Adjustable weather modification rocket launching rail

Abstract

The utility model provides an adjustable weather modification rocket launching guide rail, including mainframe box, rotary support frame, adjusting plate, rocket launching guide rail, main guide rail, first telescopic vice guide rail and second limit vice guide rail, the rotary support frame is installed on mainframe box upper end, be provided with adjusting plate in the rotary support frame, be installed with rocket launching guide rail on adjusting plate upper end, be provided with main guide rail in rocket launching guide rail, be provided with first telescopic vice guide rail in main guide rail, be provided with second limit vice guide rail in main guide rail, this design has solved the problem that needs to change different model rocket frame guide rail back and forth when the launch of two kinds of rocket bomb length is inconsistent, the utility model discloses reasonable in structure, be provided with movable frame through setting up in fixed frame front end, it cooperates with sliding limit seat and first telescopic vice guide rail and second limit vice guide rail, need not to change rocket launching guide rail to launch different model rocket bomb.

Description

Technical Field

[0001] This utility model is an adjustable rocket launch rail for artificial weather modification, belonging to the field of rocket launch rails. Background Technology

[0002] Rain-inducing and hail-suppressing rockets are civilian rockets that use rocket launch rails to seed catalysts into clouds. The catalysts alter the microphysical structure of hail and precipitation clouds, thus increasing rainfall and suppressing hail. These rockets are widely used today. However, due to the different rocket models, which vary in length, existing rocket launch rails can only launch one type of rocket. Launching another type requires repeatedly changing different rocket launch rails, making the operation cumbersome. There is an urgent need for an adjustable artificial weather modification rocket launch rail to solve these problems. Utility Model Content

[0003] To address the shortcomings of existing technologies, the purpose of this invention is to provide an adjustable artificial weather modification rocket launch rail to solve the problems mentioned in the background. This invention has a reasonable structure. By setting a movable frame at the front end of the fixed frame, which cooperates with the sliding limit seat, the first telescopic auxiliary rail, and the second limit auxiliary rail, different types of rockets can be launched without replacing the rocket launch rail.

[0004] To achieve the above objectives, this utility model provides the following technical solution: an adjustable artificial weather modification rocket launch rail, comprising a main chassis, casters, a handgrip, a first drive motor, a rotating support frame, a second drive motor, a drive gear, an adjustment plate, a rocket launch rail, a main guide rail, a first telescopic auxiliary guide rail, and a second limiting auxiliary guide rail. Casters are located below the main chassis, a handgrip is mounted at the rear of the main chassis, the first drive motor is located inside the main chassis, a rotating support frame is mounted at the top of the main chassis, a second drive motor is located inside the rotating support frame, an adjustment plate is located inside the rotating support frame, a rocket launch rail is mounted at the upper end of the adjustment plate, a main guide rail is located inside the rocket launch rail, a first telescopic auxiliary guide rail is located inside the main guide rail, and a second limiting auxiliary guide rail is located inside the main guide rail.

[0005] Furthermore, hub frames are installed on both the left and right ends of the main unit, and the movable wheels are located inside the hub frames. A limit groove is opened at the upper end of the main unit, and the first drive motor is located inside the limit groove. A first drive shaft is provided at the upper end of the first drive motor. The rotating support frame is electrically connected to the first drive motor through the first drive shaft. A left bracket is provided on the left side of the rotating support frame, a right bracket is provided on the right side of the rotating support frame, and a base plate is provided at the bottom end of the rotating support frame.

[0006] Furthermore, the second drive motor is installed on the right bracket on the side relatively close to the adjustment plate. A wire box is provided at the right end of the right bracket. A second drive shaft is installed at the left end of the second drive motor. The other end of the second drive shaft is rotatably fixed on the left bracket. A drive gear is sleeved on the second drive shaft. A meshing tooth is provided at the lower end of the adjustment plate. The adjustment plate meshes with the drive gear through the meshing tooth.

[0007] Furthermore, the left end of the adjustment plate has several sets of fixing holes, the upper end of the base plate is provided with a fixing rod support seat, the fixing rod is provided inside the fixing rod support seat, the fixing rod is fixedly connected to the adjustment plate through the fixing rod, a guide rail base is provided above the adjustment plate, and fixing nuts are provided at both ends of the adjustment plate, the adjustment plate is fixedly connected to the guide rail base through the fixing nuts, and a rotating fixing shaft is provided on the outer side of the left bracket and the right bracket, the guide rail base is rotatably connected to the left bracket and the right bracket through the rotating fixing shaft.

[0008] Furthermore, the rocket launch rail is fixed on the rail base, the lower end of the rocket launch rail is provided with a launch rail base plate, and several sets of fixed frames are provided inside the rocket launch rail, with the main rail being set inside the fixed frames.

[0009] Furthermore, a movable frame is provided on the front side of the fixed frame, and two sets of limiting slides are provided on the upper end of the launch guide rail base plate near the front end. Two sets of pulleys are provided on the lower end of the movable frame. The movable frame is slidably connected to the limiting slides through the pulleys, and the movable frame is slidably connected to the main guide rail through the first telescopic secondary guide rail and the second limiting secondary guide rail.

[0010] Furthermore, sliding limit seats are provided at both ends of the launch guide rail base plate near the front end. A first limit hole is provided through the outer side of the two sets of sliding limit seats. A second limit hole is provided at both ends of the movable frame. A fixed slide rod is provided inside the first limit hole and the second limit hole. The movable frame is slidably connected to the sliding limit seat through the fixed slide rod.

[0011] The beneficial effects of this utility model are as follows: This utility model provides an adjustable artificial weather modification rocket launch rail. It includes a rail base, a launch rail base plate, a sliding limit seat, a movable frame, a limit slide rod, a fixed frame, a main rail, a first telescopic auxiliary rail, and a second limit auxiliary rail. The launch rail base plate is located at the lower end of the rail base, and sliding limit seats are located at both ends of the launch rail base plate. A limit slide rod is provided between the sliding limit seat and the movable frame. The movable frame can be fixed and moved again after the track length is changed through the limit slide rod and the sliding limit seat. The first telescopic auxiliary rail and the second limit auxiliary rail slide and extend within the main rail and connect the fixed frame and the movable frame, assisting the movable frame in sliding and thus changing the rocket launch track length. This design solves the problem of having to repeatedly change different types of rocket launcher rails when launching rockets with inconsistent lengths. Attached Figure Description

[0012] Other features, objects, and advantages of this invention will become more apparent from the following detailed description of non-limiting embodiments with reference to the accompanying drawings:

[0013] Figure 1 This is a schematic diagram of the main structure of an adjustable artificial weather modification rocket launch rail according to this utility model.

[0014] Figure 2 This is a schematic diagram of the internal structure of the main unit of an adjustable artificial weather modification rocket launch rail according to this utility model.

[0015] Figure 3 This is a partial structural diagram of an adjustable artificial weather modification rocket launch rail according to the present invention.

[0016] Figure 4 This is a partial structural cross-sectional view of an adjustable artificial weather modification rocket launch rail according to this utility model;

[0017] Figure 5 This is a schematic diagram of the rocket launch rail structure of an adjustable artificial weather modification rocket launch rail according to this utility model;

[0018] Figure 6 This is a schematic diagram of the sliding limit seat structure of an adjustable artificial weather modification rocket launch guide rail according to this utility model.

[0019] Figure 7 This is a schematic diagram of the main rail structure of an adjustable artificial weather modification rocket launch guide rail according to this utility model;

[0020] In the diagram: 1-Main chassis, 101-Hand grip, 102-Limiting groove, 2-Hub frame, 21-Moving wheel, 3-Rotating support frame, 31-Right bracket, 32-Left bracket, 33-Base plate, 4-Drive gear, 41-Second drive shaft, 5-Adjusting plate, 51-Gear, 52-Fixing hole, 53-Fixing nut, 6-Rocket launch rail, 61-Fixing frame, 62-Launch rail base plate, 63-Limiting slide, 7-First drive Motor, 71-First drive shaft, 8-Wire box, 81-Second drive motor, 9-Guide rail base, 91-Rotating fixed shaft, 10-Fixed rod support, 1001-Fixed rod, 11-Main guide rail, 111-First telescopic auxiliary guide rail, 112-Second limiting auxiliary guide rail, 12-Sliding limiting seat, 121-First limiting hole, 13-Modible frame, 131-Second limiting hole, 132-Fixed slide rod, 133-Pulley. Detailed Implementation

[0021] To make the technical means, creative features, objectives and effects of this utility model easier to understand, the present utility model will be further described below in conjunction with specific embodiments.

[0022] Please see Figures 1-7 This utility model provides a technical solution: an adjustable artificial weather modification rocket launch rail, including a main unit 1, moving wheels 21, a handgrip 101, a first drive motor 7, a rotating support frame 3, a second drive motor 81, a drive gear 4, an adjustment plate 5, a rocket launch rail 6, a main guide rail 11, a first telescopic auxiliary guide rail 111, and a second limiting auxiliary guide rail 112. Moving wheels 21 are located below the main unit 1, and a handgrip 101 is installed at the rear end of the main unit 1. The first drive motor 7 is located inside the main unit 1, and a rotating support frame 3 is installed at the upper end of the main unit 1. The second drive motor 81 is located inside the rotating support frame 3, and an adjustment plate 5 is located inside the rotating support frame 3. The rocket launch rail 6 is installed at the upper end of the adjustment plate 5, and a main guide rail 11 is located inside the rocket launch rail 6. The first telescopic auxiliary guide rail 111 is located inside the main guide rail 11, and the second limiting auxiliary guide rail 112 is located inside the main guide rail 11. This design solves the problem of having to repeatedly change different types of rocket launch rails when launching rockets with inconsistent lengths.

[0023] As the first embodiment of this utility model: Hub frames 2 are installed on both the left and right ends of the main unit housing 1. Movable wheels 21 are located inside the hub frames 2, which protect the movable wheels 21. A limit groove 102 is formed at the upper end of the main unit housing 1. A first drive motor 7 is located inside the limit groove 102. A first drive shaft 71 is provided at the upper end of the first drive motor 7. A rotating support frame 3 is electrically connected to the first drive motor 7 via the first drive shaft 71. The first drive motor 7 controls the rotation of the rotating support frame 3 via the first drive shaft 71, thereby allowing the rocket launch rail 6, which is indirectly connected to it, to rotate freely in the horizontal direction. The rotating support frame 3 serves to support and fix the rail base 9. A left bracket 32 ​​is provided on the left side of the rotating support frame 3, and a right bracket 32 ​​is provided on the right side of the rotating support frame 3. The bracket 31 and the rotating support frame 3 have a base plate 33 at their bottom ends. The second drive motor 81 is installed on the right bracket 31, relatively close to the adjusting plate 5. A junction box 8 is installed on the right end of the right bracket 31, which supplies power to the second drive motor 81. A second drive shaft 41 is installed on the left end of the second drive motor 81, and the other end of the second drive shaft 41 is rotatably fixed on the left bracket 32. The second drive motor 81 controls the rotation of the second drive shaft 41. A drive gear 4 is sleeved on the second drive shaft 41. A meshing tooth 51 is provided at the lower end of the adjusting plate 5. The adjusting plate 5 meshes with the drive gear 4 through the meshing tooth 51. Furthermore, when the second drive motor 81 controls the rotation of the second drive shaft 41, the sleeved drive gear 4 rotates, and the adjusting plate 5 rotates accordingly by a certain angle. A through opening is provided at the left end of the adjusting plate 5. Several sets of fixing holes 52 are used to fix the adjustment plate 5. A fixing rod support 10 is provided on the upper end of the base plate 33. A fixing rod 1001 is provided inside the fixing rod support 10. The fixing rod 1001 is fixedly connected to the adjustment plate 5 through the fixing rod 1001. When the adjustment plate 5 is rotated to an appropriate angle, it can be fixed by the fixing rod 1001 to prevent it from moving. A guide rail base 9 is provided above the adjustment plate 5. The guide rail base 9 is used to fix the rocket launch guide rail 6. Fixing nuts 53 are provided on both the left and right ends of the adjustment plate 5. The adjustment plate 5 is fixedly connected to the guide rail base 9 through the fixing nuts 53. Rotation fixing shafts 91 are provided on the outer side of the left bracket 32 ​​and the right bracket 31. The guide rail base 9 is connected to the left bracket 32 ​​and the right bracket 31 through the rotation fixing shafts 91. The bracket 31 is rotatably connected, and the rotating fixed shaft 91 assists in the rotation of the guide rail base 9. When the adjusting plate 5 rotates, it drives the guide rail base 9 to rotate. The rocket launch guide rail 6 is fixed on the guide rail base 9. A launch guide rail base plate 62 is provided at the lower end of the rocket launch guide rail 6. Several sets of fixed frames 61 are provided inside the rocket launch guide rail 6. The fixed frames 61 serve to fix the rocket. The main guide rail 11 is set inside the fixed frames 61. The main guide rail 11 serves to fix the launch trajectory of the rocket. A movable frame 13 is provided on the front side of the fixed frame 61. The movable frame 13 is used to adjust the length of the rocket launch guide rail 6. Two sets of limiting slides 63 are opened at the upper end of the launch guide rail base plate 62 near the front end. Two sets of pulleys 133 are provided at the lower end of the movable frame 13.The movable frame 13 is slidably connected to the limiting slide rail 63 via pulleys 133. The movable frame 13 is slidably connected to the main guide rail 11 via the first telescopic auxiliary guide rail 111 and the second limiting auxiliary guide rail 112. Sliding limiting seats 12 are provided at both ends of the launch guide rail base plate 62, near the front end. The sliding limiting seats 12 control the movement and fixation of the movable frame 13. A first limiting hole 121 is provided through the outer side of both sets of sliding limiting seats 12, and a second limiting hole 131 is provided at both ends of the movable frame 13. A fixed slide rod 132 is provided inside the first limiting hole 121 and the second limiting hole 131. The movable frame 13 moves by moving the fixed slide rod 132 within the first limiting hole 121. Furthermore, the first telescopic auxiliary guide rail 111 and the second limiting auxiliary guide rail 112 extend and retract within the main guide rail 11 to change the track length. The movable frame 13 is slidably connected to the sliding limiting seats 12 via the fixed slide rod 132.

[0024] As a second embodiment of this utility model: When using this utility model to switch between two types of rockets for launch, the user first moves the fixed slide bar 132 inside the sliding limit seat 12 from one end to the other. At the same time, the user pushes or pulls the movable frame 13 to move inward or outward. The pulley 133 at the lower end of the movable frame 13 slides inside the limit slide 63 to assist the movement of the movable frame 13. The first telescopic auxiliary guide rail 111 and the second limit auxiliary guide rail 112 extend or retract inside the main guide rail 11 to change the length of the track. After selecting the appropriate rocket launch guide rail 6, the rocket is placed inside the fixed frame 61. After rotating the rocket launch guide rail 6 to an appropriate angle by operating the first drive motor 7 and the second drive motor 81, the user should move away from this utility model and launch the rocket remotely using the remote control.

[0025] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. It will be apparent to those skilled in the art that this utility model is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or basic characteristics of this utility model. Therefore, the embodiments should be considered exemplary and non-limiting in all respects. The scope of this utility model is defined by the appended claims rather than the foregoing description, and thus all variations falling within the meaning and scope of equivalents of the claims are intended to be included within this utility model. No reference numerals in the claims should be construed as limiting the scope of the claims.

[0026] Furthermore, it should be understood that although this specification describes embodiments, not every embodiment contains only one independent technical solution. This narrative style is merely for clarity. Those skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.

Claims

1. An adjustable artificial weather modification rocket launch rail, comprising a main housing, casters, a handgrip, a first drive motor, a rotating support frame, a second drive motor, a drive gear, an adjustment plate, a rocket launch rail, a main guide rail, a first telescopic auxiliary guide rail, and a second limiting auxiliary guide rail, characterized in that: The main unit is equipped with casters at the bottom and a handgrip at the rear. A first drive motor is installed inside the main unit, and a rotating support frame is installed at the top. A second drive motor is installed inside the rotating support frame, and an adjustment plate is installed inside the rotating support frame. A rocket launch guide rail is installed at the upper end of the adjustment plate. A main guide rail is installed inside the rocket launch guide rail, a first telescopic auxiliary guide rail is installed inside the main guide rail, and a second limiting auxiliary guide rail is installed inside the main guide rail.

2. An adjustable weather modification rocket launching rail as in claim 1, wherein: The main unit is equipped with hub brackets on both the left and right ends, and the movable wheels are located inside the hub brackets. A limit groove is opened at the top of the main unit, and the first drive motor is located inside the limit groove. A first drive shaft is provided at the top of the first drive motor. The rotating support frame is electrically connected to the first drive motor through the first drive shaft. A left bracket is provided on the left side of the rotating support frame, a right bracket is provided on the right side of the rotating support frame, and a base plate is provided at the bottom of the rotating support frame.

3. An adjustable weather modification rocket launch rail according to claim 2, wherein: The second drive motor is installed on the right bracket, which is relatively close to the adjustment plate. A wire box is provided on the right end of the right bracket. A second drive shaft is installed on the left end of the second drive motor. The other end of the second drive shaft is rotatably fixed on the left bracket. A drive gear is sleeved on the second drive shaft. A meshing tooth is provided on the lower end of the adjustment plate. The adjustment plate meshes with the drive gear through the meshing tooth.

4. An adjustable weather modification rocket launch rail in accordance with claim 3, wherein: The left end of the adjustment plate has several sets of fixing holes. The upper end of the base plate is provided with a fixing rod support seat. The fixing rod is provided inside the fixing rod support seat. The fixing rod is fixedly connected to the adjustment plate through the fixing rod. A guide rail base is provided above the adjustment plate. Fixing nuts are provided at both ends of the adjustment plate. The adjustment plate is fixedly connected to the guide rail base through the fixing nuts. Rotation fixing shafts are provided on the outer sides of the left and right brackets. The guide rail base is rotatably connected to the left and right brackets through the rotation fixing shafts.

5. An adjustable weather modification rocket launch rail in accordance with claim 4, wherein: The rocket launch rail is fixed on the rail base, and a launch rail base plate is provided at the lower end of the rocket launch rail. Several sets of fixed frames are provided inside the rocket launch rail, and the main rail is set inside the fixed frames.

6. An adjustable artificial weather modification rocket launch rail according to claim 5, characterized in that: A movable frame is provided on the front side of the fixed frame. Two sets of limiting slides are provided on the upper end of the launch guide rail base plate near the front end. Two sets of pulleys are provided on the lower end of the movable frame. The movable frame is slidably connected to the limiting slides through the pulleys. The movable frame is slidably connected to the main guide rail through the first telescopic secondary guide rail and the second limiting secondary guide rail.

7. An adjustable artificial weather modification rocket launch rail according to claim 6, characterized in that: The launch guide rail base plate has sliding limit seats at both ends near the front end. The two sets of sliding limit seats have first limit holes through the outer side. The movable frame has second limit holes at both ends. Fixed slide rods are provided inside the first limit holes and the second limit holes. The movable frame is slidably connected to the sliding limit seats through the fixed slide rods.

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