Early warning device for network engineering base station

Abstract

The early warning device for the network engineering base station comprises a machine body, supporting rods are installed at the two ends of the machine body, two limiting clamps are installed on the outer sides of the two supporting rods through screws, and a solar cell panel is rotatably installed above the supporting rod at the right end; and a light source detector is mounted above the solar cell panel through screws, the bottom of the light source detector is connected with a servo motor through a wire harness, and a mounting seat is welded and mounted above the supporting rod at the left end. According to the early warning device for the network engineering base station, the solar cell panel is rotatably mounted above the right end supporting rod through the transmission shaft, and the solar cell panel is inclined, so that energy generated by solar irradiation of the solar cell panel can be transmitted to the early warning device; and then, electric energy can be provided through the solar cell panel, so that energy consumption and waste are avoided, and the practicability of the early warning device is improved.

Description

Technical Field

[0001] The invention relates to the technical field of base station early warning, and in particular to an early warning device for a network engineering base station. Background Art

[0002] The network engineering base station is an important component of the network communication system, and is mainly responsible for the reception and transmission of wireless signals. The network engineering base station is composed of equipment such as the base station transceiver and the base station controller, which work together to complete wireless communication tasks. The base station transceiver is mainly responsible for the reception and transmission of wireless signals, which includes functions such as signal modulation and radio frequency processing. The base station controller is the interface between the base station transceiver and the mobile switching center. It is responsible for controlling and managing the services of the base station transceiver. In the network engineering base station, in addition to the hardware equipment, factors such as the location, coverage, signal interference and natural disasters of the base station also need to be considered, because these factors will affect the quality and stability of network communications, so early warning devices are needed to monitor and warn the base station when it is in use; In the "An Early Warning Device for Network Engineering Base Station" with the patent publication CN216116428U, a receiving device and a processing device are included. The receiving device includes a data acquisition template, a video monitoring device is installed on the upper left side of the data acquisition template, a temperature and humidity transmitter is installed on the lower left side of the data acquisition template, a wind sensor is installed on the upper right side of the data acquisition template, a smoke sensor is installed on the lower right side of the data acquisition template, a receiving unit is installed on the top of the data acquisition template, and a wireless transceiver module is installed on the top of the receiving unit; the processing device includes a central processing unit, the central processing unit is installed at the bottom of the data acquisition template, a network base station is installed at the bottom of the central processing unit, and a server module is installed on the upper part of the network base station. The early warning device for network engineering base stations has the advantages of comprehensive detection, rapid data analysis and transmission, accurate information, and convenient and fast; In the "An Early Warning Device for Network Engineering Base Station" with the patent CN216116428U, it includes a warehouse body, the bottom of which is movably mounted with the early warning device body, the interior of the warehouse body is provided with a clamping mechanism with one end fixedly connected to the early warning device body, the interior of the warehouse body is provided with a driving mechanism, and the early warning device body is provided with a cooling mechanism. The early warning device for network engineering base station sets the coolant temperature threshold through the controller, and adds coolant to the interior of the cooling box. The heat dissipation fins can introduce the heat inside the early warning device body into the coolant inside the cooling box to cool down and dissipate heat of the early warning device body. The temperature sensor uploads the coolant temperature inside the cooling box to the controller. When the controller detects that the uploaded temperature is high, it starts the semiconductor refrigeration sheet to cool the coolant inside the cooling box, so that the coolant is always kept at a suitable cooling temperature, achieving the purpose of good cooling and heat dissipation effect; The existing early warning device needs to use external power supply equipment to provide energy consumption for the early warning device during early warning monitoring. However, the early warning device is in operation 24 hours a day, and then monitors the relevant data inside the base station and uploads the information to the background management center. However, the amount of energy consumed is also very large, and there is no solar power supply equipment to provide energy for the early warning device, which is not convenient for the stable use of the early warning device in the later stage. Therefore, we propose an early warning device for network engineering base stations in order to solve the above-mentioned problems. Summary of the invention

[0003] The purpose of the present invention is to provide an early warning device for a network engineering base station to solve the problem raised in the above background technology that the existing early warning devices on the market need to use external power supply equipment to provide energy consumption for the early warning device when performing early warning monitoring, but the early warning device is in use 24 hours a day without interruption, and then monitors the relevant data inside the base station and uploads the information to the background management center, but the amount of energy consumed is also very large, and there is no solar power supply equipment to provide energy for the early warning device, which is not convenient for the stable use of the early warning device in the later stage.

[0004] To achieve the above object, the present invention provides the following technical solution: an early warning device for a network engineering base station, comprising a fuselage, support rods are installed at both ends of the fuselage, and two limit clamps are installed on the outer sides of the two support rods by screws, and a solar panel is rotatably installed above the support rod at the right end, and the solar panel is in an inclined shape; It also includes: a light source detector is installed on the top of the solar panel by screws, and the bottom of the light source detector is connected to a servo motor through a wiring harness, a mounting seat is welded and installed on the top of the left end of the support rod, and a connecting rod is installed through the internal slot of the mounting seat, and a fixing plate is screwed on the top of the connecting rod, and a field milling probe is screwed on the bottom slot of the fixing plate; A driving assembly is provided at the bottom of the solar panel, which can drive the driving assembly to drive the solar panel to flip and swing its position through meshing action. At this time, the solar panel can be driven to swing automatically following the movement of sunlight. Detection assemblies are provided on the outer sides of both ends of the fuselage, and the bolts connected by the limit clamps on both sides of the fuselage can be monitored for anti-loosening through the detection assembly to prevent the bolts from loosening and falling off due to shaking and vibration during later use, thereby improving the warning efficiency of the early warning device. Disassembly and assembly assemblies are provided inside the two mounting seats, and the disassembly and assembly assemblies can be used to quickly disassemble and assemble the connecting rod through meshing action, thereby facilitating the rapid replacement and maintenance of the field grinding probe in the later stage.

[0005] Preferably, the driving assembly includes a servo motor, a first worm and a second worm, wherein the servo motor is mounted on the outer wall of the right end support rod by screws, and the output end of the servo motor is connected to the first worm, and the outer side of the first worm is meshedly connected to the second worm through a bevel gear set, and the outer side of the second worm is meshedly connected to the first worm wheel, so that the second worm can be driven to rotate through the bevel gear set while the first worm rotates, thereby driving the second worm to drive the first worm wheel to rotate.

[0006] Preferably, the driving assembly also includes a first worm gear and a transmission shaft, wherein the first worm gear is rotatably installed above the right end support rod, and the internal groove of the first worm gear is penetrated by a transmission shaft, and the rear end of the transmission shaft is fixedly connected to a solar panel, so that the transmission shaft can be driven by the first worm gear to drive the solar panel to flip and swing in position while the first worm gear rotates, and the solar panel can be driven to flip and swing in position following the light source of sunlight.

[0007] Preferably, the left end of the first worm gear extends through and extends to the outside of the connecting rod, and the rear side of the left end of the first worm gear is meshedly connected with the second worm wheel, and the internal slot of the second worm wheel is connected with the connecting rod through and through, so that the connecting rod connected to the inner side of the second worm wheel can be driven to rotate while the first worm gear rotates, and then the field mill probe can be driven to rotate, and then the detection range of the field mill probe can be expanded, thereby improving the warning range of the warning device.

[0008] Preferably, the detection component includes a protective cover seat, wherein the two protective cover seats are snap-fitted and installed on the outer sides of both ends of the fuselage, and the two protective cover seats are internally connected to two limit clamps, and the two protective cover seats are internally grooved and penetrated by support rods. The detection component also includes a pressure sensor, wherein the two protective cover seats are internally grooved and pressure sensors are installed by screws, and the inner sides of the two pressure sensors are fit-connected to the outer sides of the bolts of the two limit clamps. The pressure sensor can be used to monitor the anti-loosening of the bolts on the outer sides of the limit clamps to prevent the bolts from loosening due to collision and vibration.

[0009] Preferably, the disassembly and assembly component includes a pressing rod, wherein the two pressing rods are slidably installed at the inner two ends of the mounting seat, and the two pressing rods are symmetrically arranged about the vertical center line of the mounting seat, and the inner sides of the two pressing rods are connected to the transmission gear through rack meshing, and the disassembly and assembly component also includes a transmission gear and a limit rod, wherein the two transmission gears are rotatably installed at the inner two ends of the mounting seat, and the outer sides of the two transmission gears are connected to the limit rod through rack meshing, and the two limit rods are slidably installed at the inner two ends of the mounting seat, and at the same time, the inner ends of the two limit rods are slidably connected with a slide groove, and the slide groove is opened on the bottom outer side of the connecting rod, so that the two transmission gears can be driven to drive the two limit rods to retract and move while pressing the two pressing rods, and the two limit rods can be separated from the slide groove, and then the connecting rod can be quickly disassembled and assembled, which saves time and effort.

[0010] Preferably, the disassembly and assembly component also includes a torsion spring, wherein the interiors of the two transmission gears are grooved with torsion springs, and the structures of the two torsion springs are identical, and the outer sides of the two torsion springs are connected to mounting seats, so that the two limit rods can be easily popped out into the sliding groove by the elastic force of the two torsion springs themselves, thereby preventing the connecting rod from rotating and falling off during the later rotation.

[0011] Compared with the prior art, the present invention has the following beneficial effects: (1) A solar panel is installed on the top of the right end support rod through a transmission shaft, and the solar panel is tilted. At this time, the energy generated by the sun can be transmitted to the early warning device through the solar panel, and then the solar panel can be used to provide electricity, thereby avoiding energy consumption and waste, and improving the practicality of the early warning device; (2) Furthermore, a light source detector is installed on the top of the solar panel by screws, and the irradiation angle of sunlight can be monitored by the light source detector. When the light source detector detects that the irradiation angle of sunlight has changed, the information will be transmitted to the servo motor through the wiring harness, so as to start and stop the servo motor, thereby facilitating the stable use of the later warning device; (3) Furthermore, a servo motor is installed by screws on the upper side of the right end support rod, and then a first worm is connected to the output end of the servo motor, and a second worm is meshedly connected to the outer side of the first worm through a bevel gear set. The servo motor can drive the first worm wheel meshedly connected to the outer side of the second worm to rotate while the servo motor rotates. At this time, the transmission shaft connected to the inner side of the first worm wheel can be driven to drive the solar panel to flip and swing. Then, the solar panel can be driven to flip and swing along with the rotation of the sun, so as to better provide energy for the early warning device. (4) By meshing and connecting the second worm wheel at the left end of the first worm gear, and then slotting the inner side of the second worm wheel and connecting the connecting rod through it, the field mill type probe installed above the connecting rod can be driven to rotate while the first worm gear rotates. In this case, the detection range of the field mill type probe can be expanded, thereby improving the warning efficiency of the warning device; (5) Slots are provided at both ends of the interior of the mounting seat to penetrate and slide through a pressing rod, and then the inner sides of the two pressing rods are connected to transmission gears through rack meshing, and the outer sides of the two transmission gears are connected to limit rods through rack meshing. When the two pressing rods are pressed, the two transmission gears can be driven to drive the two limit rods to retract and move at the same time, and then the mounting seat and the connecting rod can be quickly retracted and moved, and then the connecting rod can be quickly disassembled and separated, which is more convenient for the field mill probe to be quickly disassembled, replaced, repaired and used later. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Figure 1 It is a schematic diagram of the three-dimensional structure of the present invention; Figure 2 It is a schematic diagram of the partial three-dimensional structure of the fuselage and the support rod of the present invention; Figure 3 It is a schematic diagram of the local three-dimensional structure of the field milling probe of the present invention; Figure 4 It is a schematic diagram of the main cross-sectional structure of the present invention; Figure 5 It is a schematic diagram of the partial main cross-section structure of the fuselage and the protective cover seat of the present invention; Figure 6 For the present invention Figure 5 The enlarged structural diagram at A in the middle; Figure 7 It is a schematic diagram of the partial main cross-section structure of the solar cell panel and the connecting rod of the present invention; Figure 8 For the present invention Figure 7 The enlarged structural diagram at B in the middle; Fig. 9 It is a schematic diagram of the top cross-section structure of the mounting base and the field grinding probe of the present invention; Fig.10 For the present invention Fig. 9 Enlarged structural diagram at point C in the middle.

[0013] In the figure: 1. body; 2. support rod; 3. protective cover seat; 4. solar panel; 5. mounting seat; 6. connecting rod; 7. field mill probe; 8. light source detector; 9. alarm; 10. limit clamp; 11. servo motor; 12. first worm; 13. second worm; 14. first worm gear; 15. pressure sensor; 16. second worm gear; 17. bevel gear set; 18. pressing rod; 19. transmission gear; 20. limit rod; 21. rack; 22. torsion spring; 23. fixed plate; 24. transmission shaft; 25. slide groove. DETAILED DESCRIPTION

[0014] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0015] See also Figure 1-Figure 10 The present invention provides a technical solution: an early warning device for a network engineering base station, comprising a fuselage 1, a support rod 2, a protective cover seat 3, a solar panel 4, a mounting seat 5, a connecting rod 6, a field mill probe 7, a light source detector 8, an alarm 9, a limit clamp 10, a servo motor 11, a first worm 12, a second worm 13, a first worm gear 14, a pressure sensor 15, a second worm gear 16, a bevel gear set 17, a pressing rod 18, a transmission gear 19, a limit rod 20, a rack 21, a torsion spring 22, a fixed plate 23, a transmission shaft 24 and a slide groove 25; Embodiment 1:

[0016] The problem that the traditional early warning device needs external energy supply equipment to provide power is disclosed. The fuselage 1 has support rods 2 installed at both ends, and two limit clamps 10 are installed on the outer sides of the two support rods 2 by screws, and a solar panel 4 is rotatably installed above the right end support rod 2, and the solar panel 4 is in an inclined shape; It also includes: a light source detector 8 is installed on the top of the solar panel 4 by screws, and the bottom of the light source detector 8 is connected to a servo motor 11 through a harness, a mounting seat 5 is welded and installed on the top of the left end support rod 2, and a connecting rod 6 is installed through the internal slot of the mounting seat 5, and a fixing plate 23 is screwed on the top of the connecting rod 6, and a field mill probe 7 is screwed on the bottom slot of the fixing plate 23; A driving assembly is provided at the bottom of the solar panel 4, which can drive the driving assembly to drive the solar panel 4 to flip and swing its position through meshing. At this time, the solar panel 4 can be driven to swing automatically following the movement of sunlight. Detection assemblies are provided on the outer sides of both ends of the fuselage 1, and the bolts connected by the limit clamps 10 on both sides of the fuselage 1 can be monitored for anti-loosening through the detection assembly to prevent the bolts from loosening and falling off due to shaking and vibration during later use, thereby improving the warning efficiency of the early warning device. Disassembly and assembly assemblies are provided inside the two mounting seats 5, and the disassembly and assembly assemblies can be used to quickly disassemble and assemble the connecting rod 6 through meshing, thereby facilitating the rapid replacement and maintenance of the field grinding probe 7 in the later stage.

[0017] The driving assembly includes a servo motor 11, a first worm 12 and a second worm 13, wherein the servo motor 11 is installed on the outer wall of the right end support rod 2 by screws, and the output end of the servo motor 11 is connected to the first worm 12, and the outer side of the first worm 12 is meshedly connected to the second worm 13 through a bevel gear set 17, and the outer side of the second worm 13 is meshedly connected to the first worm wheel 14, and the driving assembly also includes the first worm wheel 14 and a transmission shaft 24, wherein the first worm wheel 14 is rotatably installed above the right end support rod 2, and the internal slot of the first worm wheel 14 is penetrated by the transmission shaft 24, and the rear end of the transmission shaft 24 is fixedly connected to the solar panel 4.

[0018] like Figure 1-Figure 8 As shown, when the early warning device performs early warning monitoring, the light source detector 8 is used to monitor the irradiation angle of sunlight. At this time, the light source detector 8 will transmit the information to the servo motor 11 through the wiring harness to control the servo motor 11 to start and stop. Then the servo motor 11 will drive the first worm 12 to drive the second worm 13 to rotate through the bevel gear set 17. At this time, the second worm 13 will drive the transmission shaft 24 connected to the inner side of the first worm wheel 14 to rotate, and then it can drive the solar panel 4 to flip and swing, and then it can drive the solar panel 4 to flip and swing following the rotation of the sun, so as to better provide energy for the early warning device.

[0019] Embodiment 2: Different from the first embodiment, the field milling probe 7 is driven to rotate while the first worm 12 rotates, which discloses: The left end of the first worm 12 extends through and extends to the outside of the connecting rod 6, and the rear side of the left end of the first worm 12 is meshedly connected with the second worm wheel 16, and the internal slot of the second worm wheel 16 is penetrated and connected with the connecting rod 6. When the first worm 12 rotates, the second worm wheel 16 meshedly connected on its left side will drive the connecting rod 6 connected to its inner side to rotate. At this time, the field mill probe 7 installed above the connecting rod 6 can be driven to rotate its position, and the monitoring range of the field mill probe 7 can be expanded, thereby improving the warning efficiency of the early warning device.

[0020] Embodiment three: Different from the second embodiment, in order to prevent the bolts from loosening and falling off when the early warning device is used, the following is disclosed: The detection component includes a protective sleeve seat 3, wherein the two protective sleeve seats 3 are snap-fitted and installed on the outer sides of both ends of the fuselage 1, and the interiors of the two protective sleeve seats 3 are connected to two limit clamps 10, and the interiors of the two protective sleeve seats 3 are slotted and penetrated with the support rod 2, and the detection component also includes a pressure sensor 15, wherein the interiors of the two protective sleeve seats 3 are slotted and the pressure sensor 15 is installed by screws, and the inner sides of the two pressure sensors 15 are fitted and connected to the outer sides of the bolts of the two limit clamps 10, such as Figure 1-Figure 6 As shown, when the early warning device shakes and vibrates due to external unstable factors during use, the two pressure sensors 15 arranged in the grooves on the inner sides of the two protective sleeve seats 3 will monitor the two bolts to prevent loosening. When the bolts loosen and fall off due to the shaking and vibration, the bolts fall off and squeeze and collide with the two pressure sensors 15. At this time, the two pressure sensors 15 will transmit the information to the two alarms 9 through the wiring harness and sound an alarm to remind nearby staff to deal with it in time, thereby improving the early warning efficiency of the early warning device.

[0021] Embodiment 4: Different from the third embodiment, the connecting rod 6 can be quickly disassembled, repaired and replaced, which discloses: The disassembly and assembly component includes a pressing rod 18, wherein the two pressing rods 18 are both slidably installed at the inner ends of the mounting seat 5, and the two pressing rods 18 are symmetrically arranged about the vertical center line of the mounting seat 5, and the inner sides of the two pressing rods 18 are meshed with a transmission gear 19 through a rack 21. The disassembly and assembly component also includes a transmission gear 19 and a limit rod 20, wherein the two transmission gears 19 are rotatably installed at the inner ends of the mounting seat 5, and the outer sides of the two transmission gears 19 are meshed with the limit rod 20 through the rack 21, and the two limit rods 20 are both slidably installed at the inner ends of the mounting seat 5, and at the same time, the inner ends of the two limit rods 20 are both slidably connected with a slide groove 25, and the slide groove 25 is opened on the outer side of the bottom of the connecting rod 6. The disassembly and assembly component also includes a torsion spring 22, wherein the inner sides of the two transmission gears 19 are slotted with a torsion spring 22, and the structures of the two torsion springs 22 are identical, and the outer sides of the two torsion springs 22 are connected to the mounting seat 5.

[0022] like Figure 1-10 As shown, when the field mill type probe 7 fails after long-term use and needs to be repaired and replaced, the two pressing rods 18 are pressed to drive the two transmission gears 19 to rotate through the rack 21. Because the outer sides of the two transmission gears 19 are meshed and connected with the limit rods 20 through the racks 21, the two limit rods 20 can be driven to shrink and move while pressing the two pressing rods 18. At this time, the connecting rod 6 can be separated from the mounting seat 5, and then the connecting rod 6 can be quickly disassembled and replaced, thereby facilitating the rapid repair and replacement of the field mill type probe 7. Finally, the elastic force of the two torsion springs 22 can be used to elastically reset the positions of the two rotating transmission gears 19, so that the two limit rods 20 can be ejected into the slide groove 25. At this time, the position of the installed connecting rod 6 can be slidably limited to avoid the phenomenon that the connecting rod 6 falls off while rotating in the later stage, thereby improving the warning efficiency of the early warning device, thereby completing a series of tasks.

[0023] Although the present invention has been described in detail with reference to the aforementioned embodiments, it is still possible for those skilled in the art to modify the technical solutions described in the aforementioned embodiments, or to make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. An early warning device for a network engineering base station, comprising a body (1), with support rods (2) installed at both ends, and two limit clamps (10) installed on the outer sides of the two support rods (2) by screws, and a solar panel (4) is rotatably installed above the right support rod (2), and the solar panel (4) is in an inclined shape; It is characterized in that Also includes: A light source detector (8) is installed on the top of the solar panel (4) by means of screws, and a servo motor (11) is connected to the bottom of the light source detector (8) by means of a wiring harness, a mounting seat (5) is welded and installed on the top of the left end support rod (2), a connecting rod (6) is installed through the internal slot of the mounting seat (5), a fixing plate (23) is screwed on the top of the connecting rod (6), and a field milling probe (7) is screwed on the bottom slot of the fixing plate (23); The bottom of the solar panel (4) is provided with a driving component, which can drive the driving component to drive the solar panel (4) to flip and swing through a meshing action, thereby driving the solar panel (4) to swing automatically following the movement of sunlight; Detection components are provided on the outer sides of both ends of the fuselage (1), and the detection components can be used to monitor the bolts connected to the limit clamps (10) on both sides of the fuselage (1) to prevent loosening, thereby preventing the bolts from loosening and falling off due to shaking and vibration during later use, thereby improving the warning efficiency of the warning device; The two mounting seats (5) are each provided with a disassembly assembly component, which can be used to quickly disassemble and assemble the connecting rod (6) through meshing, thereby facilitating the rapid replacement and maintenance of the field milling probe (7) at a later stage.

2. The early warning device for a network engineering base station according to claim 1, characterized in that: The drive assembly comprises a servo motor (11), a first worm (12) and a second worm (13), wherein the servo motor (11) is mounted on the outer side wall of the right end support rod (2) by means of screws, and the output end of the servo motor (11) is connected to the first worm (12), and the outer side of the first worm (12) is meshedly connected to the second worm (13) via a bevel gear set (17), and the outer side of the second worm (13) is meshedly connected to the first worm wheel (14).

3. The early warning device for a network engineering base station according to claim 2, characterized in that: The drive assembly further comprises a first worm gear (14) and a transmission shaft (24), wherein the first worm gear (14) is rotatably mounted above the right end support rod (2), and the transmission shaft (24) is installed through an internal slot of the first worm gear (14), and the rear end of the transmission shaft (24) is fixedly connected to the solar cell panel (4).

4. The early warning device for a network engineering base station according to claim 2, characterized in that: The left end of the first worm (12) extends through the outside of the connecting rod (6), and the rear side of the left end of the first worm (12) is meshedly connected with the second worm wheel (16), and the internal slot of the second worm wheel (16) is connected through the connecting rod (6).

5. The early warning device for a network engineering base station according to claim 1, characterized in that: The detection assembly comprises a protective sleeve seat (3), wherein the two protective sleeve seats (3) are both mounted on the outer sides of the two ends of the fuselage (1) in a snap-fitting manner, and the interiors of the two protective sleeve seats (3) are both connected to two limit clamps (10), and the interiors of the two protective sleeve seats (3) are both slotted and penetrated by support rods (2).

6. The early warning device for a network engineering base station according to claim 5, characterized in that: The detection assembly further comprises a pressure sensor (15), wherein the interiors of the two protective sleeve seats (3) are both slotted and the pressure sensors (15) are mounted via screws, and the inner sides of the two pressure sensors (15) are both fitted and connected to the outer sides of the bolts of the two limit clamps (10).

7. The early warning device for a network engineering base station according to claim 1, characterized in that: The disassembly assembly comprises a pressing rod (18), wherein the two pressing rods (18) are both slidably mounted at both ends of the interior of the mounting seat (5), and the two pressing rods (18) are symmetrically arranged about the vertical center line of the mounting seat (5), and the inner sides of the two pressing rods (18) are meshedly connected to the transmission gear (19) via a rack (21).

8. The early warning device for a network engineering base station according to claim 1, characterized in that: The disassembly assembly also includes a transmission gear (19) and a limit rod (20), wherein the two transmission gears (19) are rotatably mounted at both ends of the interior of the mounting seat (5), and the outer sides of the two transmission gears (19) are meshedly connected to the limit rod (20) through racks (21), and the two limit rods (20) are slidably mounted on both ends of the interior of the mounting seat (5), and the inner ends of the two limit rods (20) are slidably connected to a slide groove (25), and the slide groove (25) is opened on the outer side of the bottom of the connecting rod (6).

9. The early warning device for a network engineering base station according to claim 8, characterized in that: The disassembly and assembly assembly further comprises a torsion spring (22), wherein the interiors of the two transmission gears (19) are both grooved with torsion springs (22), the two torsion springs (22) have the same structure, and the outer sides of the two torsion springs (22) are both connected to a mounting seat (5).

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