Universal figure rocket launcher

Abstract

The utility model relates to the technical field of artificial precipitation enhancement, and provides a universal figure rocket launcher which comprises a launch canister, four hollow plates are fixed on the outer wall of the launch canister, the hollow plates are communicated with the inner side of the launch canister, the inner sides of the hollow plates are movably connected with fixing assemblies in an inserted mode, the number of the fixing assemblies is four, and the number of the fixing assemblies is four. And the fixing assembly comprises a moving plate, an arc-shaped fixing plate and a connecting rod, the moving plate is movably connected to the inner side of the hollow plate in an inserted mode, and the arc-shaped fixing plate is fixed to one side wall of the moving plate. The fixing assembly is arranged on the inner side of the hollow plate of the outer wall of the launch canister, the rocket projectile is inserted into the inner side of the launch canister, the empennage is inserted into the inner side of the empennage groove, the four arc-shaped fixing plates are pushed by the spring to clamp and fix the outer wall of the rocket projectile, and the size of a circular space defined by the four arc-shaped fixing plates can be changed according to elastic stretching of the spring. And therefore, rocket projectiles with different specifications and sizes can be fixed, and the universality during use is enhanced.

Description

Technical Field

[0001] This utility model relates to the field of artificial rain enhancement technology, specifically a universal artificial rain enhancement rocket launcher. Background Art

[0002] Artificial precipitation, also known as rain enhancement, refers to the process of artificially supplementing certain necessary conditions for precipitation formation based on the principles of natural precipitation formation. This promotes the rapid condensation or collision and enlargement of cloud droplets into raindrops, which then fall to the ground. The method involves selecting appropriate times based on the physical characteristics of different cloud layers and using aircraft or rockets to seed clouds with catalysts such as dry ice, silver iodide, and salt powder. This induces precipitation or increases the amount of precipitation, thereby relieving or alleviating drought in farmland, increasing irrigation water volume or water supply capacity in reservoirs, or increasing water production for power generation, etc.

[0003] Currently, using artificial rainmaking rockets carrying silver iodide catalysts to artificially catalyze cloud systems to influence local weather has become one of the most effective methods in recent years. The currently used artificial rainmaking rockets are mainly available in three sizes: 82mm, 66mm, and 56mm, to adapt to different weather conditions, different cloud systems, and different altitudes. However, existing rocket launchers have limited applicability and cannot be used interchangeably with all current rocket types, resulting in unsatisfactory catalytic effects and high operating costs.

[0004] Therefore, a universal man-made rocket launcher is needed that can be used for rockets of different sizes and specifications, thereby enhancing the versatility of the launcher. Utility Model Content

[0005] To address the aforementioned problems, this invention proposes a universal artificial rocket launcher, which features good versatility and simple operation.

[0006] To achieve the above objectives, the present invention proposes the following specific solutions:

[0007] A universal manned rocket launcher includes a launch tube. A hollow plate is fixed to the outer wall of the launch tube, and the hollow plate communicates with the inner side of the launch tube. Four hollow plates are provided. Four fixing components are movably inserted into the inner side of the hollow plates. Each fixing component includes a movable plate, an arc-shaped fixing plate, and a connecting rod. The movable plate is movably inserted into the inner side of the hollow plate. An arc-shaped fixing plate is fixed to one side wall of the movable plate, located inside the launch tube. A connecting groove is provided on the other side wall of the movable plate. A spring is fixed to the inner wall of one side of the connecting groove. A connecting rod is fixed to one end of the spring. One end of the connecting rod is movably inserted into the inner side of the connecting groove, and the other end is fixed to the inner wall of the hollow plate. Four tail fin grooves are provided on the inner wall of the launch tube, and the tail fin grooves are staggered with the fixing components. Four fixing rods are fixed to one side wall of the launch tube, and a fixing plate is fixed to one end of each fixing rod.

[0008] As a preferred technical solution of a general-purpose artificial rocket launcher of this utility model, a support plate is fixed to the outer wall of the launch tube, and an mounting plate is fixed to the bottom surface of the support plate.

[0009] As a preferred technical solution of a general-purpose artificial rocket launcher of this utility model, the top edge of the mounting plate is provided with a mounting hole, which penetrates the mounting plate.

[0010] As a preferred technical solution for a general-purpose man-made rocket launcher of this utility model, rectangular grooves are symmetrically provided on one side of the inner wall of the tail fin groove.

[0011] As a preferred technical solution for a general-purpose artificial rocket launcher of this utility model, a tube plug is movably inserted into the inner side of one end of the launch tube.

[0012] As a preferred technical solution of a general-purpose artificial rocket launcher of this utility model, a connecting rope is fixed to the outer wall of the tube plug, and one end of the connecting rope is fixed to the outer wall of the launch tube.

[0013] As a preferred technical solution for a general-purpose artificial rocket launcher of this utility model, the plug is made of flexible material and the connecting rope is made of elastic material.

[0014] As a preferred technical solution for a general-purpose artificial rocket launcher of this utility model, multiple mounting holes, connecting grooves, springs and connecting rods are provided.

[0015] Compared with existing technologies, this utility model has the following advantages:

[0016] This invention features a fixing assembly on the inner side of the hollow plate on the outer wall of the launch tube. The fixing assembly consists of four arc-shaped fixing plates that clamp and fix the outer wall of the rocket. Due to the elastic extension and contraction of the spring, the moving plate can move inside the hollow plate to drive the arc-shaped fixing plates to move. This allows the size of the circular space enclosed by the four arc-shaped fixing plates to be adjusted, thus ensuring that rockets of different specifications and sizes can be used, exhibiting strong versatility.

[0017] The outer wall of the launch tube of this utility model is fixed with a support plate, and the bottom surface of the support plate is fixed with a mounting plate. The mounting plate is provided with multiple mounting holes, and the launch tube can be fixed in a suitable position by bolts through the mounting holes. Multiple launch tubes can be combined for use, thereby launching multiple rockets at one time and improving the efficiency of artificial rain enhancement. Attached Figure Description

[0018] To better describe the technical solution of this utility model in detail, the present invention will be further described below with reference to the accompanying drawings and embodiments.

[0019] Figure 1 This is a three-dimensional view of the overall structure provided by this utility model;

[0020] Figure 2 This is a three-dimensional sectional view of the present invention;

[0021] Figure 3 This is a perspective view of the fixing component of this utility model;

[0022] Figure 4 This is a partial cross-sectional view of the fixing component of this utility model;

[0023] Figure 5 This utility model Figure 2 Enlarged diagram of point A in the middle.

[0024] In the diagram: 1. Launch tube; 11. Support plate; 111. Mounting plate; 112. Mounting hole; 12. Tube plug; 121. Connecting rope; 13. Fixing rod; 131. Fixing disc; 14. Hollow plate; 15. Tail fin groove; 151. Rectangular groove; 2. Fixing assembly; 21. Moving plate; 211. Connecting groove; 212. Spring; 22. Arc-shaped fixing plate; 23. Connecting rod. DETAILED DESCRIPTION

[0025] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of the present utility model. Example

[0026] Please see Figure 1-5 As shown, the present invention provides the following technical solution: a universal artificial rocket launcher, including a launch tube 1, a hollow plate 14 fixed on the outer wall of the launch tube 1, the hollow plate 14 communicating with the inner side of the launch tube 1, four hollow plates 14 are provided, the hollow plates 14 are used to accommodate the fixed component 2, and provide a certain moving space for the movable plate 21.

[0027] Reference Figure 1 , Figure 2 , Figure 3 , Figure 4 and Figure 5 As shown, specifically, a fixing assembly 2 is movably inserted into the inner side of the hollow plate 14 for fixing the rocket. There are four fixing assemblies 2, each including a movable plate 21, an arc-shaped fixing plate 22, and a connecting rod 23. The movable plate 21 is movably inserted into the inner side of the hollow plate 14, and can drive the arc-shaped fixing plate 22 to adjust its position. An arc-shaped fixing plate 22 is fixed to one side wall of the movable plate 21 for clamping and fixing the rocket. The arc-shaped fixing plate 22 is located inside the launch tube 1. A connecting groove 211 is provided on the other side wall of the movable plate 21 for accommodating a spring 212 and connecting the connecting rod 23. A spring 212 is fixed to one inner wall of the connecting groove 211. The elastic extension and contraction of the spring 212 can drive the movable plate 21 to move, and the supporting effect of the spring 212 can ensure the clamping of the rocket by the arc-shaped fixing plate 22. To maintain stability, one end of the spring 212 is fixed with a connecting rod 23, which enhances the stability of the moving plate 21. One end of the connecting rod 23 is movably inserted into the inner side of the connecting groove 211, and the other end of the connecting rod 23 is fixed to the inner wall of the hollow plate 14. A plug 12 is movably inserted into the inner side of one end of the launch tube 1 to seal the launch tube 1 and prevent foreign objects from falling into the launch tube 1. The plug 12 is made of flexible material, and a connecting rope 121 is fixed to the outer wall of the plug 12 to prevent the plug 12 from falling off. The connecting rope 121 is made of elastic material, and one end of the connecting rope 121 is fixed to the outer wall of the launch tube 1. The size of the circular space formed by the four arc-shaped fixing plates 22 in the four fixing components 2 of this scheme can change according to the extension and contraction of the spring 212, so that rockets of different specifications and sizes can be clamped and fixed, which has strong versatility.

[0028] Reference Figure 1 and Figure 2As shown, specifically, the inner wall of the launch tube 1 is provided with tail fin grooves 15 for placing the tail fins of the rocket to maintain the stability of the rocket launch. There are four tail fin grooves 15, which are staggered with the fixing component 2. A rectangular groove 151 is symmetrically provided on one side of the inner wall of the tail fin groove 15 to dissipate the flame and heat inside the launch tube 1. A fixing rod 13 is fixed on one side wall of the launch tube 1 to fix the fixing plate 131. There are four fixing rods 13, and a fixing plate 131 is fixed to one end of the fixing rod 13 to support the tail of the rocket. In this scheme, the space between the fixing plate 131 and the launch tube 1, as well as the rectangular grooves 151, can be used to dissipate the flame and heat generated when the rocket is launched to the inside of the launch tube 1, so as to avoid the excessive temperature from damaging the inside of the launch tube 1.

[0029] Reference Figure 1 and Figure 2 As shown, specifically, a support plate 11 is fixed to the outer wall of the launch tube 1 to support the launch tube 1. A mounting plate 111 is fixed to the bottom surface of the support plate 11 to fix the launch tube 1. The top edge of the mounting plate 111 is provided with mounting holes 112 to fix the mounting plate 111. The mounting holes 112 penetrate the mounting plate 111. Multiple mounting holes 112, connecting grooves 211, springs 212 and connecting rods 23 are provided. In this solution, bolts can be used to fix the mounting plate 111 in a suitable launch position, and multiple launch tubes 1 can be fixed side by side to achieve the effect of launching multiple rockets at once, thereby improving the efficiency of artificial rain enhancement.

[0030] The working principle and usage process of this utility model:

[0031] During use, bolts are used to pass through the mounting holes 112 to fix the mounting plate 111 in a suitable position, thereby stabilizing the launch tube 1. This solution allows multiple launch tubes 1 to be fixed side by side to achieve the simultaneous launch of multiple rockets. During launch, the tube plug 12 is pulled out from the inside of the launch tube 1, and the rocket is inserted into the inside of the launch tube 1. The tail fins of the rocket are located inside the tail fin groove 15. Under the elastic force of the spring 212, the moving plate 21 moves inside the hollow plate 14, causing the arc-shaped fixing plate 22 to move and fit tightly against the outer wall of the rocket. The four arcs... The four arc-shaped fixing plates 22 clamp and fix the rocket. Under the elastic extension and contraction control of the spring 212, the size of the circular space formed by the four arc-shaped fixing plates 22 can be changed, which can be used for rockets of different specifications and sizes. The fixing plate 131 can provide certain support for the tail of the rocket. The flame and heat generated during the rocket launch process can be dissipated through the space between the fixing plate 131 and the launch tube 1. The rectangular groove 151 can also help dissipate the flame and heat, so as to avoid the internal temperature of the launch tube 1 from being too high and causing damage.

[0032] Finally, it should be noted that the above description is merely a preferred embodiment of this utility model and is not intended to limit the utility model. Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. A universal artificial rocket launcher, comprising a launch tube (1), characterized in that: A hollow plate (14) is fixed to the outer wall of the launch tube (1). The hollow plate (14) is connected to the inner side of the launch tube (1). There are four hollow plates (14). A fixing component (2) is movably inserted into the inner side of the hollow plate (14). There are four fixing components (2). The fixing component (2) includes a movable plate (21), an arc-shaped fixing plate (22), and a connecting rod (23). The movable plate (21) is movably inserted into the inner side of the hollow plate (14). An arc-shaped fixing plate (22) is fixed to one side wall of the movable plate (21). The arc-shaped fixing plate (22) is located inside the launch tube (1). A connecting groove is provided on the other side wall of the movable plate (21). 211), a spring (212) is fixed on one side of the inner wall of the connecting groove (211), a connecting rod (23) is fixed at one end of the spring (212), one end of the connecting rod (23) is movably inserted into the inner side of the connecting groove (211), and the other end of the connecting rod (23) is fixed on the inner wall of the hollow plate (14). The inner wall of the launch tube (1) is provided with a tail fin groove (15), and there are four tail fin grooves (15). The tail fin grooves (15) and the fixing components (2) are arranged alternately. A fixing rod (13) is fixed on one side of the launch tube (1), and there are four fixing rods (13). A fixing plate (131) is fixed at one end of the fixing rod (13).

2. The universal artificial rocket launcher according to claim 1, characterized in that: The outer wall of the launch tube (1) is fixed with a support plate (11), and the bottom surface of the support plate (11) is fixed with an mounting plate (111).

3. A universal artificial rocket launcher according to claim 2, characterized in that: The mounting plate (111) has a mounting hole (112) on the top edge, and the mounting hole (112) penetrates the mounting plate (111).

4. A universal artificial rocket launcher according to claim 3, characterized in that: The inner wall of one side of the tail fin groove (15) is provided with symmetrical ventilation holes (151).

5. A universal artificial rocket launcher according to claim 4, characterized in that: A plug (12) is movably inserted into the inner side of one end of the launching tube (1).

6. A universal artificial rocket launcher according to claim 5, characterized in that: A connecting rope (121) is fixed to the outer wall of the plug (12), and one end of the connecting rope (121) is fixed to the outer wall of the launch tube (1).

7. A universal artificial rocket launcher according to claim 6, characterized in that: The plug (12) is made of flexible material, and the connecting rope (121) is made of elastic material.

8. A universal artificial rocket launcher according to claim 7, characterized in that: The mounting hole (112), connecting groove (211), spring (212) and connecting rod (23) are each provided with multiple holes.

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