Deflagration-proof combustion chamber structure

Abstract

The utility model discloses an anti -explosion combustion cavity structure, specifically related to the technical field of combustion cavity structure, including the combustion cavity cylinder for guiding flow, be provided with control air intake assembly on the combustion cavity cylinder, control air intake assembly includes two for the shunt fan cylinder of shunt of setting in the combustion cavity cylinder, two shunt fan cylinder between be provided with the valve for controlling flow. The utility model discloses through setting control air intake assembly, valve closure, realize the function of plugging the middle part of combustion cavity cylinder, and the exhaust gas pipeline makes the inner chamber both ends of combustion cavity cylinder intercommunication, and it is easy to exhaust to the atmosphere after the flue gas is filtered by the filter, reduces the pollution, and through temperature sensor response combustion cavity cylinder temperature then cooperate with the airflow that guiding fan is delivered to the combustion cavity cylinder, realizes the function of adjusting the oxygen content in the combustion cavity cylinder, avoids the situation of the explosion.

Description

Technical Field

[0001] This utility model relates to the field of combustion chamber structure technology, and more specifically, to an explosion-proof combustion chamber structure. Background Technology

[0002] The burner head is the key core component of the entire burner. Its function is to mix the fuel gas and combustion air and organize combustion to release heat for practical needs. The structure of this component determines the reliability and stability of the combustion process, as well as the velocity and temperature distribution throughout the combustion zone, all of which are key factors affecting flue gas emissions.

[0003] Among them, the patent with announcement number CN218442286U discloses an adjustable premixed burner premixed chamber structure, including an intake cone, a mixing disc, a gas butterfly valve adapter, a mixing disc adjusting screw, a mixing chamber, an annular hole in the intake cone, and a flame tube. The inner cavity of the intake cone is coaxially provided with an adjusting rod flow stabilizer. The inner cavity of the adjusting rod flow stabilizer has a threaded hole and the mixing disc adjusting screw is threadedly connected to the inner cavity of the threaded hole. The inner end of the mixing disc adjusting screw is connected to the mixing disc. One end of the gas butterfly valve adapter is welded to the mixing chamber and the other end is connected to the natural gas butterfly valve interface flange.

[0004] When in use, this structure can control the mixing ratio to make the combustion temperature lower than the theoretical combustion temperature, and also lower or slightly higher than the starting temperature of thermal nitrogen oxides formation. This can reduce the amount of nitrogen oxides generated. Compared with traditional diffusion combustion, the combustion conditions are better, the oxygen-air coefficient is better controlled, and the waste of gas heat energy is reduced while reducing the generation of nitrogen oxides and carbon dioxide. However, it is not easy to control the intake air volume within a certain range to achieve temperature control, and the direct emission of flue gas also pollutes the environment. Utility Model Content

[0005] In order to overcome the above-mentioned defects of the prior art, the present invention provides an explosion-proof combustion chamber structure, which aims to solve the problems mentioned in the background art.

[0006] This utility model provides the following technical solution: an explosion-proof combustion chamber structure, including a combustion chamber cylinder for guiding airflow, wherein an air intake control assembly is provided on the combustion chamber cylinder;

[0007] The air intake control assembly includes two flow divider fans disposed inside the combustion chamber for flow splitting, and a valve for controlling the flow rate is disposed between the two flow divider fans. Both the flow divider fans and the valve are provided with a horizontal shaft for support.

[0008] An ignition controller for power supply is provided at one end of the inner cavity of the combustion chamber, and a temperature sensor for temperature detection is provided at one end of the horizontal shaft. The air intake control assembly also includes a support frame disposed inside the combustion chamber. The support frame is detachably connected to the combustion chamber, and a number of guide fans are disposed on the outer side of the support frame, each located on one side of a corresponding split fan cylinder.

[0009] As can be seen, in the above technical solution, the temperature sensor feedback controls the flow guide fan to be fully open, allowing airflow to enter the combustion chamber. The valve is closed to block the middle of the combustion chamber, while the valve is open to connect the two ends of the combustion chamber, enabling segmented control of the combustion chamber. Furthermore, the temperature sensor senses the temperature inside the combustion chamber and then works with the flow guide fan to deliver airflow into the combustion chamber, thereby regulating the oxygen content inside the combustion chamber and preventing deflagration.

[0010] Optionally, in a possible implementation, a protective tube is fitted around the outside of the combustion chamber. Two protective sleeves are provided on the protective tube, and each of the two protective sleeves is provided with an external leakage filter screen. Each external leakage filter screen is located on the side of a corresponding guide fan. Hollow discs are provided at both ends of the protective tube, and each hollow disc is installed on the protective tube through a butt joint. The two hollow discs are connected through a flue gas pipeline, and a filter is embedded in one of the hollow discs.

[0011] As can be seen, in the above technical solution, the exhaust pipe connects the two ends of the combustion chamber, making it easier for the flue gas to be filtered by the filter and discharged into the atmosphere, thus reducing pollution.

[0012] The technical effects and advantages of this utility model are as follows:

[0013] By setting up the intake control assembly, the ignition controller delivers the combustion medium to the combustion chamber for combustion. The temperature sensor feedback controls the flow guide fan to open fully, allowing airflow to enter the combustion chamber. The valve closes, sealing the middle of the combustion chamber. The exhaust pipe connects the two ends of the combustion chamber, facilitating the filtration of flue gas before it is discharged into the atmosphere, reducing pollution.

[0014] The valve opening connects the two ends of the combustion chamber, enabling segmented control of the combustion chamber. The temperature sensor detects the temperature inside the combustion chamber and, in conjunction with the airflow guide fan, delivers airflow into the combustion chamber, thereby regulating the oxygen content and preventing deflagration. Attached Figure Description

[0015] To more clearly illustrate the technical solutions in this disclosure, the accompanying drawings used in some embodiments will be briefly described below. Obviously, the drawings described below are only drawings of some embodiments of this disclosure, and those skilled in the art can obtain other drawings based on these drawings. In addition, the drawings described below can be regarded as schematic diagrams and are not intended to limit the actual size of the product, the actual flow of the method, the actual timing of the signals, etc. involved in the embodiments of this disclosure.

[0016] Figure 1 This is a front view of the overall structure of this utility model.

[0017] Figure 2 This is a schematic diagram of the intake control assembly of this utility model.

[0018] Figure 3 This is a schematic diagram of the protective tube, support frame, and protective sleeve of this utility model.

[0019] Figure 4 This is a schematic diagram of the diverter fan, valve, and ignition controller of this utility model.

[0020] The attached diagram is labeled as follows: 1. Combustion chamber; 2. Flow divider; 3. Horizontal shaft; 4. Valve; 5. Ignition controller; 6. Temperature sensor; 7. Support frame; 8. Flow divider; 9. Protective sleeve; 10. External leakage filter; 11. Filter; 12. Smoke exhaust pipe; 13. Threaded joint; 14. Hollow disc; 15. Protective tube. Detailed Implementation

[0021] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0022] As attached Figures 1-4 The anti-deflagration combustion chamber structure shown uses a control air intake component on the upper combustion chamber cylinder 1. When valve 4 is opened, the two ends of the inner cavity of the combustion chamber cylinder 1 are connected, realizing the function of segmented control of the combustion chamber of the combustion chamber cylinder 1. The temperature sensor 6 senses the temperature inside the combustion chamber cylinder 1 and then works with the guide fan 8 to deliver airflow into the combustion chamber cylinder 1, thereby regulating the oxygen content inside the combustion chamber cylinder 1 and preventing deflagration. The specific structural settings of the components are as follows.

[0023] The intake control assembly includes two flow divider fans 2 disposed inside the combustion chamber 1 for flow splitting, and a valve 4 for flow control is disposed between the two flow divider fans 2. Both the flow divider fans 2 and the valve 4 are provided with a horizontal shaft 3 for support.

[0024] An ignition controller 5 for power supply is provided at one end of the inner cavity of the combustion chamber 1, and a temperature sensor 6 for temperature detection is provided at one end of the horizontal shaft 3.

[0025] The intake control assembly also includes a support frame 7 disposed inside the combustion chamber 1. The support frame 7 is detachably connected to the combustion chamber 1, and a number of guide fans 8 are disposed on the outside of the support frame 7, which are respectively located on one side of the corresponding split fan cylinder 2.

[0026] The outer side of the combustion chamber 1 is fitted with a protective tube 15, and two protective sleeves 9 are provided on the protective tube 15. Each of the two protective sleeves 9 is provided with an external leakage filter 10, and each external leakage filter 10 is located on one side of the corresponding guide fan 8. Hollow discs 14 are provided at both ends of the protective tube 15, and each hollow disc 14 is installed on the protective tube 15 through a connector 13. The two hollow discs 14 are connected through the exhaust pipe 12, and a filter 11 is embedded in one of the hollow discs 14.

[0027] The specific working principle is as follows: the ignition controller 5 delivers the combustion medium to the combustion chamber 1 for combustion. The temperature sensor 6 controls the flow guide fan 8 to be fully open, allowing airflow to enter the combustion chamber 1. The valve 4 is closed to block the middle of the combustion chamber 1. The valve 4 is opened to connect the two ends of the inner cavity of the combustion chamber 1, realizing the function of segmented control of the combustion chamber of the combustion chamber 1. The temperature sensor 6 senses the temperature inside the combustion chamber 1 and then works with the flow guide fan 8 to deliver airflow to the combustion chamber 1, thereby regulating the oxygen content inside the combustion chamber 1 and preventing deflagration.

[0028] Furthermore, by using temperature sensor 6 to provide feedback on the opening of valve 4 and the airflow delivered by guide fan 8, the intake volume is controlled within a certain range, thereby achieving temperature control.

[0029] Furthermore, the exhaust pipe 12 connects the two ends of the combustion chamber 1, making it easier for the flue gas to be filtered by the filter 11 and discharged into the atmosphere, thus reducing pollution.

[0030] Unlike existing technologies, this application discloses an anti-deflagration combustion chamber structure. By opening valve 4, the two ends of the inner cavity of combustion chamber 1 are connected, enabling segmented control of the combustion chamber of combustion chamber 1. Furthermore, by sensing the temperature inside combustion chamber 1 through temperature sensor 6 and then cooperating with guide fan 8 to deliver airflow into combustion chamber 1, the oxygen content inside combustion chamber 1 is regulated, thus preventing deflagration.

[0031] The above are merely preferred embodiments of the present utility model and are not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. An explosion-proof combustion chamber structure, comprising a combustion chamber cylinder (1) for guiding flow, characterized in that: The combustion chamber (1) is equipped with an air intake control assembly; The air intake control assembly includes two flow divider fans (2) disposed in the combustion chamber (1) for flow division, and a valve (4) for flow control is disposed between the two flow divider fans (2). Both the flow divider fans (2) and the valve (4) are provided with a horizontal shaft (3) for support. An ignition controller (5) for power supply is provided at one end of the inner cavity of the combustion chamber (1), and a temperature sensor (6) for temperature detection is provided at one end of the horizontal shaft (3).

2. The explosion-proof combustion chamber structure according to claim 1, characterized in that: The air intake control assembly also includes a support frame (7) disposed inside the combustion chamber (1), and the support frame (7) is detachably connected to the combustion chamber (1).

3. The explosion-proof combustion chamber structure according to claim 2, characterized in that: The support frame (7) has several guide fans (8) located on one side of the corresponding diversion fan cylinder (2).

4. The explosion-proof combustion chamber structure according to claim 1, characterized in that: The outer side of the combustion chamber (1) is fitted with a protective tube (15), and two protective sleeves (9) are provided on the protective tube (15).

5. The explosion-proof combustion chamber structure according to claim 4, characterized in that: Each of the two protective sleeves (9) is provided with an external leakage filter (10), and each external leakage filter (10) is located on one side of the corresponding guide fan (8).

6. The explosion-proof combustion chamber structure according to claim 4, characterized in that: Hollow discs (14) are provided at both ends of the protective tube (15), and each hollow disc (14) is installed on the protective tube (15) through a connector (13).

7. The explosion-proof combustion chamber structure according to claim 6, characterized in that: The two hollow discs (14) are connected by a smoke exhaust pipe (12), and a filter (11) is embedded in one of the hollow discs (14).

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