Mobile shelter for weather modification operations

Abstract

A kind of weather modification operation mobile shelter, including self-propelled vehicle, vehicle-mounted shelter is installed on the self-propelled vehicle, the slide rail is transversely arranged in the bottom of the inside of vehicle-mounted shelter, the rotary adjusting mechanism is equipped on the slide rail, the launcher is equipped on the rotary adjusting mechanism, multiple sleeve groups are installed in the inside of the launcher, auxiliary guide mechanism is also arranged in multiple sleeve groups, the inside of vehicle-mounted shelter is also equipped with launching mechanism, the inside of vehicle-mounted shelter is also provided with monitoring system, monitoring system is also respectively connected with rotary adjusting mechanism, auxiliary guide mechanism and launching mechanism signal.The present application realizes the automatic material taking, positioning, filling and launching preparation of rocket projectile by the cooperative operation of feeding groove, launching mechanism, auxiliary guide mechanism and rotary adjusting mechanism, without manual intervention in whole process, secondly, rotary adjusting mechanism can automatically adjust the horizontal position, rotation angle and pitch angle of launcher according to monitoring system, adapt to multi-cycle, high frequency operation demand.

Description

Technical Field

[0001] This invention relates to the field of meteorological monitoring, and in particular to a mobile container for artificial weather modification operations. Background Technology

[0002] Weather modification refers to the use of scientific and technological means to artificially intervene in the physical processes of the local atmosphere under appropriate conditions in order to increase precipitation, suppress hail, reduce rain and snow, and disperse fog and haze. Its core is to change the microphysical structure of clouds by seeding them with catalysts or causing physical disturbances, thereby regulating the development of precipitation or severe weather.

[0003] Current mobile weather modification cabins are mainly mounted on transport vehicles, typically with the cabin mounted on the vehicle's frame. The cabin contains rocket launchers and various meteorological measurement modules. Manual loading of rockets into the cabin is a common but significantly flawed method. While this method is low-cost, it lags behind in terms of safety, efficiency, and environmental adaptability. Rockets are flammable and explosive hazardous materials, and the traditional loading process involves manual handling and loading. Loading a single rocket manually takes 1-2 minutes, and loading multiple launchers takes even longer, easily missing the optimal catalytic window, such as strong convective clouds. Furthermore, after each launch, the cabin must be reopened and manually replenished, making it difficult to achieve multiple, high-frequency, and precise interventions. Additionally, forcibly loading rockets during thunderstorms, strong winds, or low temperatures increases the risk of operational errors due to slippage or poor visibility. Summary of the Invention

[0004] To address the aforementioned problems, the present invention employs the following technical solution:

[0005] A mobile weather modification container includes a self-propelled vehicle (WPV) with a vehicle-mounted container mounted on it. A horizontally arranged slide rail is installed at the bottom of the vehicle-mounted container's interior. A rotation adjustment mechanism is mounted on the slide rail, and a launcher is mounted on the rotation adjustment mechanism. Multiple sleeve assemblies are installed inside the launcher. Each sleeve assembly includes a first sleeve plate and a second sleeve plate, with a space between the first and second sleeve plates for placing rockets to be launched. An auxiliary guiding mechanism is also provided between the multiple sleeve assemblies, and each side of the auxiliary guiding mechanism is equipped with a retaining ring located inside the corresponding first and second sleeve plates. A feeding trough is also provided on one side of the vehicle-mounted container, extending partially into the container. A delivery mechanism is also installed inside the vehicle-mounted container, located at the conveying end of the feeding trough and above the launcher. A monitoring system is also installed inside the vehicle-mounted container to monitor the external meteorological environment. The monitoring system is also signal-connected to the rotation adjustment mechanism, the auxiliary guiding mechanism, and the delivery mechanism.

[0006] Preferably, the rotation adjustment mechanism includes a base, which is slidably mounted on a slide rail. A rotating plate is rotatably mounted on the upper part of the base, and a support frame is fixedly mounted on the rotating plate. Lifting electric cylinders are symmetrically arranged on the upper part of the support frame. The top of each lifting electric cylinder is movably connected to the launcher. Connecting arms are rotatably arranged on both sides of the launcher, and the other end of each connecting arm is movably connected to one side of the support frame.

[0007] Preferably, arc-shaped grooves are formed on the opposite sides of the first and second sets of plates, and a trigger is also provided at the rear end of the transmitter, which is also connected to the monitoring system signal.

[0008] Preferably, the auxiliary guiding mechanism includes a guide plate with a hollow interior and a strip-shaped guide groove on each side. A lead screw motor is also installed inside the guide plate and is fixedly connected to the lead screw. A movable plate is also installed on the lead screw and is located inside the guide plate. Sliding arms are fixedly connected to both sides of the movable plate. The sliding arms pass through the corresponding guide grooves, and a retaining ring is fixed at the far end of each sliding arm. A through hole is opened in the middle of the retaining ring.

[0009] Preferably, the conveying end of the feeding trough is also equipped with a rotating shaft, and a servo motor is fixedly installed on one side of the feeding trough. The servo motor is also connected to the rotating shaft. Multiple flow stabilizers are fixed at intervals on the rotating shaft. Each flow stabilizer is arc-shaped and has a stationary part and a segmented part.

[0010] Preferably, the delivery mechanism includes multiple symmetrically arranged mounting plates, one end of each mounting plate is fixed to the inner wall of the vehicle-mounted container, and guide columns are vertically installed between the upper and lower distributed mounting plates. A lifting seat is movably mounted between two guide columns, and a delivery column is movably mounted on the lifting seat. A first clamping plate and a second clamping plate are movably installed at the bottom of the delivery column, and the delivery column is also movably installed with a linkage mechanism.

[0011] Preferably, the lifting seat is further provided with a transverse guide groove, and a sliding column is installed in the transverse guide groove. The sliding column is also vertically connected to the delivery column. An adjustment seat is movably installed at the bottom of the delivery column. A traction plate is also provided on the adjustment seat. An angle adjustment electric cylinder is also movably installed on the delivery column. The telescopic end of the angle adjustment electric cylinder is also movably connected to the traction plate. A clamping electric cylinder is provided below the adjustment seat. The telescopic ends on both sides of the clamping electric cylinder are fixedly connected to the corresponding first clamping plate and second clamping plate through arc-shaped rods.

[0012] Preferably, the linkage mechanism includes a first connecting plate and a second connecting plate, both of which are fixedly installed on the top of the vehicle-mounted container. A rotating seat is movably installed on one side of the bottom of the first connecting plate, and a first connecting arm and a second connecting arm are fixedly installed on the rotating seat. A straight slot is formed on the first connecting arm, and the top of the delivery column extends into the straight slot. One end of the second connecting arm is movably connected to a hinge rod, and the other end of the hinge rod is movably connected to a swing arm. The swing arm is movably installed on the bottom of the second connecting plate and is also connected to the output end of the drive motor.

[0013] Preferably, the first connecting arm and the second connecting arm are fixedly mounted on the rotating seat in an alternating manner, and the length of the first connecting plate is greater than that of the second connecting plate, and the first connecting plate is also arranged in an alternating manner with the second connecting plate.

[0014] Preferably, the vehicle-mounted container has a window on its top, and two telescopic top plates are movably mounted on both sides of the window. An inspection door is also installed on the vehicle-mounted container via hinges. A rocket storage box is also fixedly installed on one side of the vehicle-mounted container, and the storage box is located below the feeding chute.

[0015] The beneficial effects of this invention are as follows: First, this invention achieves automatic material handling, positioning, loading, and launch preparation of rockets through the coordinated operation of the feeding trough, delivery mechanism, auxiliary guiding mechanism, and rotation adjustment mechanism. The entire process requires no manual intervention and can achieve continuous and orderly loading of multiple rockets, significantly shortening the operation preparation time and adapting to the needs of multi-round, high-frequency operations.

[0016] Secondly, the rotation adjustment mechanism can automatically adjust the horizontal position, rotation angle and pitch angle of the launcher based on meteorological data (such as wind direction and cloud height) obtained by the monitoring system, ensuring that the launch trajectory is accurately aligned with the target cloud layer. In addition, the lifting cylinder and connecting arm structure enable stable tilt adjustment of the launcher to adapt to the launch angle requirements of different operating scenarios. Attached Figure Description

[0017] Figure 1 This is a three-dimensional structural diagram of the present invention; Figure 2 This is a schematic diagram of the rear view structure of the present invention; Figure 3 for Figure 2 Enlarged structural diagram of section C; Figure 4 This is a top view of the structure of the present invention; Figure 5 for Figure 4 A three-dimensional structural diagram showing the cross-section along line AA. Figure 6 for Figure 5Enlarged structural diagram of section D in the middle; Figure 7 for Figure 4 A three-dimensional structural diagram of the cross-section along line BB; Figure 8 for Figure 7 Enlarged structural diagram of section E; In the diagram: 1. Self-propelled vehicle; 2. Vehicle-mounted container; 3. Slide rail; 4. Rotation adjustment mechanism; 5. Launcher; 6. Sleeve assembly; 60. First sleeve plate; 61. Second sleeve plate; 7. Auxiliary guide mechanism; 8. Retaining ring; 9. Feeding chute; 10. Dispensing mechanism; 11. Monitoring system; 40. Base; 41. Rotating plate; 42. Support frame; 43. Lifting cylinder; 44. Connecting arm; 45. Arc groove; 12. Trigger; 70. Guide plate; 71. Guide groove; 72. Lead screw motor; 73. Lead screw; 74. Moving plate; 75. Sliding arm; 76. Through hole; 13. Rotating shaft; 14. Servo motor; 15. Flow stabilizer plate; 15. Stationary part; 151. Dividing part; 152. Mounting plate. 101. Guide column; 102. Lifting seat; 103. Dispensing column; 104. First clamping plate; 105. Second clamping plate; 106. Linkage mechanism; 107. Transverse guide groove; 16. Sliding column; 17. Adjusting seat; 18. Traction plate; 19. Angle adjustment electric cylinder; 20. Clamping electric cylinder; 21. Arc rod; 22. First connecting plate; 1070. Second connecting plate; 1071. Rotating seat; 1072. First connecting arm; 1073. Second connecting arm; 1074. Straight slot; 23. Hinge rod; 1075. Swing arm; 1076. Drive motor; 1077. Window; 24. Telescopic top plate; 25. Inspection door; 26. Storage box; 27. Detailed Implementation

[0018] To make the objectives, technical solutions, and advantages of this invention clearer, the invention will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative and not intended to limit the invention.

[0019] In the description of this invention, it should be understood that the terms "length," "width," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this invention. In the description of this invention, "a plurality of" means two or more, unless otherwise explicitly specified.

[0020] Example 1: See appendix Figure 1-8A mobile weather modification container includes a self-propelled vehicle 1, which is a traditional transport vehicle and mainly serves to move the vehicle-mounted container 2. The vehicle-mounted container 2 is installed on the self-propelled vehicle 1. A horizontal slide rail 3 is arranged at the bottom of the interior of the vehicle-mounted container 2. A rotation adjustment mechanism 4 is installed on the slide rail 3. The rotation adjustment mechanism 4 can move left and right on the slide rail 3. Generally, during operation, the bottom of the rotation adjustment mechanism 4 is fixed, such as by screws or self-locking, to prevent the launcher 5 from moving left and right during the launch of rockets. The position and height of the launcher 5 can be automatically adjusted by the rotation adjustment mechanism 4. The launcher 5 is installed on the rotation adjustment mechanism 4. Multiple sleeve assemblies 6 are installed inside the launcher 5. Group 6 is mainly used for guiding and fixing rockets during launch. Each sleeve group 6 includes a first sleeve plate 60 and a second sleeve plate 61. The rocket to be launched is placed between the first sleeve plate 60 and the second sleeve plate 61. An auxiliary guiding mechanism 7 is also provided between multiple sleeve groups 6, and each side of the auxiliary guiding mechanism 7 is equipped with a retaining ring 8, which is located between the corresponding first sleeve plate 60 and second sleeve plate 61. The auxiliary guiding mechanism 7 is mainly to prevent the bottom of the rocket from abnormally contacting the trigger 12 due to gravity or other factors during the loading process, which could lead to safety hazards. Secondly, the auxiliary guiding mechanism 7 allows for slow and stable loading. The rocket given in Embodiment 1... The rocket loading process involves simultaneously lowering all rockets to their designated positions after they have reached them. A feeding trough 9 is located on one side of the vehicle-mounted container 2, holding the rockets to be launched. Before being placed in the feeding trough 9, the ignition contacts of the rockets need to be polished and cleaned. The ignition contacts are typically coated with an insulating film, such as paint. This film is removed before deployment to ensure electrical contact between the launcher 5 and the trigger 12, thus achieving ignition. The feeding trough 9 extends partially into the vehicle-mounted container 2. The container 2 also houses a deployment mechanism 10, which is used to gradually clamp and move the rockets from the feeding trough 9 to their designated positions, i.e., to each sleeve assembly. At the front end of 6, the delivery mechanism 10 is located at the conveying end of the feeding trough 9 and above the launcher 5. The vehicle-mounted container 2 is also equipped with a monitoring system 11. The monitoring system 11 includes various meteorological element measurement modules. The monitoring system 11 is mainly used to monitor the current external meteorological environment and, based on environmental factors such as cloud base height, wind direction and speed (ground and upper altitude), cloud top height / cloud thickness, precipitation intensity / radar echo, etc., the monitoring system 11 is also connected to the rotation adjustment mechanism 4, the auxiliary guidance mechanism 7 and the delivery mechanism 10. Then, based on the monitored meteorological parameters, the system controls the entire system to complete the automatic loading, position and angle adjustment of the rocket, so that the entire process can be completed without relying on manual labor, with a high degree of automation.

[0021] See Figure 2 and Figure 5 The rotating adjustment mechanism 4 includes a base 40, which is slidably mounted on a slide rail 3. The entire rotating adjustment mechanism 4 can move left and right on the slide rail 3. A rotating plate 41 is rotatably mounted on the upper part of the base 40. A rotating motor is installed inside the base 40, and the output end of the rotating motor is fixedly connected to the bottom of the rotating plate 41. When the position needs to be adjusted, the rotating motor is activated, which causes the rotating plate 41 to rotate, thereby adjusting the position of the launcher 5 as a whole. A support frame 42 is fixedly mounted on the rotating plate 41. A lifting electric cylinder 43 is symmetrically arranged on the upper part of the support frame 42. The top of each lifting electric cylinder 43 is movably connected to the launcher 5. Connecting arms 44 are rotatably mounted on both sides of the launcher 5, and the other end of each connecting arm 44 is movably connected to one side of the support frame 42. The launcher 5 can also be angled so that the front end of the launcher 5 is aligned with the window 24. When adjusting the tilt angle, only the lifting cylinder 43 needs to be controlled. During the raising and lowering process of the extension end of the lifting cylinder 43, the launcher 5 will tilt at a certain angle. The connecting arms 44 mainly play the role of fixing and rotating connection. Through the above technical solution, under the command of the monitoring system 11, the position and angle of the launcher 5 can be automatically adjusted, completely replacing manual adjustment, which is faster and more convenient.

[0022] See Figure 5 and Figure 8 The first sleeve plate 60 and the second sleeve plate 61 each have an arc-shaped groove 45 on their opposite sides. Each sleeve group 6 is composed of the first sleeve plate 60 and the second sleeve plate 61 arranged vertically, and the opposite sides have an arc-shaped groove 45. The arc-shaped groove 45 serves as a guide. The rear end of the launcher 5 is also equipped with a trigger 12. When all the rockets to be launched reach the designated position under the action of the auxiliary guide mechanism 7, that is, when the bottom of all the rockets contacts the trigger end of the trigger 12, the monitoring system 11 sends a trigger command. The trigger 12 receives the command and causes the bottom of each rocket to receive the sending command, thereby launching the rockets into the clouds to artificially influence the weather. The trigger 12 is also connected to the monitoring system 11.

[0023] See Figure 2 and Figure 8The auxiliary guiding mechanism 7 includes a guide plate 70, which has a hollow internal structure. The guide plate 70 primarily serves as a guide rail for the movable plate 74, allowing the movable plate 74 to move within it. Each side of the guide plate 70 has a strip-shaped guide groove 71, through which a sliding arm 75, fixedly connected to the movable plate 74 on each side, passes. During the movement of the movable plate 74, the distal end of the sliding arm 75 drives a retaining ring 8 to move between the first set of plates 60 and the second set of plates 61. The retaining ring 8 supports the bottom of the rocket and, during movement, smoothly transports the rocket to the launch position. The guide plate 70 is also equipped with a lead screw. The motor 72 is fixedly connected to the lead screw 73. The lead screw 73 is also equipped with a movable plate 74. The forward and reverse rotation of the lead screw motor 72 will cause the lead screw 73 to rotate forward or in reverse. Since the movable plate 74 is threadedly connected to the lead screw 73, the rotation of the lead screw 73 will cause the movable plate 74 to rise and fall. The movable plate 74 is located inside the guide plate 70, and the two sides of the movable plate 74 are also fixedly connected to the sliding arms 75. The sliding arms 75 pass through the corresponding guide grooves 71, and the far end of each sliding arm 75 is fixed with a retaining ring 8. The retaining ring 8 has a through hole 76 in the middle. The through hole 76 in the middle of the retaining ring 8 is to facilitate the contact between the bottom of the rocket and the trigger end of the trigger 12.

[0024] See Figure 3 and Figure 5 The feeding trough 9 is mainly used for conveying rockets. A rotating shaft 13 is also mounted on the conveying end of the feeding trough 9. For stable and orderly conveying, a servo motor 14 is fixedly installed on one side of the feeding trough 9. After the servo motor 14 is started, it causes the rotating shaft 13 to rotate. When the rotating shaft 13 rotates, it synchronously causes the flow stabilizer plate 15 on it to rotate. Figure 5 As shown, at this time, the front end of the flow stabilizer 15 is in the raised position, so the stationary part 151 of the flow stabilizer 15 will contact the rocket. At this time, the rocket is stationary, and the segmented part 152 of the flow stabilizer 15 will be at the bottom between the two rockets. When the rotating shaft 13 rotates, the delivery mechanism 10 also moves closer. When the first clamping plate 105 and the second clamping plate 106 clamp the rocket, the rotating shaft 13 continues to rotate, causing the segmented part 152 to rise from the bottom, thereby preventing the next rocket from being launched. As the rocket falls off, it effectively blocks the next rocket. When the delivery mechanism 10 picks it up again, the rotating shaft 13 will rotate in the opposite direction, causing the next rocket to return to the stationary part 151 of the flow stabilizer plate 15. This process is repeated continuously until all rockets are loaded into the designated position. The servo motor 14 is also connected to the rotating shaft 13. Multiple flow stabilizers 15 are fixed at intervals on the rotating shaft 13. Each flow stabilizer 15 is arc-shaped and has a stationary part 151 and a dividing part 152.

[0025] See Figure 3 and Figure 6 The delivery mechanism 10 includes a plurality of symmetrically arranged mounting plates 101. One end of each mounting plate 101 is fixed to the inner wall of the vehicle-mounted container 2. Guide columns 102 are vertically installed between the vertically distributed mounting plates 101. A lifting seat 103 is movably mounted between two guide columns 102. A delivery column 104 is movably mounted on the lifting seat 103. A first clamping plate 105 and a second clamping plate 106 are movably mounted at the bottom of the delivery column 104. The delivery column 104 is also movably mounted with a linkage mechanism 107, which mainly plays a driving role. The linkage mechanism 107 controls the first clamping plate 105 and the second clamping plate 106 to clamp the rocket and move and lift it.

[0026] See appendix Figure 6 The lifting seat 103 is also provided with a transverse guide groove 16, and a sliding column 17 is installed in the transverse guide groove 16. The sliding column 17 is also vertically connected to the launch column 104. An adjusting seat 18 is also movably installed at the bottom of the launch column 104. A traction plate 19 is also provided on the adjusting seat 18. An angle adjusting electric cylinder 20 is also movably installed on the launch column 104. The main function of the angle adjusting electric cylinder 20 is to adjust the angle when the rocket is launched. The telescopic end of the angle adjusting electric cylinder 20 is also movably connected to the traction plate 19. A clamping electric cylinder 21 is provided below the adjusting seat 18. When the clamping electric cylinder 21 is activated, it will cause the first clamping plate 105 and the second clamping plate 106 to move closer or further apart. The telescopic ends on both sides of the clamping electric cylinder 21 are fixedly connected to the corresponding first clamping plate 105 and second clamping plate 106 through arc rods 22.

[0027] See appendix Figure 3 and Figure 6 The linkage mechanism 107 includes a first connecting plate 1070 and a second connecting plate 1071. Both the first connecting plate 1070 and the second connecting plate 1071 are fixedly installed on the top of the interior of the vehicle-mounted container 2. A rotating seat 1072 is movably installed on one side of the bottom of the first connecting plate 1070. A first connecting arm 1073 and a second connecting arm 1074 are fixedly installed on the rotating seat 1072. A straight slot 23 is opened on the first connecting arm 1073. The top of the delivery column 104 extends into the straight slot 23. One end of the second connecting arm 1074 is movably connected to a hinge rod 1075. The other end of the hinge rod 1075 is movably connected to a swing arm 1076. The swing arm 1076 is movably installed on the bottom of the second connecting plate 1071. The swing arm 1076 is also connected to the output end of the drive motor 1077.

[0028] Through the above technical solution, the automatic and uninterrupted transfer of rockets can be realized under the action of the linkage mechanism 107. During the release, in order to adapt to the tilt angle of the launcher 5, the angle adjustment cylinder 20 can make the adjustment seat 18 tilt relative to the release column 104. The tilt range is determined by the length of the telescopic end of the angle adjustment cylinder 20. In this way, loading can be carried out quickly to adapt to the launch angle of the launcher 5.

[0029] Delivery principle: like Figure 3 As shown, when delivery is required, the rocket at the end of the feeding trough 9 must first be clamped. Before clamping, the drive motor 1077 starts, causing the swing arm 1076 to rotate. During rotation, the hinge rod 1075 moves along with it, and the hinge rod 1075 also drives the second connecting arm 1074. The movement of the second connecting arm 1074 causes the rotating seat 1072 to rotate around the bottom of the first connecting plate 1070. During the rotation of the rotating seat 1072, the first connecting arm 1073 rotates, causing the lifting seat 103 to continuously rise and fall. The delivery column 104 can also move laterally under the action of the transverse guide groove 16, thereby adjusting the position of the first clamping plate 105 and the second clamping plate 106 to facilitate the loading and unloading of the rocket. Figure 3 At the position shown, the rocket is being transferred. During this process, the second connecting arm 1074 will lift up and the first connecting arm 1073 will descend. During the descent, the release column 104 will drive the lifting seat 103 to descend along the guide column 102. During the descent, the rocket will also move to the left and vice versa. When the swing arm 1076 rotates one revolution, the release column 104 completes a closed loop of gripping and releasing the rocket.

[0030] See Figure 3 and Figure 6 The first connecting arm 1073 and the second connecting arm 1074 are both staggered and fixedly mounted on the rotating seat 1072. The length of the first connecting plate 1070 is greater than that of the second connecting plate 1071, and the first connecting plate 1070 is also staggered with the second connecting plate 1071. Through this technical solution, the staggered arrangement avoids interference between the hinge rod 1075 and the first connecting arm 1073. In a closed-loop process, collisions are prevented, and they do not affect each other, thus ensuring operational safety.

[0031] See Figure 1 , Figure 2 and Figure 7The vehicle-mounted container 2 has a window 24 on its top, and two telescopic top plates 25 are movably mounted on both sides of the window 24. The telescopic top plates 25 are used to close the window 24 when not in operation, and will be opened when in operation. The vehicle-mounted container 2 is also equipped with an inspection door 26 via hinges. A rocket storage box 27 is also fixedly installed on one side of the vehicle-mounted container 2, and the storage box 27 is located below the feeding trough 9.

[0032] The above are merely preferred embodiments of the present invention and are not intended to limit the present invention in any other way. Any person skilled in the art may make changes or modifications to the above-disclosed technical content to create equivalent embodiments that can be applied to other fields. However, any simple modifications, equivalent changes, and modifications made to the above embodiments based on the technical essence of the present invention without departing from the scope of the present invention shall still fall within the protection scope of the present invention.

Claims

1. A mobile weather modification operation cabin, comprising a self-propelled vehicle (1), characterized in that, The self-propelled vehicle (1) is equipped with a vehicle-mounted container (2). A horizontal slide rail (3) is installed at the bottom of the container (2). A rotation adjustment mechanism (4) is mounted on the slide rail (3). A launcher (5) is mounted on the rotation adjustment mechanism (4). Multiple sleeve assemblies (6) are installed inside the launcher (5). Each sleeve assembly (6) includes a first sleeve plate (60) and a second sleeve plate (61). The space between the first sleeve plate (60) and the second sleeve plate (61) is used to place the rocket to be launched. An auxiliary guide mechanism (7) is also provided between the multiple sleeve assemblies (6). Each side of the auxiliary guide mechanism (7) is equipped with a retaining ring (8), and the retaining ring (8) is located between the corresponding first sleeve plate (60) and second sleeve plate (61). A feeding trough (9) is also provided on one side of the interior of the vehicle-mounted container (2). The feeding trough (9) extends into the interior of the vehicle-mounted container (2). The auxiliary guiding mechanism (7) includes a guide plate (70). The guide plate (70) has a hollow structure inside, and each side of the guide plate (70) is provided with a strip guide groove (71). The guide plate (70) is also equipped with a lead screw motor (72). The lead screw motor (72) is also fixedly connected to the lead screw (73). The lead screw (73) is also equipped with a moving plate (74). The moving plate (74) is located inside the guide plate (70), and the two sides of the moving plate (74) are also fixedly connected with sliding arms (75). The sliding arms (75) pass through the corresponding guide groove (71), and each sliding arm (75) passes through the corresponding guide groove (71). 75) is also fixed with a retaining ring (8) at the far end, and a through hole (76) is opened in the middle of the retaining ring (8). The vehicle-mounted cabin (2) is also equipped with a delivery mechanism (10). The delivery mechanism (10) is located at the conveying end of the feeding trough (9) and above the launcher (5). The delivery mechanism (10) includes a plurality of symmetrically arranged mounting plates (101). One end of each mounting plate (101) is fixed to the inner wall of the vehicle-mounted cabin (2). Guide columns (102) are vertically installed between the upper and lower distributed mounting plates (101). A lifting seat (103) is movably mounted between two guide columns (102). A delivery column (104) is movably mounted on the lifting seat (103). The bottom of the delivery column (104) is movable. The first clamping plate (105) and the second clamping plate (106) are installed. The delivery column (104) is also movably installed with the linkage mechanism (107). The lifting seat (103) is also provided with a transverse guide groove (16). A sliding column (17) is installed in the transverse guide groove (16). The sliding column (17) is also vertically connected to the delivery column (104). An adjusting seat (18) is also movably installed at the bottom of the delivery column (104). A traction plate (19) is also provided on the adjusting seat (18). An angle adjusting electric cylinder (20) is also movably installed on the delivery column (104). The telescopic end of the angle adjusting electric cylinder (20) is also movably connected to the traction plate (19). A clamping electric cylinder (21) is provided below the adjusting seat (18).The telescopic ends on both sides of the clamping electric cylinder (21) are fixedly connected to the corresponding first clamping plate (105) and second clamping plate (106) via arc-shaped rods (22). The linkage mechanism (107) includes a first connecting plate (1070) and a second connecting plate (1071). The first connecting plate (1070) and the second connecting plate (1071) are both fixedly installed on the top of the vehicle-mounted container (2). A rotating seat is movably installed on one side of the bottom of the first connecting plate (1070). (1072) A first connecting arm (1073) and a second connecting arm (1074) are fixedly installed on the rotating seat (1072). A straight groove (23) is opened on the first connecting arm (1073), and the top of the delivery column (104) extends into the straight groove (23). One end of the second connecting arm (1074) is movably connected to a hinge rod (1075), and the other end of the hinge rod (1075) is movably connected to a swing arm (1076). The arm (1076) is movably mounted on the bottom of the second connecting plate (1071). The arm (1076) is also connected to the output end of the drive motor (1077). The first connecting arm (1073) and the second connecting arm (1074) are both staggered and fixedly mounted on the rotating seat (1072). The length of the first connecting plate (1070) is greater than that of the second connecting plate (1071), and the first connecting plate (1070) is also staggered with the second connecting plate (1071). The vehicle-mounted cabin (2) is also equipped with a monitoring system (11). The monitoring system (11) is used to monitor the external meteorological environment of the vehicle-mounted cabin (2). The monitoring system (11) is also connected to the rotation adjustment mechanism (4), the auxiliary guiding mechanism (7), and the delivery mechanism (10) respectively. The monitoring system (11) calculates the target launch angle based on the monitored meteorological data and controls the rotation adjustment mechanism (4) to adjust the launcher (5) to the target launch angle. The angle adjustment cylinder (20) drives the adjustment seat (18) to tilt relative to the launch column (104) according to the target launch angle, so that the axis of the rocket held by the first clamping plate (105) and the second clamping plate (106) is collinear with the axis of the sleeve assembly (6) of the launcher (5); the rear end of the launcher (5) is also provided with a trigger (12), the trigger (12) is connected to the monitoring system (11) by signal, the retaining ring (8) of the auxiliary guide mechanism (7) pushes the rocket to the trigger (12), and the trigger (12) contacts the bottom of the rocket through the through hole (76).

2. The mobile weather modification cabin according to claim 1, characterized in that, The rotating adjustment mechanism (4) includes a base (40), which is slidably mounted on a slide rail (3). A rotating plate (41) is rotatably mounted on the upper part of the base (40). A support frame (42) is fixedly mounted on the rotating plate (41). Lifting cylinders (43) are symmetrically arranged on the upper part of the support frame (42). The top of each lifting cylinder (43) is movably connected to the launcher (5). Connecting arms (44) are rotatably mounted on both sides of the launcher (5), and the other end of each connecting arm (44) is movably connected to one side of the support frame (42).

3. The mobile weather modification cabin according to claim 1, characterized in that, Arc-shaped grooves (45) are provided on the opposite sides of the first set plate (60) and the second set plate (61).

4. The mobile weather modification cabin according to claim 1, characterized in that, The conveying end of the feeding trough (9) is also equipped with a rotating shaft (13). A servo motor (14) is also fixedly installed on one side of the feeding trough (9). The servo motor (14) is also connected to the rotating shaft (13). Multiple flow stabilizers (15) are fixed at intervals on the rotating shaft (13). Each flow stabilizer (15) is arc-shaped and has a stationary part (151) and a dividing part (152).

5. The mobile weather modification cabin according to claim 1, characterized in that, The vehicle-mounted container (2) has a window (24) on its top, and two telescopic top plates (25) are movably mounted on both sides of the window (24). The vehicle-mounted container (2) also has an inspection door (26) installed on it via hinges. A rocket storage box (27) is also fixedly installed on one side of the vehicle-mounted container (2), and the storage box (27) is located below the feeding trough (9).

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