CN216203311U - Integrated linear combustor system - Google Patents
Integrated linear combustor system Download PDFInfo
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- CN216203311U CN216203311U CN202122706011.XU CN202122706011U CN216203311U CN 216203311 U CN216203311 U CN 216203311U CN 202122706011 U CN202122706011 U CN 202122706011U CN 216203311 U CN216203311 U CN 216203311U
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Abstract
The utility model discloses an integrated linear burner system, comprising: the shell is provided with an accommodating cavity; the combustion assembly is provided with a combustion cavity, a gas inlet assembly is connected to the combustion cavity, and a striking part is arranged in the combustion cavity; the air outlet of the combustion-supporting air supply assembly is communicated with the combustion cavity; the combustion-supporting wind pressure control system is provided with a detection end and a controller, the detection end is used for detecting the air pressure value of combustion-supporting wind, and the controller is used for controlling the on-off of the gas inlet assembly. The technical effect of the scheme is as follows: through setting up combustion-supporting wind pressure control system, can detect the size of combustion-supporting wind pressure, when the numerical value of combustion-supporting wind pressure is not in the actual settlement within range, the detection end gives the controller with signal transmission this moment, then the controller comes the switch of controlling the gas subassembly that admits air to close, and the gas air feed is interrupted in the gas subassembly this moment.
Description
Technical Field
The utility model relates to the technical field of combustors, in particular to an integrated linear combustor system.
Background
The burners can be classified into three types, i.e., an oil burner, a coal burner, and a gas burner. The gas burner takes natural gas and other gases as fuels, and has the characteristics of sufficient combustion, high combustion temperature, easy control of combustion and the like. Therefore, the combustion system with the gas burner is widely applied to various industries, such as petrochemical industry, building materials, electric power, textile, printing and dyeing, steel, metallurgy, machinery, food and the like. The combustion system mainly comprises a combustor, a valve bank and a control part, and has a huge structure, which puts certain requirements on arrangement space. In the control part, a large number of lines exist, and a large amount of time is needed for field installation and debugging and later maintenance, so that the time for putting a customer into use is prolonged, and the installation and debugging are also a test.
In addition, the burner has a large flame and is fiercely combusted, a stable and efficient gas supply scheme is needed, and a certain automatic control is needed to realize the efficient and stable work of the burner.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model discloses an integrated linear combustor which can detect the magnitude of combustion-supporting air pressure by arranging a combustion-supporting air pressure control system, wherein when the numerical value of the combustion-supporting air pressure is not in an actual set range, a signal is transmitted to a controller by a detection end at the moment, then the controller controls the switch of a gas inlet assembly to be closed, and the gas supply in the gas inlet assembly is interrupted at the moment.
Specifically, the present invention discloses an integrated linear burner system, comprising:
the shell is provided with an accommodating cavity;
the combustion assembly is provided with a combustion cavity, a gas inlet assembly is connected to the combustion cavity, and an ignition part is arranged in the combustion cavity;
the air outlet of the combustion-supporting air supply assembly is communicated with the combustion cavity;
the combustion-supporting wind pressure control system, combustion-supporting wind pressure control system has a sense terminal and a controller, the sense terminal is used for detecting the atmospheric pressure value of combustion-supporting wind, the controller is used for controlling the switch that the gas admitted air subassembly.
The technical effect of the scheme is as follows: through setting up combustion-supporting wind pressure control system, can detect the size of combustion-supporting wind pressure, when the numerical value of combustion-supporting wind pressure is not in the actual settlement within range, the detection end gives the controller with signal transmission this moment, then the controller comes the switch of controlling the gas subassembly that admits air to close, and the gas air feed is interrupted in the gas subassembly this moment.
Preferably, two sides of the shell are respectively provided with a circulating air port communicated with the accommodating cavity. The technical effect of the scheme is as follows: the flame of the combustion chamber can be conveniently sprayed out, and the full combustion of the fuel gas can be ensured.
Further, the combustion assembly has an exhaust port communicating with the combustion chamber, the exhaust port facing one of the circulation ports.
Preferably, hold and be equipped with circulation wind pressure control system on the chamber, circulation wind pressure control system has circulation wind pressure detection end and the control unit, the control unit is used for controlling the switch of gas subassembly that admits air. The technical effect of the scheme is as follows: through the scope that detects circulation wind pressure to can indirectly obtain the carminative speed of combustion chamber and stability, when the actual value of circulation wind pressure is not in the setting value, cut off the gas and admit air, thereby can the troubleshooting, prevent dangerous emergence.
Preferably, the gas air inlet assembly comprises a gas inlet pipe, and a double-cut electromagnetic valve is arranged on the gas inlet pipe. The technical effect of the scheme is as follows: the setting of double-cutting solenoid valve can cooperate combustion-supporting wind pressure control system and circulation wind pressure control system to use to can ensure closing in time of gas intake pipe, improve the safety in utilization of combustor.
Preferably, a filter is arranged on the gas inlet pipe. The technical effect of the scheme is as follows: the gas supply of the gas can be filtered, and the cleanness degree of the gas is ensured.
Preferably, a gas high-voltage switch and a gas low-voltage switch are arranged on the gas inlet pipe. The technical effect of the scheme is as follows: the stability of gas intake is maintained by setting a double switch.
Preferably, the combustion-supporting air supply assembly comprises a fan and a fan housing, the fan is mounted on the shell, and the air outlet end of the fan is communicated with the combustion cavity through the fan housing. The technical effect of the scheme is as follows: facilitating the full combustion of the combustion chamber.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings used in the embodiments or the description of the prior art will be briefly described below.
Fig. 1 is a schematic perspective view of an integrated linear burner system according to the present embodiment;
FIG. 2 is a schematic diagram of the internal structure of a receiving chamber of the integrated linear burner system according to the present embodiment;
fig. 3 is a schematic structural view of a front view direction of the integrated linear burner system proposed in the present embodiment;
fig. 4 is a schematic structural diagram of the integrated linear burner system according to the present embodiment in a right view.
Wherein the reference numbers referred to in the figures are as follows:
11-a housing; 12-a containment chamber; 13-a combustion assembly; 14-a gas intake assembly; 15-combustion-supporting air supply assembly; 16-combustion-supporting wind pressure switch; 17-a circulating tuyere; 18-an exhaust port; 19-circulating wind pressure switch; 20-a gas inlet pipe; 21-double-cut electromagnetic valve; 22-gas inlet ball valve; 23-a filter; 24-a gas pressure regulating valve; 25-gas low-voltage switch; 26-gas side leakage switch; 27-gas high-voltage switch; 28-ignition solenoid valve; 29-adjusting the ignition valve; 30-an ignition transformer; 31-a fan; 32-wind shield.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
As shown in fig. 1 to 4, the present embodiment discloses an integrated linear burner system, including:
a shell 11, wherein an accommodating cavity 12 is arranged on the shell 11;
the combustion assembly 13 is provided with a combustion cavity, a gas inlet assembly 14 is connected to the combustion cavity, and an ignition part is arranged in the combustion cavity;
the combustion-supporting air supply assembly 15 is communicated with the combustion cavity through an air outlet of the combustion-supporting air supply assembly 15;
the combustion-supporting wind pressure control system is provided with a detection end and a controller, the detection end is used for detecting the air pressure value of combustion-supporting wind, and the controller is used for controlling the on-off of the gas inlet assembly 14.
The technical effect of the scheme is as follows: through setting up combustion-supporting wind pressure control system, can detect the size of combustion-supporting wind pressure, when the numerical value of combustion-supporting wind pressure is not in the actual settlement within range, the detection end gives the controller with signal transmission this moment, and then the controller comes the switch of control gas subassembly 14 and closes, and the gas air feed is interrupted in the gas subassembly 14 this moment.
The detection end is a combustion-supporting wind pressure switch 16, the combustion-supporting wind pressure switch 16 feeds back the detected wind pressure value to the controller by an electric signal, and the controller controls the on-off of the gas inlet assembly 14 according to the feedback information of the electric signal.
As an embodiment of the present embodiment, the housing 11 is provided with a circulation air opening 17 on each side thereof, which is communicated with the accommodating chamber 12. The technical effect of the scheme is as follows: the flame of the combustion chamber can be conveniently sprayed out, and the full combustion of the fuel gas can be ensured.
Further, the combustion assembly 13 has an exhaust port 18 communicating with the combustion chamber, the exhaust port 18 facing a circulation tuyere 17.
As an implementation manner of the embodiment, a circulating wind pressure control system is disposed on the accommodating chamber 12, and the circulating wind pressure control system has a circulating wind pressure detecting end and a control unit, and the control unit is used for controlling the on/off of the gas intake assembly 14. The technical effect of the scheme is as follows: through the scope that detects circulation wind pressure to can indirectly obtain the carminative speed of combustion chamber and stability, when the actual value of circulation wind pressure is not in the setting value, cut off the gas and admit air, thereby can the troubleshooting, prevent dangerous emergence.
Wherein, the circulation wind pressure detection end is circulation wind pressure switch 19, and when circulation wind pressure switch 19 detects that the pressure value of circulation wind is not in the settlement scope, transmit the detection information to the control unit in the form of electrical signal, control the switch of gas subassembly 14 that admits air through the control unit. The conventional technology is to control the on-off of the equipment or the on-off of the electromagnetic valve in a mode of combining the pressure sensing element and the single chip microcomputer. The control unit in the scheme can adopt a single chip microcomputer.
As an embodiment of the present embodiment, the gas inlet assembly 14 includes a gas inlet pipe 20, and a double-cut electromagnetic valve 21 is disposed on the gas inlet pipe 20. The technical effect of the scheme is as follows: the setting of double-switch power-off solenoid valve 21 can cooperate combustion-supporting wind pressure control system and circulation wind pressure control system to use to can ensure closing in time of gas intake pipe 20, improve the safety in utilization of combustor.
Wherein, be provided with gas inlet ball valve 22, filter 23, gas pressure-regulating valve 24, gas low-pressure switch 25, two switching off solenoid valve 21, gas side leakage switch 26 and gas high-pressure switch 27 on the gas intake pipe 20 in proper order, this scheme is used for being that the atmospheric pressure in the gas intake pipe 20 flows more stably, and wherein gas side leakage switch 26 is used for preventing the incident that the gas leakage caused, and wherein, filter 23 is used for improving the clean degree of gas. The gas side leakage switch 26 is installed on the double-cut electromagnetic valve 21, and detects whether gas leakage exists or not through a sensitive element.
This scheme is still being equipped with the power supply subassembly of striking sparks, and the power supply subassembly of striking sparks includes ignition solenoid valve 28, adjusts ignition valve 29 and ignition transformer 30, and this three passes through the circuit and establishes ties, during the operation, opens ignition solenoid valve 28, and ignition transformer 30 controls the portion of striking sparks and discharges this moment, then adjusts ignition valve 29 and is used for controlling the voltage of ignition transformer 30 to the portion of striking sparks that makes can produce the electric spark of different intensity for improve the efficiency that the gas struck sparks.
The combustion-supporting air supply assembly 15 comprises a fan 31 and a wind shield 32, the fan 31 is installed on the shell 11, and the air outlet end of the fan 31 is communicated with the combustion cavity through the wind shield 32. The technical effect of the scheme is as follows: facilitating the full combustion of the combustion chamber.
The working principle of the scheme is as follows: and opening the combustion-supporting air supply assembly 15 and the gas inlet assembly 14, and burning the gas in the combustion cavity after the gas is ignited successfully.
The combustion-supporting wind pressure switch 16 monitors the combustion-supporting wind pressure condition, and when the wind pressure is not within the set value, the combustion-supporting fan is cut off, and the gas supply of the gas inlet component 14 is cut off by the double-cut electromagnetic valve 21; if the wind pressure is within the set value, the combustion is kept continuously.
When the circulating wind pressure switch 19 detects that the pressure value of the circulating wind is not in the set range, an alarm is generated, and the gas supply of the gas inlet assembly 14 is cut off through the double-cut electromagnetic valve 21; if the wind pressure is within the set value, the combustion is kept continuously.
It will be apparent to those skilled in the art that various changes and modifications can be made without departing from the inventive concept thereof, and these changes and modifications can be made without departing from the spirit and scope of the utility model.
Claims (8)
1. An integrated linear burner system, comprising:
the device comprises a shell (11), wherein an accommodating cavity (12) is formed in the shell (11);
the combustion assembly (13) is provided with a combustion cavity, a gas inlet assembly (14) is connected to the combustion cavity, and an ignition part is arranged in the combustion cavity;
the air outlet of the combustion-supporting air supply assembly (15) is communicated with the combustion cavity;
the combustion-supporting wind pressure control system, combustion-supporting wind pressure control system has a sense terminal and a controller, the sense terminal is used for detecting the atmospheric pressure value of combustion-supporting wind, the controller is used for controlling the switch that the gas admitted air subassembly (14).
2. The integrated linear burner system according to claim 1, characterized in that the housing (11) is provided on both sides with circulation tuyeres (17) respectively, which are in communication with the accommodation chamber (12).
3. The integrated linear burner system according to claim 2, wherein said combustion assembly (13) has an exhaust port (18) communicating with said combustion chamber, said exhaust port (18) facing one of said circulation tuyeres (17).
4. The integrated linear burner system according to claim 3, wherein a circulating wind pressure control system is provided on the receiving chamber (12), the circulating wind pressure control system having a circulating wind pressure detecting terminal and a control unit for controlling the on/off of the gas intake assembly (14).
5. The integrated linear burner system according to claim 4, wherein the gas inlet assembly (14) comprises a gas inlet pipe (20), and a double-shut solenoid valve (21) is provided on the gas inlet pipe (20).
6. The integrated linear burner system according to claim 5, wherein a filter (23) is provided on the gas inlet pipe (20).
7. The integrated linear burner system according to claim 5, characterized in that a gas high-pressure switch (27) and a gas low-pressure switch (25) are provided on the gas inlet pipe (20).
8. The integrated linear burner system according to claim 1, wherein the combustion air supply assembly (15) comprises a fan (31) and a hood (32), the fan (31) is mounted on the housing (11), and an air outlet end of the fan (31) is communicated with the combustion chamber through the hood (32).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122706011.XU CN216203311U (en) | 2021-11-05 | 2021-11-05 | Integrated linear combustor system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122706011.XU CN216203311U (en) | 2021-11-05 | 2021-11-05 | Integrated linear combustor system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216203311U true CN216203311U (en) | 2022-04-05 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122706011.XU Active CN216203311U (en) | 2021-11-05 | 2021-11-05 | Integrated linear combustor system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216203311U (en) |
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2021
- 2021-11-05 CN CN202122706011.XU patent/CN216203311U/en active Active
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