combustor body (22).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711386011.8A CN109945179B (en) | 2017-12-20 | 2017-12-20 | Turbo-charged combustor |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711386011.8A CN109945179B (en) | 2017-12-20 | 2017-12-20 | Turbo-charged combustor |
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| Publication Number | Publication Date |
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| CN109945179A CN109945179A (en) | 2019-06-28 |
| CN109945179B true CN109945179B (en) | 2021-04-06 |
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| CN201711386011.8A Active CN109945179B (en) | 2017-12-20 | 2017-12-20 | Turbo-charged combustor |
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Family Cites Families (8)
| 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 |
| 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 |
| CN104197327B (en) * | 2014-09-02 | 2018-03-02 | 李良君 | A kind of alcohol radical burner |
| 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 |
| CN207729590U (en) * | 2017-12-20 | 2018-08-14 | 洁醇事业股份有限公司 | Turbocharging type combustor |
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