Real-time monitoring and analyzing equipment for spaceflight gasifier

Abstract

The utility model relates to the technical field of spaceflight gasifiers, and discloses a spaceflight gasifier real-time monitoring and analyzing device which comprises a furnace body, a fixing pipe is fixedly connected to the middle of the left side of the front face of the furnace body, a connecting mechanism is arranged on the front face of the fixing pipe, and the connecting mechanism comprises a first threaded groove. The first threaded groove is formed in the edge of the front face of the fixing pipe, a first threaded pipe is arranged outside the front face of the fixing pipe, a fixing cylinder is fixedly connected to the front face of the first threaded pipe, and a second threaded groove is formed in the front face of the fixing cylinder. The first threaded groove is formed in the front face of the fixing pipe, the first threaded pipe can be screwed into the first threaded groove, the fixing barrel can be in threaded connection with the fixing pipe through the first threaded pipe, the sealing disc can be in threaded connection with the fixing barrel through the second threaded pipe, and the front face of the fixing barrel is sealed; therefore, an effect of conveniently and quickly disassembling and assembling the monitoring equipment by an operator can be achieved.

Description

Technical Field

[0001] The utility model relates to the technical field of aerospace gasifiers, and particularly relates to a real-time monitoring and analysis device for aerospace gasifiers. Background Technique

[0002] An aerospace gasifier is a gasification device specifically used in the aerospace field, mainly used to convert solid or liquid fuels into high-temperature and high-pressure gases. Such gases can be used as propellants or for power generation and other purposes. With the continuous improvement of environmental protection requirements, the coal chemical industry is facing increasing pressure. At the same time, changes in the coal market have also brought great challenges to coal chemical enterprises. Therefore, carrying out research on the influence of coal types and pulverized coal moisture content on the operation technology of aerospace gasifiers can not only improve the production efficiency and product quality of enterprises, but also reduce the energy consumption and pollutant emissions of enterprises.

[0003] However, the monitoring means during the operation of traditional gasifiers are single, and it is rather troublesome for operators to disassemble and assemble them, which affects the monitoring efficiency. Content of the Utility Model

[0004] (1) Technical Problems to be Solved

[0005] Aiming at the deficiencies of the prior art, the utility model provides a real-time monitoring and analysis device for aerospace gasifiers, which has the advantages of facilitating operators to quickly disassemble and assemble the monitoring equipment, etc., and solves the problems mentioned in the above background technique.

[0006] (2) Technical Solutions

[0007] To achieve the above object, the utility model provides the following technical solution: A real-time monitoring and analysis device for aerospace gasifiers, including a furnace body. In the middle of the left side of the front of the furnace body, a fixed pipe is fixedly connected. A connection mechanism is arranged on the front of the fixed pipe. The connection mechanism includes a first thread groove, which is opened at the edge of the front of the fixed pipe. A first threaded pipe is arranged outside the front of the fixed pipe. A fixed cylinder is fixedly connected to the front of the first threaded pipe. A second thread groove is opened on the front of the fixed cylinder. A second threaded pipe is arranged outside the front of the second thread groove. A sealing disc is fixedly connected to the front of the second threaded pipe. A through hole is opened in the middle of the front of the sealing disc. A rubber disc is arranged outside the front of the through hole. A number of monitoring mechanisms are arranged inside the fixed cylinder.

[0008] Preferably, a placement plate is fixedly connected to the middle of the lower part of the front of the furnace body.

[0009] Preferably, a control device is fixedly installed on the upper surface of the placement plate.

[0010] The back of the placement plate is vertically connected to the lower part of the front of the furnace body and is used for installing control equipment, which is used to control the operation of temperature sensors, pressure sensors, and gas sensors.

[0011] Preferably, the monitoring mechanism includes fixed rods, and the number of the fixed rods is three. One ends of the three fixed rods are evenly connected to the middle part of the inner wall of the fixed cylinder.

[0012] Preferably, the other ends of the fixed rods are fixedly connected with placement tubes.

[0013] Preferably, a threaded rod is arranged in the middle of one side of the placement tube.

[0014] Preferably, one end of the threaded rod is fixedly connected with an extrusion disc.

[0015] One ends of the three fixed rods are evenly and vertically connected to the middle part of the inner wall of the fixed cylinder, and the other ends are vertically connected to the middle part of the outer surface of the placement tube. The inside is used to place temperature sensors, pressure sensors, and gas sensors. The threaded rod penetrates through the middle of one side of the placement tube and can perform threaded rotational movement inside it. Rotating the threaded rod drives the extrusion disc to move, and the temperature sensors, pressure sensors, and gas sensors are squeezed and fixed.

[0016] Preferably, temperature sensors, pressure sensors, and gas sensors are respectively arranged inside the three placement tubes.

[0017] The temperature sensor measures the temperature at different positions inside the gasifier in real time and converts the temperature signal into an electrical signal. The pressure sensor measures the pressure change inside the gasifier and converts the pressure signal into a processable electrical signal. The gas sensor is used to detect the chemical composition and concentration of the gas inside the gasifier.

[0018] Compared with the prior art, the present utility model provides a real-time monitoring and analysis device for an aerospace gasifier, having the following beneficial effects:

[0019] 1. Through the first thread groove opened on the front of the fixed tube in the present utility model, the first threaded tube can be screwed into the inside of the first thread groove. The fixed cylinder can be threadedly connected to the fixed tube through the first threaded tube, and the sealing disc can be threadedly connected to the fixed cylinder through the second threaded tube, sealing the front of the fixed cylinder, so as to achieve the effect of facilitating the operator to quickly disassemble and assemble the monitoring equipment.

[0020] 2. In the utility model, through the fixing rod connected to the inner wall of the fixing cylinder, the inside of the placing tube is hollow and used for placing a temperature sensor, a pressure sensor and a gas sensor. The threaded rod penetrates through the middle of one side of the fixing cylinder and can perform threaded rotational movement inside it. Rotating the threaded rod drives the extrusion disc to move, squeezing and fixing the temperature sensor, the pressure sensor and the gas sensor, so as to simplify the structure of the device and reduce the installation space. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 is a schematic diagram of the overall structure of the utility model;

[0022] Figure 2 is a schematic diagram of the structure of the connection mechanism of the utility model;

[0023] Figure 3 is a schematic diagram of the internal structure of the connection mechanism of the utility model;

[0024] Figure 4 is a front view schematic diagram of the monitoring mechanism of the utility model.

[0025] Wherein: 1. Furnace body; 101. Placing plate; 102. Control equipment; 103. Fixed tube; 2. Connection mechanism; 201. First thread groove; 202. First threaded tube; 203. Fixing cylinder; 204. Second thread groove; 205. Second threaded tube; 206. Sealing disc; 207. Through hole; 208. Rubber disc; 3. Monitoring mechanism; 301. Fixing rod; 302. Placing tube; 303. Threaded rod; 304. Extrusion disc; 305. Temperature sensor; 306. Pressure sensor; 307. Gas sensor. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0026] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0027] Please refer to Figures 1-4, A real-time monitoring and analysis device for an aerospace gasifier, including a furnace body 1. In the middle of the left side of the front of the furnace body 1, a fixed pipe 103 is fixedly connected. A connecting mechanism 2 is arranged on the front of the fixed pipe 103. The connecting mechanism 2 includes a first thread groove 201, which is opened at the front edge of the fixed pipe 103. A first threaded pipe 202 is arranged outside the front of the fixed pipe 103. The front of the so-called first threaded pipe 202 is fixedly connected with a fixed cylinder 203. A second thread groove 204 is opened on the front of the fixed cylinder 203. A second threaded pipe 205 is arranged outside the front of the second thread groove 204. The front of the second threaded pipe 205 is fixedly connected with a sealing disc 206. A through hole 207 is opened in the middle of the front of the sealing disc 206. A rubber disc 208 is arranged outside the front of the through hole 207. A number of monitoring mechanisms 3 are arranged inside the fixed cylinder 203. The fixed pipe 103 communicates with the furnace body 1; the first thread groove 201 is fitted at the front edge of the fixed pipe 103. The first threaded pipe 202 can be screwed into the inside of the first thread groove 201. The fixed cylinder 203 can be threadedly connected with the fixed pipe 103 through the first threaded pipe 202. The second thread groove 204 is fitted at the front edge of the fixed cylinder 203. The second threaded pipe 205 can be screwed into the inside of the second thread groove 204. The sealing disc 206 can be threadedly connected with the fixed cylinder 203 through the second threaded pipe 205 to seal the front of the fixed cylinder 203. The through hole 207 penetrates through the middle of the front of the sealing disc 206 to facilitate the passage of wires. The rubber disc 208 can be attached to the middle of the front of the sealing disc 206 to seal the through hole 207 and ensure the sealing performance of the fixed cylinder 203.

[0028] Specifically, as Figure 1 shown, a placement plate 101 is fixedly connected to the middle of the lower part of the front of the furnace body 1. A control device 102 is fixedly installed on the upper surface of the placement plate 101.

[0029] Through the above technical solution, the back of the placement plate 101 is vertically connected to the lower part of the front of the furnace body 1 for installing the control device 102. The control device 102 is used to control the operation of the temperature sensor 305, the pressure sensor 306 and the gas sensor 307.

[0030] Specifically, as Figure 3 and Figure 4 shown, the monitoring mechanism 3 includes fixed rods 301. The number of fixed rods 301 is three. One ends of the three fixed rods 301 are evenly connected to the middle of the inner wall of the fixed cylinder 203. The other ends of the fixed rods 301 are fixedly connected with a placement pipe 302. A threaded rod 303 is arranged in the middle of one side of the placement pipe 302. One end of the threaded rod 303 is fixedly connected with an extrusion disc 304.

[0031] Through the above technical solution, one end of the three fixing rods 301 is vertically and evenly connected to the middle part of the inner wall of the fixing cylinder 203, and the other end is vertically connected to the middle part of the outer surface of the placing tube 302. The inside thereof is used to place the temperature sensor 305, the pressure sensor 306 and the gas sensor 307. The threaded rod 303 penetrates through the middle part of one side of the placing tube 302 and can perform threaded rotational movement inside it. By rotating the threaded rod 303, the pressing disc 304 is driven to move, and the temperature sensor 305, the pressure sensor 306 and the gas sensor 307 are pressed and fixed.

[0032] Specifically, as Figure 3 shown, the temperature sensor 305, the pressure sensor 306 and the gas sensor 307 are respectively arranged inside the three placing tubes 302.

[0033] Through the above technical solution, the temperature sensor 305 measures the temperature at different positions inside the gasifier in real time and converts the temperature signal into an electrical signal. The pressure sensor 306 measures the pressure change inside the gasifier and converts the pressure signal into a processable electrical signal. The gas sensor 307 is used to detect the chemical composition and concentration of the gas inside the gasifier.

[0034] During use, the operator screws the first threaded tube 202 on the back of the fixing cylinder 203 into the inside of the first threaded groove 201 to connect the fixing cylinder 203 with the fixing tube 103. Subsequently, the temperature sensor 305, the pressure sensor 306 and the gas sensor 307 are respectively placed inside the three placing tubes 302. The threaded rod 303 is rotated, and the temperature sensor 305, the pressure sensor 306 and the gas sensor 307 are clamped and fixed by the pressing disc 304. Finally, the second threaded tube 205 on the back of the sealing disc 206 is screwed into the inside of the second threaded groove 204 to seal the front of the fixing cylinder 203.

[0035] Although the embodiments of the present invention have been shown and described, it will be understood by those of ordinary skill in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principle and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A real-time monitoring and analysis device for an aerospace gasifier, comprising a furnace body (1), characterized in that: In the middle of the left side of the front of the furnace body (1), a fixed pipe (103) is fixedly connected. A connecting mechanism (2) is arranged on the front of the fixed pipe (103). The connecting mechanism (2) includes a first thread groove (201), and the first thread groove (201) is opened at the front edge of the fixed pipe (103). A first threaded pipe (202) is arranged outside the front of the fixed pipe (103). The front of the first threaded pipe (202) is fixedly connected with a fixed cylinder (203). A second thread groove (204) is opened on the front of the fixed cylinder (203). A second threaded pipe (205) is arranged outside the front of the second thread groove (204). The front of the second threaded pipe (205) is fixedly connected with a sealing disc (206). A through hole (207) is opened in the middle of the front of the sealing disc (206). A rubber disc (208) is arranged outside the front of the through hole (207). A number of monitoring mechanisms (3) are arranged inside the fixed cylinder (203).

2. The real-time monitoring and analysis device for an aerospace gasifier according to claim 1, wherein: In the middle of the lower part of the front of the furnace body (1), a placing plate (101) is fixedly connected.

3. The real-time monitoring and analysis device for an aerospace gasifier according to claim 2, wherein: A control device (102) is fixedly installed on the upper surface of the placing plate (101).

4. The real-time monitoring and analysis device for an aerospace gasifier according to claim 1, characterized in that: The monitoring mechanism (3) includes fixed rods (301). The number of the fixed rods (301) is three. One ends of the three fixed rods (301) are evenly connected to the middle of the inner wall of the fixed cylinder (203).

5. The real-time monitoring and analysis device for an aerospace gasifier according to claim 4, wherein: The other ends of the fixed rods (301) are fixedly connected with placing pipes (302).

6. The real-time monitoring and analysis device for an aerospace gasifier according to claim 5, characterized in that: A threaded rod (303) is arranged in the middle of one side of the placing pipe (302).

7. An on-orbit gasifier real-time monitoring and analysis device according to claim 6, characterized in that: One end of the threaded rod (303) is fixedly connected with an extrusion disc (304).

8. The real-time monitoring and analysis device for an aerospace gasifier according to claim 5, characterized in that: A temperature sensor (305), a pressure sensor (306) and a gas sensor (307) are respectively arranged inside the three placing pipes (302).

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