Integrated special vehicle equipment system for monitoring, commanding and operating meteorological data

Abstract

The invention relates to the technical field of integrated special vehicle equipment, in particular to an integrated special vehicle equipment system for monitoring, commanding and operating meteorological data. The device comprises a second-class chassis, a square cabin is installed at the upper end of the second-class chassis, a vehicle-mounted air conditioner is installed at the upper end of the square cabin, an installation area is arranged at the upper end of the square cabin, a lodging mechanism and a radar are arranged on the inner wall of the installation area, and an installation area, an operation area, a power generation area and a loading area are arranged on the inner wall of the square cabin. The problems that when a rocket projectile is launched, a launching rack and a trolley platform need to be installed and fixed, when the launching rack is installed, a plurality of installing holes in the launching rack and installing holes in the trolley platform need to be horizontally and vertically aligned, then screws are screwed into the installing holes for fixing, and the installing holes are misplaced possibly in the screw screwing process, so that the launching rack is damaged are solved. And therefore, the problem that the launcher is relatively tedious to mount and fix due to the fact that the mounting hole needs to be aligned again and then the screw rod is screwed in is solved.

Description

Technical Field

[0001] The present invention relates to the technical field of integrated special vehicle equipment, and in particular to an integrated special vehicle equipment system for meteorological data monitoring, command and operation. Background Art

[0002] In recent years, my country's artificial weather modification work has developed rapidly, and its operational capabilities and management levels have been continuously improved. It has played an important role in serving agricultural production, supporting disaster prevention, mitigation and relief, helping to build an ecological civilization and ensuring major events. In order to further promote the development of artificial weather modification, it is necessary to further improve the basic business capabilities such as meteorological monitoring capabilities, operational capabilities and command capabilities in the field of artificial weather modification. All parts of the country have carried out research on artificial weather modification technology systems based on their own conditions, and established comprehensive technical systems of varying degrees and designs. By using integrated special vehicle equipment, good decision-making technical support and mobile operation capabilities can be achieved, and the level of artificial weather modification can be improved. The integrated special vehicle equipment is mainly composed of an environmental monitoring subsystem, a rocket operation subsystem, a communication transmission subsystem, The system consists of six subsystems: software integration subsystem, comprehensive support subsystem, and vehicle-mounted platform subsystem. When using integrated special vehicle equipment, the environmental monitoring subsystem uses radar, precipitation phenomenon instrument and intelligent weather station to collect meteorological data; the rocket operation subsystem can implement artificial hail prevention and rain enhancement operations and provide ammunition support services; the communication transmission subsystem provides the system with all-weather communication capabilities, ensures information transmission and command communication between modules, and reports the operation parameters, effects, videos, etc. to the superior command agency after the operation; the software integration subsystem is the support for the realization of the entire system function. Through the secondary processing of meteorological data, the monitoring data is visualized, and data analysis and decision-making assistance services are provided at the same time. According to the superior's instructions, the operation plan and operation deployment are completed, and the operation effect is evaluated after the operation is completed. The comprehensive support subsystem is the guarantee of the system operation, providing the system with auxiliary functions such as power, video monitoring, lighting and security. The vehicle-mounted platform subsystem is an important carrier of the system, providing the system with space, mobility, basic support and other conditions, and then improving the decision-making technical support and mobile operation capabilities through multiple subsystems, so as to improve the level of artificial weather influence.

[0003] The inventor found in his daily work that when the integrated special vehicle equipment is in use, since when launching rockets, it is necessary to install and fix the launcher and the trolley platform. When installing the launcher, it is necessary to align the multiple mounting holes on the launcher with the mounting holes on the trolley platform horizontally and vertically and then screw in the screws to fix them. Since the mounting holes may be misaligned in the process of screwing the screws, it is necessary to realign the mounting holes and then screw in the screws, which makes the installation and fixation of the launcher more cumbersome. Summary of the invention

[0004] The purpose of the present invention is to solve the problem that in actual use, when launching a rocket, the launcher and the trolley platform need to be installed and fixed. When installing the launcher, multiple mounting holes on the launcher need to be horizontally and vertically aligned with the mounting holes on the trolley platform and then screwed in to fix them. Since the mounting holes may be misaligned in the process of screwing the screws, it is necessary to realign the mounting holes and then screw in the screws, which leads to the problem of cumbersome installation and fixation of the launcher. An integrated special vehicle equipment system for meteorological data monitoring, command and operation is proposed.

[0005] In order to achieve the above-mentioned objectives, the present invention adopts the following technical scheme: an integrated special vehicle equipment system for meteorological data monitoring, command and operation, comprising a second-class chassis, a cabin is installed at the upper end of the second-class chassis, a vehicle-mounted air conditioner is installed at the upper end of the cabin, an installation area is provided at the upper end of the cabin, a lodging mechanism and a radar are provided on the inner wall of the installation area, an installation area, an operation area, a power generation area and a loading area are provided on the inner wall of the cabin, a cabinet is installed on the inner wall of the cabinet, a vehicle-mounted computer is installed on the inner wall of the cabinet, an electric telescopic rod is installed at the bottom of the inner wall of the installation area, a six-element weather station and a precipitation phenomenon meter are provided on the top of the electric telescopic rod, an in-cabin camera is installed on the top of the inner wall of the operation area, a display is installed on the side of the operation area away from the electric telescopic rod, the vehicle-mounted air conditioner acts on the operation area, and the six-element weather station and the precipitation phenomenon meter are controlled by the electric telescopic rod. The retracted rod is raised to the outside of the cabin for detection, a generator is installed on one side of the inner wall of the power generation area, an electric lifting tail plate is installed on the left end of the square cabin, and the electric lifting tail plate is connected to the square cabin by screws and welding, and baffles are fixedly connected at both ends of the bottom of the inner wall of the loading area, a trolley platform and an ammunition transfer box are provided on the inner wall of the loading area, the trolley platform slides between the two baffles, a detachable launching rack is provided at the upper end of the trolley platform, a pre-fixing component is provided between the launching rack and the trolley platform, a leveling leg is provided at the lower end of the second type chassis, a lighting lamp is installed at the upper end of the square cabin, a mounting component is provided between the electric telescopic rod and the square cabin, the pre-fixing component includes a limit pin sliding on the inner wall of the mounting hole of the launching rack, and the limit pin slides on the inner wall of the mounting hole on the trolley platform, and a circular plate is provided on the side of the trolley platform away from the launching rack, and the circular plate is fixed to the limit pin.

[0006] The effect achieved by the above-mentioned components is: by setting up a pre-fixing component, when it is necessary to install and fix the launch frame to the trolley platform, the mounting hole on the launch frame is inserted into the limit pin in the mounting hole on the trolley platform, thereby limiting the launch frame, and then inserting the screw rod so that it presses downward against the limit pin, and at the same time, the screw rod is turned to fix it with the mounting hole threads on the trolley platform and the launch frame. Under the limitation of other limit pins, the mounting hole is prevented from being misaligned, thereby avoiding the effect of misalignment of the mounting hole during the process of turning the screw rod as much as possible.

[0007] Preferably, an operating panel is fixedly connected to one side of the trolley platform close to the circular plate, and the limit latch is slidably inserted into the operating panel.

[0008] The effect achieved by the above components is that the limit latch moves downward so as to be inserted into the operation panel, thereby limiting the position of the limit latch.

[0009] Preferably, a spring is sleeved on the arc surface of the limit latch, one end of the spring is fixed to the circular plate, and the other end of the spring is fixed to the operating plate.

[0010] The effect achieved by the above components is: by arranging the spring and the operating plate, after the screw rod is screwed out, the spring drives the limit latch to reset.

[0011] Preferably, a positioning groove is provided on the arc surface of the limit latch, and a circular latch is slidably inserted into the left end of the operating panel.

[0012] The effect achieved by the above components is: dragging the circular latch and inserting it into the positioning groove, thereby limiting the position of the limit latch.

[0013] Preferably, the size and shape of the circular latch are matched with the size and shape of the inner wall of the positioning groove, and the inner wall of the positioning groove is provided with a plurality of evenly distributed protrusions.

[0014] The effect achieved by the above-mentioned components is: by setting the protrusion, the circular latch is dragged and inserted into the positioning groove, so that the circular latch is limited in the positioning groove.

[0015] Preferably, the mounting assembly comprises an arc block 1 and an arc block 2 which are arranged on the arc surface of the electric telescopic rod, the arc block 1 and the arc block 2 are rotatably connected to each other, the circle enclosed by the arc block 1 and the arc block 2 is adapted to the arc surface of the electric telescopic rod, the arc surface of the arc block 2 is fixedly connected to a connecting rod, and the connecting rod is detachably connected to the cabin.

[0016] The effect achieved by the above components is: when installing the electric telescopic rod, rotate the arc block one, and then fit the electric telescopic rod with the arc block two, then rotate the arc block one to fit the electric telescopic rod, and then fix the arc block one and the arc block two through the fixing mechanism, and limit the electric telescopic rod under the limit of the connecting rod, so that the worker can fix the electric telescopic rod.

[0017] Preferably, the upper end of the arc-shaped block 2 is fixedly connected with a rectangular plate, and a positioning pin is slidably inserted into the upper end of the rectangular plate.

[0018] The effect achieved by the above components is: dragging the positioning pins to insert them into the rectangular plate and the arc plate 2, thereby fixing the arc block 1 and the arc block 2.

[0019] Preferably, the positioning pins are slidably inserted into the arc block 1, and the arc block 1 and the arc block 2 are respectively provided with two.

[0020] The effect achieved by the above components is: by providing two arc blocks 1 and arc block 2 and a connecting rod, the electric telescopic rod is further limited.

[0021] In summary, the beneficial effects of the present invention are: In the present invention, a pre-fixing component is provided, and when it is necessary to install and fix the launch rack to the trolley platform, the mounting hole on the launch rack is inserted into the limit pin in the mounting hole on the trolley platform, so as to limit the launch rack, and then the screw is inserted so as to press downward against the limit pin, and at the same time, the screw is turned to be threaded and fixed with the mounting holes on the trolley platform and the launch rack, and under the limitation of other limit pins, the mounting holes are placed in a misaligned position, thereby avoiding the misalignment of the mounting holes in the process of turning the screw as much as possible, solving the problem that when launching a rocket, the launch rack and the trolley platform need to be installed and fixed, and when installing the launch rack, multiple mounting holes on the launch rack need to be horizontally and vertically aligned with the mounting holes on the trolley platform and then the screws are screwed in for fixation, and since the mounting holes may be misaligned in the process of turning the screws, it is necessary to realign the mounting holes and then screw in the screws, which leads to the problem that the installation and fixation of the launch rack is relatively cumbersome. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] 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 three-dimensional structure of the back side of the present invention; Figure 3 It is a schematic diagram of the three-dimensional structure of the electric lifting tailgate of the present invention; Figure 4 It is a schematic diagram of the three-dimensional structure of the cross section of the present invention; Figure 5 It is a schematic diagram of the three-dimensional structure of the pre-fixing assembly of the present invention; Figure 6 It is a three-dimensional structural schematic diagram of the cross section of the installation component of the present invention.

[0023] Legend: 1. Second-class chassis; 2. Pre-fixed components; 3. Installation components; 4. Shelter; 5. On-board air conditioner; 6. Radar; 7. Electric lifting tail plate; 8. Trolley platform; 9. Lighting; 10. Leveling legs; 11. Baffle; 12. Launcher; 13. Ammunition transfer box; 14. Lodging mechanism; 15. Generator; 16. Installation area; 17. Electric telescopic rod; 18. Six-element weather station; 19. Precipitation phenomenon meter; 20. Display; 21. Limit latch; 22. Spring; 23. Round plate; 24. Operating panel; 25. Positioning slot; 26. Round latch; 31. Arc block one; 32. Arc block two; 33. Connecting rod; 34. Rectangular plate; 35. Positioning pin. DETAILED DESCRIPTION

[0024] Reference Figures 1 to 4 As shown, the present invention provides a technical solution: an integrated special vehicle equipment system for meteorological data monitoring, command and operation includes a second-class chassis 1, a cabin 4 is installed on the upper end of the second-class chassis 1, a vehicle-mounted air conditioner 5 is installed on the upper end of the cabin 4, an installation area is provided on the upper end of the cabin 4, a lodging mechanism 14 and a radar 6 are provided on the inner wall of the installation area, an installation area 16, an operation area, a power generation area and a loading area are provided on the inner wall of the cabin 4, a cabinet is installed on the inner wall of the installation area 16, a vehicle-mounted computer is installed on the inner wall of the cabinet, an electric telescopic rod 17 is installed on the bottom of the inner wall of the installation area 16, a six-element meteorological station 18 and a precipitation phenomenon meter 19 are provided on the top of the electric telescopic rod 17, an in-cabin camera is installed on the top of the inner wall of the operation area, and a display 2 is installed on the side of the operation area away from the electric telescopic rod 17 0, the vehicle air conditioner 5 acts in the operation area, the six-element weather station 18 and the precipitation phenomenon meter 19 are raised to the outside of the cabin for detection by means of the electric telescopic rod 17, a generator 15 is installed on one side of the inner wall of the power generation area, an electric lifting tail plate 7 is installed at the left end of the square cabin 4, and the electric lifting tail plate 7 is connected to the square cabin 4 by screws and welding, baffles 11 are fixedly connected at both ends of the bottom of the inner wall of the loading area, a trolley platform 8 and an ammunition transfer box 13 are arranged on the inner wall of the loading area, the trolley platform 8 slides between the two baffles 11, a detachable launching frame 12 is arranged at the upper end of the trolley platform 8, a pre-fixed component 2 is arranged between the launching frame 12 and the trolley platform 8, a leveling leg 10 is arranged at the lower end of the second-class chassis 1, a lighting lamp 9 is installed at the upper end of the square cabin 4, and a mounting component 3 is arranged between the electric telescopic rod 17 and the square cabin 4.

[0025] The specific settings and functions of the pre-fixing component 2 and the installation component 3 are described in detail below.

[0026] Reference Figure 5As shown, in this embodiment: the pre-fixing component 2 includes a limit pin 21 that slides on the inner wall of the mounting hole of the launch frame 12, and the limit pin 21 slides on the inner wall of the mounting hole on the trolley platform 8. A circular plate 23 is provided on the side of the trolley platform 8 away from the launch frame 12, and the circular plate 23 and the limit pin 21 are fixed. By setting the pre-fixing component 2, when it is necessary to install and fix the launch frame 12 to the trolley platform 8, the mounting hole on the launch frame 12 is inserted into the limit pin 21 in the mounting hole on the trolley platform 8, so as to limit the launch frame 12, and then the screw is inserted so that it presses against the limit pin 21 downward, and at the same time, the screw is screwed to be fixed with the trolley platform 8 and the mounting holes on the launch frame 12. Under the limitation of other limit pins 21, the mounting holes are placed in misalignment, thereby avoiding the effect of misalignment of the mounting holes during the screw rotation process as much as possible. The side of the trolley platform 8 close to the circular plate 23 is fixedly connected with an operating plate 24, and the limit pin 2 1 is slidably inserted into the operating plate 24, and the limit latch 21 moves downward so as to be inserted into the operating plate 24, thereby limiting the limit latch 21. The arc surface of the limit latch 21 is sleeved with a spring 22, and one end of the spring 22 is fixed to the circular plate 23. By setting the spring 22 and the operating plate 24, after the screw is screwed out, the spring 22 drives the limit latch 21 to reset, and the other end of the spring 22 is fixed to the operating plate 24. A positioning groove 25 is opened on the arc surface of the limit latch 21, and a circular latch 26 is slidably inserted at the left end of the operating plate 24. The circular latch 26 is dragged and inserted into the positioning groove 25, thereby limiting the limit latch 21. The size and shape of the circular latch 26 are adapted to the size and shape of the inner wall of the positioning groove 25. The inner wall of the positioning groove 25 is provided with a plurality of evenly distributed protrusions. By setting the protrusions, the circular latch 26 is dragged and inserted into the positioning groove 25, so that the circular latch 26 is limited to the positioning groove 25.

[0027] Reference Figure 6As shown, in this embodiment: the installation component 3 includes an arc block 1 31 and an arc block 2 32 arranged on the arc surface of the electric telescopic rod 17, and the arc block 1 31 and the arc block 2 32 are rotatably connected. The circle surrounded by the arc block 1 31 and the arc block 2 32 is adapted to the arc surface of the electric telescopic rod 17, and the arc surface of the arc block 2 32 is fixedly connected with a connecting rod 33, and the connecting rod 33 is detachably connected to the cabin 4. When installing the electric telescopic rod 17, the arc block 1 31 is rotated, and then the electric telescopic rod 17 is fitted with the arc block 2 32, and then the arc block 1 31 is rotated to fit with the electric telescopic rod 17, and then the arc block 1 31 and the arc block 2 32 are fixedly connected to the arc surface of the electric telescopic rod 17 by the fixing mechanism. The arc block 2 32 is fixed, and the electric telescopic rod 17 is limited under the limit of the connecting rod 33, so that the worker can fix the electric telescopic rod 17. The upper end of the arc block 2 32 is fixedly connected with a rectangular plate 34, and a positioning pin 35 is slidably inserted into the upper end of the rectangular plate 34. The positioning pin 35 is dragged to be inserted into the rectangular plate 34 and the arc plate 2 to fix the arc block 1 31 and the arc block 2 32. The positioning pin 35 is slidably inserted into the arc block 1 31. There are two arc blocks 1 31 and two arc blocks 2 32 respectively. By setting two arc blocks 1 31 and arc blocks 2 32 and a connecting rod 33, the electric telescopic rod 17 is further limited.

[0028] Working principle: When using the integrated special vehicle equipment, it is driven to the designated location, the second-class chassis 1 is used as the bearing platform of the square cabin 4, the balance is adjusted by four leveling legs 10, and the six-element weather station 18 and the precipitation phenomenon instrument 19 are lifted out of the square cabin 4 by the electric telescopic rod 17. Through the joint action of the radar 6, the lodging mechanism 14, the six-element weather station 18 and the precipitation phenomenon instrument 19, the changes of the air and ground meteorological parameters before, during and after the operation can be obtained locally and quickly in real time in the target intervention area, such as the position, intensity, average Doppler velocity and velocity spectrum width and polarization parameters of the weather target, the vertical profile distribution parameters of the cloud and rain intensity, speed, spectrum width, wind speed, wind direction, raindrop spectrum, rainfall rate, liquid water content, etc., and the on-board computer in the cabinet can be used to obtain the weather real-time data in pairs. The system uses Doppler weather radar 6 data to monitor and identify possible severe convection and rainstorm clouds within the scanning range of radar 6, calculates and extracts the strongest reflectivity factor, the strongest echo top height, the vertical liquid water content density, the vertical liquid water content jump value and other human shadow operation index criteria, combines numerical forecast products to realize the potential forecast of human shadow operation, converts the identified area into a human shadow operation shot point, calculates the operation parameters, and compares and evaluates the effects before and after the operation. The staff can operate by observing the display 20, the power supply of the equipment can be guaranteed by the generator 15, and the communication with the upper The electric lifting tail plate 7 is fixedly connected to the rear frame of the cabin 4 by bolts and welding, and the tail plate can be flipped and lifted. The trolley platform 8 can be transferred between the inside of the cabin 4 and the ground through the electric lifting tail plate 7. The ammunition in the ammunition transfer box 13 is installed on the launch rack 12 for launching. The working environment of the staff is guaranteed by the vehicle-mounted air conditioner 5, and the lighting lamp 9 provides brightness for night operations. When it is necessary to install and fix the launch rack 12 to the trolley platform 8, the mounting hole on the launch rack 12 is inserted into the limit pin 21 in the mounting hole on the trolley platform 8, so as to limit the launch rack 12, and then the screw is inserted so that it is pressed against the limit pin 21 downward, and the screw is turned to make the launch rack 12 move downward. It is threadedly fixed with the mounting holes on the trolley platform 8 and the launching frame 12. Under the limitation of other limiting pins 21, the mounting hole is prevented from being misaligned, thereby avoiding the effect of misalignment of the mounting hole during the screwing process as much as possible. The limiting pin 21 moves downward so that it is inserted into the operating plate 24, thereby limiting the limiting pin 21. By setting a spring 22, an operating plate 24 and a circular plate 23, after the screw is screwed out, the spring 22 drives the limiting pin 21 to reset, drags the circular pin 26, and inserts it into the positioning groove 25, thereby limiting the limiting pin 21. By setting a protrusion, the circular pin 26 is dragged and inserted into the positioning groove 25, so that the circular pin 26 is limited to the positioning groove 25. When installing the electric telescopic rod 17, the arc block 1 31 is rotated.Then the electric telescopic rod 17 is fitted with the arc block 2 32, and then the arc block 1 31 is rotated to fit with the electric telescopic rod 17, and then the arc block 1 31 and the arc block 2 32 are fixed by the fixing mechanism, and the electric telescopic rod 17 is limited under the limit of the connecting rod 33, so that the worker can fix the electric telescopic rod 17. When installing the electric telescopic rod 17, the arc block 1 31 is rotated, and then the electric telescopic rod 17 is fitted with the arc block 2 32, and then the arc block 1 31 is rotated. 1, so that it fits with the electric telescopic rod 17, and then drag the positioning pin 35 to insert it into the rectangular plate 34 and the arc plate 2, fix the arc block 1 31 and the arc block 2 32, fix the arc block 1 31 and the arc block 2 32, and limit the electric telescopic rod 17 under the limit of the connecting rod 33, so that the worker can fix the electric telescopic rod 17. By setting two arc blocks 1 31 and arc block 2 32 and the connecting rod 33, the electric telescopic rod 17 is further limited.

[0029] The above is only a preferred embodiment of the present invention, and is not intended to limit the present invention in other forms. Any technician familiar with the profession may use the above disclosed technical content to change or modify it into an equivalent embodiment with equivalent changes and apply it to other fields. However, any simple modification, equivalent change and modification made to the above embodiment based on the technical essence of the present invention without departing from the technical solution of the present invention still belongs to the protection scope of the technical solution of the present invention. In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installation", "connection" and "connection" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal connection of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

Claims

1. An integrated special vehicle equipment system for meteorological data monitoring, command and operation, comprising a second-class chassis (1), characterized in that: A cabin (4) is installed at the upper end of the second-class chassis (1), an on-board air conditioner (5) is installed at the upper end of the cabin (4), an installation area is provided at the upper end of the cabin (4), a lodging mechanism (14) and a radar (6) are provided on the inner wall of the installation area, an installation area (16), an operation area, a power generation area and a loading area are provided on the inner wall of the cabin (4), a cabinet is installed on the inner wall of the installation area (16), an on-board computer is installed on the inner wall of the cabinet, an electric telescopic rod (17) is installed at the bottom of the inner wall of the installation area (16), a six-element weather station (18) and a precipitation phenomenon meter (19) are provided on the top of the electric telescopic rod (17), an in-cabin camera is installed on the top of the inner wall of the operation area, a display (20) is installed on the side of the operation area away from the electric telescopic rod (17), the on-board air conditioner (5) acts on the operation area, the six-element weather station (18) and the precipitation phenomenon meter (19) are installed on the inner wall of the operation area, and the on-board air conditioner (5) acts on the operation area. 19) is lifted to the outside of the cabin for detection by means of an electric telescopic rod (17); a generator (15) is installed on one side of the inner wall of the power generation area; an electric lifting tail plate (7) is installed at the left end of the cabin (4); the electric lifting tail plate (7) is connected to the cabin (4) by means of screws and welding; baffles (11) are fixedly connected at both ends of the bottom of the inner wall of the loading area; a trolley platform (8) and an ammunition transfer box (13) are arranged on the inner wall of the loading area; the trolley platform (8) slides between the two baffles (11); a detachable launch rack (12) is arranged at the upper end of the trolley platform (8); a pre-fixing component (2) is arranged between the launch rack (12) and the trolley platform (8); a leveling leg (10) is arranged at the lower end of the second-class chassis (1); a lighting lamp (9) is installed at the upper end of the cabin (4); and a mounting component (3) is arranged between the electric telescopic rod (17) and the cabin (4).

2. The integrated special vehicle equipment system for meteorological data monitoring, command and operation according to claim 1 is characterized in that: An operating plate (24) is fixedly connected to one side of the trolley platform (8) close to the circular plate (23), and the limit latch (21) is slidably inserted into the operating plate (24).

3. The integrated special vehicle equipment system for meteorological data monitoring, command and operation according to claim 2 is characterized in that: A spring (22) is sleeved on the arc surface of the limit latch (21); one end of the spring (22) is fixed to a circular plate (23), and the other end of the spring (22) is fixed to an operating plate (24).

4. The integrated special vehicle equipment system for meteorological data monitoring, command and operation according to claim 3 is characterized by: The arc surface of the limit latch (21) is provided with a positioning groove (25), and the left end of the operating panel (24) is slidably provided with a circular latch (26).

5. The integrated special vehicle equipment system for meteorological data monitoring, command and operation according to claim 4 is characterized in that: The size and shape of the circular latch (26) match the size and shape of the inner wall of the positioning groove (25), and the inner wall of the positioning groove (25) is provided with a plurality of evenly distributed protrusions.

6. The integrated special vehicle equipment system for meteorological data monitoring, command and operation according to claim 5 is characterized in that: The mounting assembly (3) comprises an arc block 1 (31) and an arc block 2 (32) arranged on the arc surface of the electric telescopic rod (17); the arc block 1 (31) and the arc block 2 (32) are rotatably connected to each other; the circle enclosed by the arc block 1 (31) and the arc block 2 (32) is compatible with the arc surface of the electric telescopic rod (17); the arc surface of the arc block 2 (32) is fixedly connected to a connecting rod (33); and the connecting rod (33) is detachably connected to the cabin (4).

7. The integrated special vehicle equipment system for meteorological data monitoring, command and operation according to claim 6 is characterized by: The upper end of the arc-shaped block 2 (32) is fixedly connected to a rectangular plate (34), and the upper end of the rectangular plate (34) is slidably inserted with a positioning pin (35).

8. The integrated special vehicle equipment system for meteorological data monitoring, command and operation according to claim 7 is characterized in that: The positioning pin (35) is slidably inserted into the arc block one (31), and two arc blocks one (31) and two arc blocks two (32) are respectively provided.

9. The integrated special vehicle equipment system for meteorological data monitoring, command and operation according to claim 8 is characterized in that: The pre-fixing assembly (2) comprises a limit pin (21) which slides on the inner wall of the mounting hole of the launch frame (12), and the limit pin (21) slides on the inner wall of the mounting hole on the trolley platform (8).

10. The integrated special vehicle equipment system for meteorological data monitoring, command and operation according to claim 9, characterized in that: A circular plate (23) is provided on one side of the trolley platform (8) away from the launching frame (12), and the circular plate (23) is fixed to the limiting latch (21).

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