Portable artificial rainmaking rocket stable launching rack

Abstract

The utility model relates to the technical field of artificial rain enhancement, and specifically discloses a portable artificial rain enhancement rocket missile stable launching rack, which comprises a base, an adjusting mechanism, a rotating seat, a connecting frame, a rotating shaft, a rotating sleeve seat, a mounting rod, an inserting slot and a limiting inserting rod. When the launching rack is disassembled, the limiting inserting rod is separated from the mounting limit on the mounting rod through the rotation of the nut seat, so that the overall disassembly operation of the clamping mechanism on the mounting rod is carried out, the disassembly of the clamping mechanism is facilitated, the modular disassembly of the clamping mechanism is realized, the transportation volume is greatly reduced, the portability is improved, and the user is allowed to freely combine single or multiple launching arrays on the mounting rod according to task requirements.

Description

Technical Field

[0001] This utility model belongs to the field of artificial rain enhancement technology, specifically relating to a portable artificial rain enhancement rocket stable launcher. Background Technology

[0002] Artificial rain enhancement is a scientific operation that increases precipitation by artificially intervening in the microphysical processes of clouds that have natural precipitation conditions. Catalysts are seeded into the clouds to promote the formation and growth of ice crystals or the collision and growth of cloud droplets. At the same time, the latent heat released by water vapor condensation can enhance the upward motion within the cloud, further improving precipitation efficiency.

[0003] In the current artificial rain enhancement system, the rocket launcher is a key piece of equipment for accurately delivering rain-enhancing rockets containing catalysts to the target cloud layer. Its performance directly affects the coverage and efficiency of the operation. Most of the existing mainstream rain-enhancing rocket launchers adopt a fixed integrated frame structure design, that is, the launching device, support base, directional guide rail and control system are highly integrated into a rigid frame. The whole is in the form of a large box or truss. The structure is stable, but there are significant limitations in space and mobility. Utility Model Content

[0004] The purpose of this invention is to provide a portable artificial rainmaking rocket launcher to solve the problem mentioned in the background art that existing rainmaking rocket launchers mostly adopt a fixed integrated frame structure, which is bulky and cannot be disassembled, making them difficult to carry.

[0005] To achieve the above objectives, this utility model provides the following technical solution:

[0006] A portable artificial rainmaking rocket stabilization launcher includes:

[0007] Base;

[0008] An adjustment mechanism is installed above the base. The adjustment mechanism includes a rotating seat, a connecting frame is fixedly connected to the top of the rotating seat, and a rotating shaft is provided on the outside of the connecting frame.

[0009] The mounting mechanism is located outside the adjusting mechanism. The mounting mechanism includes a rotating sleeve connected to a rotating shaft. An mounting rod is fixedly connected to the outer wall of the rotating sleeve. The mounting rod has several insertion slots. The mounting mechanism also includes a clamping mechanism, which includes a mounting base. A limiting rod is provided at the top of the mounting base. The limiting rod is inserted into the insertion slot. The mounting base is fastened to the mounting rod through a nut seat.

[0010] Preferably, the clamping mechanism further includes a movable shaft disposed on the mounting base, two clamping rings symmetrically connected on the movable shaft, and a pressing rod connected to the outer side wall of the clamping ring.

[0011] Preferably, a rain-inducing bullet is inserted inside the clamping mechanism, and the clamping ring is semi-circular.

[0012] Preferably, the mounting rod is a strip-shaped metal rod, and the insertion slots are evenly distributed along the length of the mounting rod.

[0013] Preferably, the connection of the rotating shaft is provided with an angle scale for quantitatively displaying the pitch angle of the mounting rod.

[0014] Preferably, the connecting frame is rotatably connected to the outside of the base via a rotating seat, and the rotating shaft is rotatably connected to the rotating sleeve.

[0015] Preferably, the inner side of the clamping ring is provided with a rubber anti-slip pad for conforming to the outer wall of the rain-inducing bomb.

[0016] Compared with the prior art, the beneficial effects of this utility model are:

[0017] (1) By setting a rotating sleeve, mounting rod, insertion slot and limiting rod, this utility model enables the limiting rod to disengage from the mounting rod by rotating the nut seat when disassembling the launcher, thereby enabling the clamping mechanism to be disassembled as a whole on the mounting rod. This facilitates the disassembly of the clamping mechanism and realizes the modular assembly and disassembly of the clamping mechanism. This not only greatly reduces the transportation volume and improves portability, but also allows users to freely combine single or multiple launch arrays on the mounting rod according to mission requirements.

[0018] (2) The present invention, through the installation base, extrusion rod, clamping ring and movable shaft, enables the clamping ring and extrusion rod to be elastically connected, so that the clamping ring and movable shaft can perform elastic clamping operation on the rain enhancement bomb after rotation, and can adapt to rain enhancement bombs of different diameters, realizing rapid filling and reliable circumferential fastening, and improving the versatility of field operations. Attached Figure Description

[0019] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0020] Figure 2 This utility model Figure 1 A schematic diagram of the overall structure of the central adjustment mechanism;

[0021] Figure 3 This utility model Figure 1 Overall structural diagram of the installation mechanism;

[0022] Figure 4 This utility model Figure 3 A schematic diagram of the overall structure of the clamping mechanism.

[0023] In the diagram: 1. Base; 2. Adjustment mechanism; 201. Rotating seat; 202. Connecting frame; 203. Rotating shaft; 3. Mounting mechanism; 301. Rotating sleeve; 302. Mounting rod; 303. Insertion slot; 304. Limiting rod; 305. Nut seat; 4. Rain-inducing bullet; 5. Clamping mechanism; 501. Mounting seat; 502. Extrusion rod; 503. Clamping ring; 504. Movable shaft. Detailed Implementation

[0024] 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 of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0025] Example 1:

[0026] Please see Figures 1-4 As shown, a portable artificial rainmaking rocket stabilization launcher includes:

[0027] Base 1;

[0028] Adjustment mechanism 2 is installed above base 1. Adjustment mechanism 2 includes a rotating seat 201. A connecting frame 202 is fixedly connected to the top of the rotating seat 201. A rotating shaft 203 is provided on the outside of the connecting frame 202.

[0029] The mounting mechanism 3 is located outside the adjusting mechanism 2. The mounting mechanism 3 includes a rotating sleeve 301 connected to the rotating shaft 203. An installation rod 302 is fixedly connected to the outer wall of the rotating sleeve 301. The installation rod 302 is provided with several insertion slots 303. The mounting mechanism 3 is also provided with a clamping mechanism 5. The clamping mechanism 5 includes a mounting base 501. A limiting insertion rod 304 is provided at the top of the mounting base 501. The limiting insertion rod 304 is inserted into the insertion slot 303. The mounting base 501 is fastened to the installation rod 302 through a nut seat 305. The clamping mechanism 5 also includes a movable shaft 504 provided on the mounting base 501. Two clamping rings 503 are symmetrically connected on the movable shaft 504. A pressing rod 502 is connected to the outer wall of the clamping ring 503. A rain-inducing bullet 4 is inserted inside the clamping mechanism 5. The clamping ring 503 is semi-circular.

[0030] Specifically, the clamping mechanism 5 has a sturdy mounting base 501 at its bottom. A precision-machined limiting rod 304 extends vertically downwards from the bottom surface of the mounting base 501. During assembly, the operator first precisely aligns the limiting rod 304 with one of the multiple insertion slots 303 distributed at specific intervals on the mounting rod 302. By pressing vertically downwards, the limiting rod 304 is smoothly inserted into the insertion slot 303, thus achieving the initial positioning of the clamping mechanism 5 in the axial direction of the mounting rod 302 and the coarse adjustment in the height direction. When the operator rotates the nut seat 305 clockwise, its… The built-in threaded drive nut seat 305 moves along the threaded part towards the center of the mounting rod 302 until the end face of the nut seat 305 is tightly fitted with the lateral contact surface of the mounting base 501. Through the thread self-locking effect and the frictional resistance between the contact surfaces, the clamping mechanism 5 is rigidly locked on the mounting rod 302 in all directions, forming a stable mechanical connection. This not only ensures the positioning accuracy and structural stability of the clamping mechanism 5 during launch, but also realizes the quick assembly and disassembly function under the modular design, allowing operators to conveniently adjust the position and number configuration of the clamping mechanism 5 on the launcher according to different mission requirements.

[0031] As can be seen from the above, when the launcher needs to be disassembled, the operator only needs to rotate the nut seat 305, which uses its built-in threaded transmission mechanism to drive the limiting rod 304 to move axially, so that its end disengages from the preset installation limiting hole on the mounting rod 302, thereby releasing the mechanical lock on the clamping mechanism 5. This design allows the clamping mechanism 5 to be easily disassembled from the mounting rod 302 as a complete functional module, which not only greatly simplifies the disassembly and assembly process and avoids the tedious operation of disassembling each part one by one in the traditional structure, but also realizes the standardized and modular design concept of the clamping mechanism 5. This innovative structure not only allows the launcher to be disassembled but also... The overall volume of the frame is reduced to less than 60% of the original fixed design, significantly improving the individual soldier's carrying capacity and the efficiency of small vehicle transportation in complex terrain environments such as mountains and forests. It also gives users the ability to flexibly configure the system according to actual mission requirements. A single launch unit can be freely combined and installed on the same mounting pole 302 to meet the needs of precise fixed-point operations, or multiple launch units can be assembled at the same time to form a dense launch array to expand the catalytic coverage range. Thus, without sacrificing launch stability, it takes into account both the portability and mission adaptability of the equipment, providing a more efficient equipment solution for artificial rain enhancement operations under complex terrain conditions.

[0032] Example 2:

[0033] refer to Figure 3 and Figure 4As shown, the mounting rod 302 is a strip-shaped metal rod, the insertion slots 303 are evenly distributed along the length of the mounting rod 302, the connection of the rotating shaft 203 is provided with an angle scale for quantitatively displaying the pitch angle of the mounting rod 302, the connecting frame 202 is rotatably connected to the outside of the base 1 through the rotating seat 201, the rotating shaft 203 is rotatably connected to the rotating sleeve 301, and the inner side of the clamping ring 503 is provided with a rubber anti-slip pad for adhering to the outer wall of the rain-inducing bullet 4.

[0034] Specifically, the mounting rod 302 is made of high-strength aluminum alloy strip plate, and its upper surface is machined with several insertion slots 303 arranged in a linear array. This arrayed slot design provides multiple optional mounting positions for the clamping mechanism 5, allowing one or more rain-inducing bullets 4 to be flexibly arranged on the same mounting rod 302 according to the needs of the operation task.

[0035] As can be seen from the above, when it is necessary to load the rain-enhancing bullet 4, the squeezing rod 502 is operated to cause the two clamping rings 503 to open outward around the movable shaft 504. At this time, the rain-enhancing bullet 4 can be placed between the two clamping rings 503. After loading into place, the squeezing rod 502 is operated in the opposite direction to drive the two clamping rings 503 to close inward, so that the clamping rings 503 tightly abut against the surface of the rain-enhancing bullet 4 to achieve circumferential fastening.

[0036] For portable transport, multiple clamping mechanisms 5 can be pulled out from the mounting rod 302 by loosening the nut seat 305, and the mounting rod 302 can be pulled out from the rotating sleeve 301, achieving modular disassembly. The disassembled components are significantly smaller and can be categorized and stored in a backpack. During operation, according to the required cloud coverage area, the corresponding number of clamping mechanisms 5 are inserted into the mounting rod 302, the rotating seat 201 and the rotating shaft 203 are adjusted to a predetermined angle and locked, and then array-based stable launch can be performed.

[0037] All standard parts used in this invention can be purchased from the market, and irregularly shaped parts can be customized according to the description and drawings. The specific connection methods for each part all employ conventional methods such as bolts, rivets, and welding, which are mature technologies in the prior art. The machinery, parts, and equipment all use conventional models in the prior art, and the circuit connections also use conventional connection methods in the prior art, which will not be detailed here. Any content not described in detail in this specification belongs to the prior art known to those skilled in the art.

[0038] Although the present invention 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 the present invention should be included within the protection scope of the present invention.

Claims

1. A portable artificial rainmaking rocket launcher, characterized in that, include: Base (1); Adjustment mechanism (2), the adjustment mechanism (2) is installed above the base (1), the adjustment mechanism (2) includes a rotating seat (201), the top of the rotating seat (201) is fixedly connected to a connecting frame (202), and a rotating shaft (203) is provided on the outside of the connecting frame (202). The mounting mechanism (3) is located outside the adjustment mechanism (2). The mounting mechanism (3) includes a rotating sleeve (301) connected to the rotating shaft (203). An installation rod (302) is fixedly connected to the outer wall of the rotating sleeve (301). The installation rod (302) is provided with several insertion slots (303). The mounting mechanism (3) is also provided with a clamping mechanism (5). The clamping mechanism (5) includes a mounting seat (501). The top of the mounting seat (501) is provided with a limiting rod (304). The limiting rod (304) is inserted into the insertion slot (303). The mounting seat (501) is fastened to the mounting rod (302) through a nut seat (305).

2. The portable artificial rainmaking rocket stabilization launcher according to claim 1, characterized in that: The clamping mechanism (5) further includes a movable shaft (504) disposed on the mounting base (501), and two clamping rings (503) are symmetrically connected on the movable shaft (504). A pressing rod (502) is connected to the outer side wall of the clamping ring (503).

3. The portable artificial rainmaking rocket launcher according to claim 2, characterized in that: The clamping mechanism (5) is equipped with a rain-inducing bullet (4), and the clamping ring (503) is semi-circular.

4. The portable artificial rainmaking rocket stabilization launcher according to claim 1, characterized in that: The mounting rod (302) is a strip-shaped metal rod, and the insertion slots (303) are evenly distributed along the length of the mounting rod (302).

5. The portable artificial rainmaking rocket launcher according to claim 1, characterized in that: The connection of the rotating shaft (203) is provided with an angle scale for quantifying and displaying the pitch angle of the mounting rod (302).

6. The portable artificial rainmaking rocket launcher according to claim 1, characterized in that: The connecting frame (202) is rotatably connected to the outside of the base (1) via the rotating seat (201), and the rotating shaft (203) is rotatably connected to the rotating sleeve (301).

7. A portable artificial rainmaking rocket launcher according to claim 2, characterized in that: The inner side of the clamping ring (503) is provided with a rubber anti-slip pad for fitting the outer wall of the rain-inducing bullet (4).

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