FR3075318A3 - BURNER-JET - Google Patents

Abstract

A jet burner of the present disclosure generally includes a burner unit and an air blower disposed at a rear end of a burning chamber of the burner unit, wherein the burner unit is equipped. a fuel tank for storing a fuel and the combustion chamber having a tubular shape. The interior of the combustion chamber is equipped with at least one nozzle, at least one fuel pipe coupled to the fuel tank is installed at each nozzle, a front end of the combustion chamber is equipped with a pipe jet, and a pipe diameter of each jet pipe is less than an internal diameter of the fire chamber. Under the reaction of the jet pipe, the burning time of the fuel in the interior of the combustion chamber is increased, so as to achieve the objective of increasing fuel burn efficiency.

Description

CONTEXT

1. TECHNICAL FIELD

The present disclosure relates to a burner, in particular a jet burner for sufficiently increasing fuel burning efficiency.

2. DESCRIPTION OF THE RELATED ART

According to the prior art, the burner is widely used in a boiler, a heating furnace, a drying equipment and an industrial furnace and other thermal machinery, and the basic architecture of the conventional burner is shown in FIG. conventional burner is equipped with a burner chamber 12 coupled to an air blower 11, and the interior of the burner chamber 12 is equipped with a plurality of nozzles 13 coupled to a fuel delivery device (not shown). on the drawings). Primarily, the air blower 11 generates the accelerating gaseous fluid in the combustion chamber 12, and after the fuel injected into the combustion chamber 12 is ignited, accompanying the gaseous fluid in the combustion chamber 12, the fire may burst and burn at the front end of the burning chamber 12.

The classic burner fuel is mainly diesel of good ignition capacity. Currently, a burner is also provided as follows. After the burner uses a heater to heat the heavy oil at the high temperature of 110 degrees Celsius, the high pressure pump transfers the heated heavy oil to the firing position via the piping, and thus the heavy oil can to be the fuel. The main applications of the burners are currently applied thermal machineries and applied heat exchange devices, both of which are directly coupled to the front ends of the burner burners 12, and thus the increased efficiency is entirely determined according to the invention. fuel burning efficiency and fire reaction range at the front end of the firebox 12.

Although the conventional burner uses the air blower to generate the gaseous fluid in acceleration, in actual application, the fuel injected into the burner chamber can be blown from the burner chamber into the incomplete burner state. because of the over-reaction of the gaseous fluid in acceleration, so that the conventional burner can not have the expected fuel burning efficiency.

ABSTRACT

To achieve one of the objectives mentioned in this disclosure, the present disclosure proposes a jet burner capable of sufficiently increasing the fuel burn efficiency.

An embodiment of the present disclosure provides a jet burner of the present disclosure comprising at least one burner unit and an air blower; wherein: the burner unit is equipped with a fuel tank for storing a fuel and a burner chamber having a tubular shape, the interior of the burner chamber is equipped with at least one nozzle, at the unless a fuel pipe coupled to the fuel tank is disposed at each nozzle, a front end of the fire chamber is equipped with at least one jet pipe, and a pipe diameter of each jet pipe is less than an internal diameter of the burning chamber; the air blower is coupled to the burning chamber.

Accordingly, under the reaction of the jet pipe, the jet burner of the present disclosure can increase the fuel burning dwell time in the interior of the fire chamber, so as to achieve the objective of increasing the fuel burn rate. fuel burning efficiency.

Regarding the above features, the jet burner further comprises a high pressure gas supply unit; the high pressure gas supply unit is equipped with a gas storage tank for storing a high pressure gas, and each nozzle is equipped with a high pressure pipe coupled to the gas storage tank.

Regarding the above features, the jet burner further comprises an auxiliary wind speed unit; the auxiliary wind speed unit is equipped with a wind speed tank covering at least the outside of the air blower, a front end and a rear end of the wind speed tank are open, a gap for creating a passage for a gaseous fluid is formed between the wind speed reservoir and the air blower, and the rear end of the wind speed reservoir is equipped with a blade and a motor for driving the blade in rotation.

Regarding the above features, the jet burner further comprises a control unit; the control unit is equipped with a control circuit, a matched lighter in the interior of the combustion chamber and a fuel pump coupled to the fuel pipe of each nozzle, and the control is at least electrically connected to the lighter, the fuel pump and the air blower.

Regarding the above features, the jet burner further comprises a high pressure gas supply unit and an auxiliary wind speed unit; the high pressure gas supply unit is equipped with a gas storage tank for storing a high pressure gas, and each nozzle is equipped with a high pressure pipe coupled to the gas storage tank; the auxiliary wind speed unit is equipped with a wind speed tank covering at least the outside of the air blower, a front end and a rear end of the wind speed tank are open, a gap for creating a passage for a gaseous fluid is formed between the wind speed reservoir and the air blower, and the rear end of the wind speed reservoir is equipped with a blade and a motor for driving the blade in rotation.

Regarding the above features, the jet burner further comprises a high pressure gas supply unit and a control unit; the high pressure gas supply unit is equipped with a gas storage tank for storing a high pressure gas, and each nozzle is equipped with a high pressure pipe coupled to the gas storage tank; the control unit is equipped with a control circuit, a lighter arranged in correspondence within the combustion chamber, a fuel pump coupled to the fuel pipe of each nozzle, and a choke coupled to the high-pressure hose of each nozzle, and the control circuit is at least electrically connected to the lighter, the fuel pump, the choke and the air blower.

Regarding the above features, the jet burner further comprises an auxiliary wind speed unit and a control unit; the auxiliary wind speed unit is equipped with a wind speed tank covering at least the outside of the air blower, a front end and a rear end of the wind speed tank are open, a gap for creating a passage for a gaseous fluid is formed between the wind speed reservoir and the air blower, and the rear end of the wind speed reservoir is equipped with a blade and a motor for driving the blade in rotation; the control unit is equipped with a control circuit, a matched lighter in the interior of the combustion chamber and a fuel pump coupled to the fuel pipe of each nozzle, and the control is at least electrically connected to the lighter, the fuel pump, the air blower and the engine of the auxiliary wind speed unit.

Regarding the above features, the jet burner further comprises a high pressure gas supply unit, an auxiliary wind speed unit and a control unit; the high pressure gas supply unit is equipped with a gas storage tank for storing a high pressure gas, and each nozzle is equipped with a high pressure pipe coupled to the gas storage tank; the auxiliary wind speed unit is equipped with a wind speed tank covering at least the outside of the air blower, a front end and a rear end of the wind speed tank are open, a gap for creating a passage for a gaseous fluid is formed between the wind speed reservoir and the air blower, and the rear end of the wind speed reservoir is equipped with a blade and a motor for driving the blade in rotation; the control unit is equipped with a control circuit, a lighter arranged in correspondence within the combustion chamber, a fuel pump coupled to the fuel pipe of each nozzle, and a choke coupled to the high-pressure hose of each nozzle, and the control circuit is at least electrically connected to the lighter, fuel pump, choke, air blower and auxiliary unit motor wind speed.

With respect to the above features, the auxiliary wind speed unit is provided with a lubricant reservoir for storing a lubricant and at least one lubricant pipe coupled to the lubricant reservoir and a pivot establishment location. on an axis of rotation of the motor.

Regarding the above features, the auxiliary wind speed unit is equipped with at least one hatch disposed at a tank side of the wind speed reservoir, the hatch being capable of opening and closing.

With respect to the above features, the auxiliary wind speed unit is provided with a lubricant reservoir for storing a lubricant and at least one lubricant pipe coupled to the lubricant reservoir and a pivot establishment location. on an axis of rotation of the engine, and the auxiliary wind speed unit is equipped with at least one hatch disposed at a reservoir side of the wind speed reservoir, the hatch being capable of opening and closing .

Regarding the above features, the high pressure gas supply unit is further equipped with an air compressor coupled to the gas storage tank, and the air compressor is electrically connected to the control circuit of the control unit.

Regarding the above features, the high pressure gas supply unit is further equipped with an air compressor coupled to the gas storage tank, and the air compressor is electrically connected to the control circuit of the control unit ; and the auxiliary wind speed unit is provided with a lubricant reservoir for storing a lubricant and at least one lubricant hose coupled to the lubricant reservoir and a pivot establishment location on a lubricant axis. rotation of the motor.

Regarding the above features, the high pressure gas supply unit is further equipped with an air compressor coupled to the gas storage tank, and the air compressor is electrically connected to the control circuit of the control unit ; and the auxiliary wind speed unit is equipped with at least one hatch disposed at a reservoir side of the wind speed reservoir, the hatch being capable of opening and closing.

Regarding the above features, the high pressure gas supply unit is further equipped with an air compressor coupled to the gas storage tank, and the air compressor is electrically connected to the control circuit of the control unit ; the auxiliary wind speed unit is equipped with a lubricant reservoir for storing a lubricant and at least one lubricant pipe coupled to the lubricant reservoir and a pivot establishment location on an engine rotation axis , and the auxiliary wind speed unit is equipped with at least one hatch disposed at a tank side of the wind speed tank, the hatch being capable of opening and closing.

Primarily under the reaction of the jet hose, the jet burner proposed by the present disclosure can increase the burning time of the fuel within the combustion chamber to achieve the goal of increasing fuel burn efficiency. In addition, by using the effect that the high pressure gas supply unit accelerates the fuel entering the nozzle, the atomization effect of the fuel that has passed the nozzle is increased, and simultaneously, the flow of gaseous fluid is supplied to the inner combustion chamber to increase the fuel burn efficiency. Similarly, under the reaction of the auxiliary wind speed unit, the flow velocity and the flow flow of the accelerated gaseous fluid are increased, so that the relatively positive and reliable means for increasing the burning efficiency Fuel and performance are provided, and the effect of high temperature on relative units can be prevented. In addition, using the jet burner, not only the pollutant generated by the burning of diesel and heavy oil can be reduced, but it also helps the alcohol to serve as fuel, so that the jet burner can be used in the environment of a restaurant, organization or school room.

BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings are included to provide further understanding of the present disclosure, and are incorporated in and constitute a part of this specification. The drawings illustrate exemplary embodiments of the present disclosure and, together with the description, serve to explain the principles of the present disclosure.

Figure 1 is an architectural drawing of a conventional burner.

Fig. 2 is a basic architectural drawing of a jet burner according to a first embodiment of the present disclosure.

Figure 3 is a three-dimensional outline drawing of a burning chamber with respect to a front view of the present disclosure.

Figure 4 is an architectural sectional drawing of a burn chamber of the present disclosure.

Fig. 5 is a sectional architectural drawing of a jet burner according to a first embodiment of the present disclosure.

Fig. 6 is an operating drawing of a jet burner of the present disclosure.

Fig. 7 is a three-dimensional outline drawing of a burning chamber and an auxiliary wind speed unit according to a first embodiment of the present disclosure.

Fig. 8 is an operating drawing of an auxiliary wind speed unit of the present disclosure.

Fig. 9 is a three-dimensional outline drawing of a burning chamber and an auxiliary wind speed unit according to a second embodiment of the present disclosure.

DESCRIPTION OF EXAMPLES OF EMBODIMENTS

To understand the technical features, content and advantages of the present disclosure and its effectiveness, the present disclosure will be described in detail with reference to the accompanying drawings. The drawings are for illustration and help only and may not necessarily be the true scale and configuration of the present disclosure. Accordingly, the scope of the present disclosure should not be limited to the scale and configuration of the accompanying drawings.

The present disclosure provides primarily a jet burner to sufficiently increase the fuel burning efficiency, the jet burner of the present disclosure generally comprises a burner unit 20 and an air blower 30 as shown in FIGS. , and the details are illustrated as follows. The burner unit 20 is equipped with a fuel tank 21 for storing a fuel and a combustion chamber 22 having a tubular shape, the inside of the combustion chamber 22 is equipped with at least one nozzle 23 at least one fuel pipe 24 coupled to the fuel tank 21 is disposed at each nozzle 23, a front end of the combustion chamber 22 is equipped with at least one jet pipe 26, and a pipe diameter of each jet pipe 26 is smaller than an internal diameter of the burning chamber 22.

The air blower 30 is coupled to the burn chamber 22, so that the gaseous fluid can be supercharged by the air blower 30 and then supplied to the blast chamber 22. In one embodiment, the blower 22 air 30 is disposed at a rear end of the burning chamber 22, and a wind blowing direction of the air blower 30 is parallel to an axis of the burning chamber 22. As a variant, in a In another embodiment, the air blower 30 is coupled to the burn chamber 22 via piping (not shown in the drawings), the piping communicating with the air blower 30 and the burn chamber 22, so that that the gaseous fluid supercharged by the air blower 30 can be supplied to the combustion chamber 22. In the practical implementation, the air blower 30 is preferably disposed on the axis of the combustion chamber 22.

Principally, when the jet burner is operating, under the reaction of the jet pipes 26, the fuel burning residence time in the interior of the combustion chamber 22 can be increased (as shown in FIG. to achieve the goal of increasing the efficiency of fuel burning.

In addition, when the jet burner of the present disclosure is implemented, the jet burner may further comprise a high pressure gas supply unit 60. The high pressure gas supply unit 60 is equipped with a gas storage tank 61 for storing a high pressure gas, and each nozzle 23 is equipped with a high pressure pipe 25 coupled to the gas storage tank 61. In the practical implementation, the supply unit High pressure gas 60 may further include an air compressor 62 coupled to the gas storage tank 61, and under the operation of the air compressor 62, the high pressure gas is supplied continuously.

Refer simultaneously to Figures 5, 7 and 8. When the jet burner of the present disclosure is implemented, the jet burner may further comprise an auxiliary wind speed unit 40. The auxiliary wind speed unit 40 is equipped with a wind speed tank 41 covering at least the outside of the air blower 30, a front end and a rear end of the wind speed tank 41 are open, a gap to create a passage for a gaseous fluid is formed between the wind speed reservoir 41 and the air blower 30, and the rear end of the wind speed reservoir 41 is equipped with a blade 42 and a motor 43 to drive the blade 42 in rotation.

Accordingly, under the operating reaction of the blade 42 of the auxiliary wind speed unit 40 (as shown in FIG. 7), the gaseous fluid flow of the air blower 30 is increased, and not only the flow velocity and the flow of the accelerated gaseous fluid are increased, but also the partial flow fluid is accelerated to pass the gap between the wind speed reservoir 41 and the air blower 30, so as to increase the As a result, the relatively positive and reliable means for preventing the effect of high temperature on the relative units can be provided.

It is noted that since the jet burner of the present disclosure can increase the flow velocity and the accelerated flow under the reaction of the auxiliary wind speed unit 40, the size of the air blower can to be reduced. Similarly, because of the design according to which the air blower 30 is disposed on the axis of the combustion chamber 22, the contours of the whole of the combustion chamber 22, the air blower 30 and the auxiliary wind speed unit 40 can be integrated, and this contributes to facilitate the miniature and compact development of the burner.

When the jet burner of the present disclosure is implemented, the jet burner may further comprise a control unit 50. The control unit 50 is equipped with a control circuit 51, a funnel 52 disposed in correspondence within the combustion chamber 22 and a fuel pump 53 coupled to the fuel hose 24 of each nozzle 23, and the control circuit 51 is at least electrically connected to the igniter 52, at the fuel pump 53 and the air blower 30.

As a result, when the control circuit 51 of the control unit 50 loads or sets the related work items or parameters, whether the lighter 52, the fuel pump 53, and the air blower 30 are working or not. is controlled by the control circuit 51 according to the elements and parameters loaded and fixed, so as to achieve the purpose of automatic operation.

When the jet burner of the present disclosure is implemented, the jet burner may further comprise a high pressure gas supply unit 60 and the auxiliary wind speed unit 40. The gas supply unit high pressure 60 is equipped with a gas storage tank 61 for storing a high pressure gas, and each nozzle 23 is equipped with a high pressure pipe 25 coupled to the gas storage tank 61. wind 40 is equipped with a wind speed reservoir 41 covering at least the outside of the air blower 30, a front end and a rear end of the wind speed tank 41 are open, a gap to create a passage for a gaseous fluid is formed between the wind speed reservoir 41 and the air blower 30, and the rear end of the wind speed reservoir 41 is equipped with a blade 42 and a motor 43 to drive the wind. has a blade 42 in rotation.

When the jet burner of the present disclosure is implemented, the jet burner may further comprise a high pressure gas supply unit 60 and a control unit 50. The high pressure gas supply unit 60 is equipped with a gas storage tank 61 for storing a high pressure gas, and each nozzle 23 is equipped with a high pressure pipe 25 coupled to the gas storage tank 61. The control unit 50 is equipped with a control circuit 51, a lighter 52 arranged in correspondence within the combustion chamber 22, a fuel pump 53 coupled to the fuel pipe 24 of each nozzle 23, and a choke 54 coupled to the high pressure hose 25 of each nozzle 23, and the control circuit 51 is at least electrically connected to the funnel 52, the fuel pump 53, the choke 54 and the air blower 30.

When the jet burner of the present disclosure is implemented, the jet burner may further comprise an auxiliary wind speed unit 40 and a control unit 50. The auxiliary wind speed unit 40 is equipped with a wind speed reservoir 41 covering at least the outside of the air blower 30, a front end and a rear end of the wind speed tank 41 are open, a gap to create a passage for a gaseous fluid is formed between the wind speed reservoir 41 and the air blower 30, and the rear end of the wind speed reservoir 40 is equipped with a blade 42 and a motor 43 for driving the blade 42 in rotation. The control unit 50 is equipped with a control circuit 51, a lighter 52 arranged in correspondence within the combustion chamber 22 and a fuel pump 53 coupled to the fuel pipe 24 of each nozzle 23, and the control circuit 51 is at least electrically connected to the funnel 52, the fuel pump 53, the air blower 30 and the motor 43 of the auxiliary wind speed unit 40.

Certainly, when the jet burner of the present disclosure is implemented, the jet burner may further comprise the high pressure gas supply unit 60, the auxiliary wind speed unit 40 and the control unit 50. The high pressure gas supply unit 60 is equipped with the gas storage tank 61 for storing the high pressure gas, and each nozzle 23 is equipped with the high pressure pipe 25 coupled to the gas storage tank 61 The auxiliary wind speed unit 40 is equipped with the wind speed tank 41 covering at least the outside of the air blower 30, the front end and the rear end of the wind speed tank 41 are emerging, the gap to create a passage for the gaseous fluid is formed between the wind speed reservoir 41 and the air blower 30, and the rear end of the wind speed reservoir 41 is equipped with the blade 42 andmotor 43 to drive the blade 42 in rotation. The control unit 50 is equipped with the control circuit 51, the lighter 52 arranged in correspondence within the combustion chamber 22, of the fuel pump 53 coupled to the fuel pipe 24 of each nozzle 23 and the throttle coupled to the high pressure hose 25 of each nozzle 23, and the control circuit 51 is at least electrically connected to the funnel 52, the fuel pump 53, the air blower 30, the choke 54 and the motor 43 of the auxiliary wind speed unit 40.

According to the possible implementations above of the present disclosure, the auxiliary wind speed unit 40 is equipped with a lubricant reservoir 44 (as shown in FIG. 5) for storing a lubricant and at least one lubricant pipe 45 coupled to the lubricant reservoir 44 and to a pivot establishment location on an axis of rotation of the engine 43. By use of the lubricant reservoir 44 and the lubricant hose 45 to typically supply the lubricant to the lubricant. The pivoting location of the motor 43, the motor 43 is assured to operate successfully, and the entire operating performance of the jet burner can be increased.

Refer simultaneously to FIG. 9. In accordance with the above possible implementations of the present disclosure, the auxiliary wind speed unit 40 is provided with at least one hatch 411 disposed at a reservoir side of the tank. wind speed 41, the hatch 411 being capable of opening and closing. By the use of the hatch 411 design, the purpose of facilitating assembly and checking the relative units can be achieved.

Of course, as shown both in FIG. 5 and FIG. 9, the auxiliary wind speed unit 40 is further equipped with the lubricant reservoir 44 for storing the lubricant and the at least one lubricant pipe 45 coupled to the lubricant reservoir 44 and the pivot establishment location on the axis of rotation of the motor 43, and the wind speed reservoir 41 is preferably equipped with the at least one hatch 411 disposed at the tank side of the wind speed tank 41, the hatch 411 being capable of opening and closing.

Moreover, in the embodiment in which the jet burner comprises the control unit 50 and the high pressure gas supply unit 60 which is further equipped with the air compressor 62 coupled to the gas storage tank 61, the air compressor 62 is electrically connected to the control unit 51 of the control unit 50, and under the operation of the air compressor 62, the high pressure gas is supplied continuously.

In the embodiment in which the jet burner of the present disclosure comprises the control unit 50 and the high pressure gas supply unit 60 further equipped with the air compressor 62 coupled to the gas storage tank 61 , and the air compressor 62 is electrically connected to the control circuit of the control unit 50, the auxiliary wind speed unit 40 may further be provided with the lubricant reservoir 44 for storing the lubricant and the minus a lubricant pipe 45 coupled to the lubricant reservoir 44 and the pivot establishment location on the axis of rotation (i.e. the bearing position) of the engine 43.

In the embodiment in which the jet burner of the present disclosure comprises the control unit 50 and the high pressure gas supply unit 60 further equipped with the air compressor 62 coupled to the gas storage tank 61 , and the air compressor 62 is electrically connected to the control circuit of the control unit 50, the auxiliary wind speed unit 40 is equipped with the at least one hatch 411 disposed at the reservoir side of the tank of the wind speed 41, the hatch 411 being capable of opening and closing.

Certainly, in the embodiment in which the jet burner of the present disclosure comprises the control unit 50 and the high pressure gas supply unit 60 further equipped with the air compressor 62 coupled to the fuel tank. storing gas 61, and the air compressor 62 is electrically connected to the control circuit of the control unit 50, the auxiliary wind speed unit 40 may further be provided with the lubricant reservoir 44 for storing the lubricant and at least one lubricant pipe 45 coupled to the lubricant reservoir 44 and the pivot location on the axis of rotation (i.e., the bearing position) of the engine 43, and auxiliary wind speed unit 40 is preferably equipped with the at least one hatch 411 disposed at the reservoir side of the wind speed reservoir 41, the hatch 411 being capable of opening and closing.

In comparison with the conventional prior art, the jet burner disclosed by the present disclosure, under the reaction of the jet pipe, the burning time of the fuel in the interior of the fire chamber is increased to achieve the objective of 'increase fuel burn efficiency. By using the effect that the high pressure gas supply unit accelerates the microatomization of the fuel entering the nozzle, the fuel molecules are further refined and burned more completely, so that the objective of increasing the efficiency of fuel burning. In addition, under the reaction of the air blower, the gaseous fluid entering the combustion chamber is increased, so that the fuel is burned more completely to increase the fuel burn performance. Similarly, under the reaction of the auxiliary wind speed unit, the flow velocity and the flow flow of the accelerated gaseous fluid are increased, so that the relatively positive and reliable means for increasing the burning efficiency Fuel and performance are provided, and the effect of high temperature on relative units can be prevented. In addition, by the use of the jet burner, not only the pollutant generated by burning diesel and heavy oil can be reduced, but also it helps the alcohol to serve as fuel, so that the jet burner may be used in the environment of a restaurant, organization or school room.

The foregoing descriptions merely represent the exemplary embodiment of the present disclosure, without any intention to limit the scope of the present disclosure. Various changes, alternatives or equivalent modifications based on the claims of the present disclosure are therefore all considered to be encompassed by the scope of the present disclosure.

Claims (17)

A jet burner comprising at least: a burner unit (20) and an air blower (30); wherein: the burner unit (20) is equipped with a fuel tank (21) for storing fuel and a burner chamber (22) having a tubular shape, the interior of the burner chamber ( 22) is equipped with at least one nozzle (23), at least one fuel pipe (24) coupled to the fuel tank (21) is disposed at each nozzle (23), a front end of the combustion chamber (22) is equipped with at least one jet pipe (26), and a pipe diameter of each jet pipe (26) is less than an internal diameter of the burning chamber (22); the air blower (30) is coupled to the combustion chamber (22). The jet burner according to claim 1, wherein the jet burner further comprises a high pressure gas supply unit (60); the high pressure gas supply unit (60) is equipped with a gas storage tank (61) for storing a high pressure gas, and each nozzle (23) is equipped with a high pressure pipe (25) coupled to the gas storage tank (61). The jet burner according to claim 1, wherein the jet burner further comprises an auxiliary wind speed unit (40); the auxiliary wind speed unit (40) is equipped with a wind speed tank (41) covering at least the outside of the air blower (30), a front end and a rear end of the air blower (40). wind speed (41) are open, a gap to create a passage for a gaseous fluid is formed between the wind speed tank (41) and the air blower (30), and the rear end of the speed tank wind (41) is equipped with a blade (42) and a motor (43) for driving the blade (42) in rotation. The jet burner according to claim 1, wherein the jet burner further comprises a control unit (50); the control unit (50) is equipped with a control circuit (51), a lighter (52) arranged in correspondence within the combustion chamber (22) and a fuel pump ( 53) coupled to the fuel hose (24) of each nozzle (23), and the control circuit (51) is at least electrically connected to the lighter (52), the fuel pump (53) and the snowblower of air (30). The jet burner according to claim 1, wherein the jet burner further comprises a high pressure gas supply unit (60) and an auxiliary wind speed unit (40); The high pressure gas supply unit (60) is equipped with a gas storage tank (61) for storing a high pressure gas, and each nozzle (23) is equipped with a high pressure pipe (25). coupled to the gas storage tank (61); the auxiliary wind speed unit (40) is equipped with a wind speed tank (41) covering at least the outside of the air blower (30), a front end and a rear end of the air blower (40). wind speed (41) are open, a gap to create a passage for a gaseous fluid is formed between the wind speed tank (41) and the air blower (30), and the rear end of the speed tank wind (41) is equipped with a blade (42) and a motor (43) for driving the blade (42) in rotation. The jet burner according to claim 1, wherein the jet burner further comprises a high pressure gas supply unit (60) and a control unit (50); the high pressure gas supply unit (60) is equipped with a gas storage tank (6i) for storing a high pressure gas, and each nozzle (23) is equipped with a high pressure pipe (25) coupled to the gas storage tank (61); the control unit (50) is equipped with a control circuit (51), a lighter (52) arranged in correspondence within the combustion chamber (22), with a fuel pump ( 53) coupled to the fuel hose (24) of each nozzle (23), and a choke (54) coupled to the high pressure hose (25) of each nozzle (23), and the control circuit (51) is less electrically connected to the lighter (52), the fuel pump (53), the choke (54) and the air blower (30). The jet burner according to claim 1, wherein the jet burner further comprises an auxiliary wind speed unit (40) and a control unit (50); the auxiliary wind speed unit (40) is equipped with a wind speed tank (41) covering at least the outside of the air blower (30), a front end and a rear end of the air blower (40). wind speed (41) are open, a gap to create a passage for a gaseous fluid is formed between the wind speed tank (41) and the air blower (30), and the rear end of the speed tank wind turbine (41) is equipped with a blade (42) and a motor (43) for driving the blade (42) in rotation; the control unit (50) is equipped with a control circuit (51), a lighter (52) arranged in correspondence within the combustion chamber (22) and a fuel pump ( 53) coupled to the fuel hose (24) of each nozzle (23), and the control circuit (51) is at least electrically connected to the lighter (52), the fuel pump (53), the snowblower air (30) and the motor (43) of the auxiliary wind speed unit (40). The jet burner according to claim 1, wherein the jet burner further comprises a high pressure gas supply unit (60), an auxiliary wind speed unit (40) and a control unit (50). ; the high pressure gas supply unit (60) is equipped with a gas storage tank (61) for storing a high pressure gas, and each nozzle (23) is equipped with a high pressure pipe (25) coupled to the gas storage tank (61); the auxiliary wind speed unit (40) is equipped with a wind speed tank (41) covering at least the outside of the air blower (30), a front end and a rear end of the air blower (40). wind speed (41) are open, a gap to create a passage for a gaseous fluid is formed between the wind speed tank (41) and the air blower (30), and the rear end of the speed tank wind turbine (41) is equipped with a blade (42) and a motor (43) for driving the blade (42) in rotation; the control unit (50) is equipped with a control circuit (51), a lighter (52) arranged in correspondence within the combustion chamber (22), with a fuel pump ( 53) coupled to the fuel hose (24) of each nozzle (23), and a choke (54) coupled to the high pressure hose (25) of each nozzle (23), and the control circuit (51) is less electrically connected to the lighter (52), the fuel pump (53), the choke (54), the air blower (30) and the motor (43) of the auxiliary speed unit wind (40). Jet burner according to claim 3, wherein the auxiliary wind speed unit (40) is equipped with a lubricant reservoir (44) for storing a lubricant and at least one lubricant pipe (45). coupled to the lubricant reservoir (44) and to a pivot location on an axis of rotation of the engine (43). The jet burner according to the claim, wherein the auxiliary wind speed unit (40) is equipped with at least one hatch (411) disposed at a reservoir side of the wind speed reservoir (41). in which the hatch (411) is capable of opening and closing. The jet burner according to claim 3, wherein the auxiliary wind speed unit (40) is equipped with a lubricant reservoir (44) for storing a lubricant and at least one lubricant pipe (45). coupled to the lubricant reservoir (44) and to a pivot location on an axis of rotation of the motor (43), and the auxiliary wind speed unit (40) is provided with at least one flap (411). ) disposed at a tank side of the wind speed tank (41), wherein the hatch (411) is capable of opening and closing. The jet burner according to claim 6, wherein the high pressure gas supply unit (60) is further equipped with an air compressor (62) coupled to the gas storage tank (61), and the air compressor (62) is electrically connected to the control circuit (51) of the control unit (50). The jet burner according to claim 8, wherein the high pressure gas supply unit (60) is further equipped with an air compressor (62) coupled to the gas storage tank (61), and the air compressor (62) is electrically connected to the control circuit (51) of the control unit (50); and the auxiliary wind speed unit (40) is provided with a lubricant reservoir (44) for storing a lubricant and at least one lubricant hose (45) coupled to the lubricant reservoir (44) and a pivot setting location on an axis of rotation of the motor (43). The jet burner according to claim 8, wherein the high pressure gas supply unit (60) is further equipped with an air compressor (62) coupled to the gas storage tank (61), and the air compressor (62) is electrically connected to the control circuit (51) of the control unit (50); and the auxiliary wind speed unit (40) is equipped with at least one flap (411) disposed at a reservoir side of the wind speed reservoir (41), wherein the flap (411) is capable of opening and closing. The jet burner according to claim 8, wherein the high pressure gas supply unit (60) is further equipped with an air compressor (62) coupled to the gas storage tank (61), and the air compressor (62) is electrically connected to the control circuit (51) of the control unit (50); the auxiliary wind speed unit (40) is provided with a lubricant reservoir (44) for storing a lubricant and at least one lubricant hose (45) coupled to the lubricant reservoir (44) and at a location for establishing a pivot on an axis of rotation of the motor (43), the auxiliary wind speed unit (40) is equipped with at least one flap (411) disposed at a reservoir side of the speed tank wind (41), wherein the hatch (411) is capable of opening and closing. The jet burner according to claim 1, wherein the air blower (30) is disposed at a rear end of the blast chamber (22), and a blower wind direction of the blower. air (30) is parallel to an axis of the combustion chamber (22). The jet burner of claim 1, wherein the air blower (30) is coupled to the fire chamber (22) via piping.