An artificial weather jamming device

Abstract

This invention provides an artificial weather jamming device, including a launching body and a cluster cabin disposed on the launching body; the cluster cabin is provided with an installation and adjustment mechanism, and a plurality of sub-launchers are disposed on the installation and adjustment mechanism; wherein, the installation and adjustment mechanism includes: a main shaft disposed in the cluster cabin; a first adjustment group and a second adjustment group respectively disposed at both ends of the main shaft, and the plurality of sub-launchers are disposed on the first adjustment group and the second adjustment group; and a catapult device disposed on the main shaft and positioned between the first adjustment group and the second adjustment group; the artificial weather jamming device proposed in this invention can launch multiple sub-launchers simultaneously after a single launch, ensuring that a sufficient area can be reached after a single launch; avoiding multiple launches in the prior art, thereby reducing the launch difficulty and risk factor while saving manpower and time costs.

Description

Technical Field

[0001] This utility model relates to the field of weather interference device technology, and in particular to an artificial weather interference device. Background Technology

[0002] Artificial weather modification rockets are widely used in current human activities to intervene in meteorology, bringing many benefits to human society. Their basic principle is to disperse catalysts such as silver iodide and dry ice in the clouds, so that the clouds can condense faster under the action of the catalyst to form rainfall, thereby achieving the purpose of artificial rain, cooling and cloud dispersal.

[0003] In existing technologies, single rockets are commonly used to disperse artificial catalysts. However, as society's demand for weather intervention increases, higher requirements will inevitably be placed on the effectiveness of weather intervention. In recent years, some regions have failed to achieve the expected results in implementing weather modification. Therefore, more effective rocket technologies for weather modification are needed to improve the capabilities and effectiveness of weather modification.

[0004] Due to the low efficiency of existing rockets, they cannot achieve the desired effects in weather modification. Specifically, the total amount of dry ice, silver iodide, and other catalysts carried by a single rocket is limited, making it difficult to produce significant effects in large-scale or severe convective weather. At the same time, the catalyst dispersion area of ​​a single rocket is relatively concentrated, usually only affecting local cloud layers and failing to effectively impact large cloud systems. Furthermore, the insufficient efficiency of a single rocket means that multiple launches are required to achieve the desired effect, resulting in excessively high costs per unit area and low overall efficiency.

[0005] To address the aforementioned issues, existing technologies require multiple rocket launches; however, multiple launches increase the difficulty and risk of launches, as well as the costs of manpower, resources, and time. Utility Model Content

[0006] The purpose of this invention is to provide an artificial weather interference device that can solve the above-mentioned technical problems.

[0007] This utility model provides an artificial weather interference device, comprising:

[0008] The launch vehicle and the cluster module mounted on the launch vehicle;

[0009] The cluster cabin is equipped with an installation and adjustment mechanism, on which several sub-launchers are mounted; during use, the angles of the sub-launchers are adjusted through the installation and adjustment mechanism.

[0010] The installation and adjustment mechanism includes: a main shaft, which is installed inside the cluster compartment; a first adjustment group and a second adjustment group, which are respectively installed at both ends of the main shaft, and several sub-launchers are installed on the first adjustment group and the second adjustment group; and a catapult device, which is installed on the main shaft and positioned between the first adjustment group and the second adjustment group.

[0011] As a further technical solution, a linkage rod is provided between the first adjustment group and the second adjustment group.

[0012] As a further technical solution, the first adjustment group includes:

[0013] The first fixed plate is located at one end of the spindle;

[0014] Several first main rods, one end of which is set on a first fixed plate, and the other end of which is connected to one end of several first support rods respectively;

[0015] The other end of each of the first support rods is connected to a first drive device mounted on the main shaft.

[0016] As a further technical solution, the first adjustment group also includes:

[0017] Several first auxiliary rods are connected at one end to several first main rods, and at the other end to a first drive device.

[0018] As a further technical solution, one end of several first support rods is connected to several first main rods via first locking pins.

[0019] As a further technical solution, the first driving device includes:

[0020] A first actuating cylinder is mounted on the main shaft; and a first inner actuating body is disposed inside the first actuating cylinder.

[0021] The first external actuator is disposed outside the first actuator cylinder and connected to the first internal actuator via a first connecting rod; and the other ends of several first support rods are disposed on the first external actuator.

[0022] As a further technical solution, the second adjustment group includes:

[0023] The second fixed plate is located at one end of the spindle;

[0024] Several second main rods, one end of which is set on the second fixed plate, and the other end of which is connected to one end of several second support rods respectively;

[0025] The other end of several second support rods is connected to a second drive device mounted on the main shaft.

[0026] As a further technical solution, the second adjustment group also includes:

[0027] Several second auxiliary rods are connected at one end to several first main rods, and at the other end to a second drive device.

[0028] As a further technical solution, one end of several second support rods is connected to several second main rods via second locking pins.

[0029] As a further technical solution, the second driving device includes:

[0030] The second action cylinder is mounted on the main shaft; and a second inner action body is installed inside the second action cylinder.

[0031] The second external actuator is located outside the second actuator cylinder and is connected to the second internal actuator via a second connecting rod; and the other ends of several second support rods are all located on the second external actuator.

[0032] The technical solution of this utility model involves setting an installation and adjustment mechanism inside the cluster compartment on the launch body, and setting several sub-launchers on the installation and adjustment mechanism. During use, by controlling the first and second adjustment groups on the installation and adjustment mechanism, the angles of the several sub-launchers set thereon are changed, and the several sub-launchers are launched to predetermined positions by a catapult device. The sub-launchers are launched after being carried by the launch body to the designated position. Compared with the prior art, the technical solution of this utility model can launch multiple sub-launchers simultaneously after one launch, ensuring that a sufficient area can be reached after one launch. It avoids the multiple launches required in the prior art, thereby reducing the launch difficulty and risk factor while saving manpower and time costs. Attached Figure Description

[0033] To more clearly illustrate the specific embodiments of this utility model or the technical solutions in the prior art, the drawings used in the description of the specific embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are some embodiments of this utility model. For those skilled in the art, other drawings can be obtained from these drawings without creative effort.

[0034] Figure 1 This is a schematic diagram of the mechanism of an artificial weather interference device according to the present invention;

[0035] Figure 2 This is an enlarged schematic diagram of the internal structure of the cluster compartment in this utility model.

[0036] Explanation of reference numerals in the attached figures:

[0037] 100-Launch body; 101-Power module; 102-Guidance module; 200-Cluster module; 301-Main shaft; 302-First adjustment group; 321-First fixing plate; 322-First main rod; 323-First support rod; 324-First drive device; 3241-First actuating cylinder; 3242-First inner actuating body; 3243-First outer actuating body; 3244-First connecting rod; 325-First auxiliary rod; 326-First locking pin; 3 03-Second Adjustment Group; 331-Second Fixed Plate; 332-Second Main Rod; 333-Second Support Rod; 334-Second Drive Device; 3341-Second Actuating Cylinder; 3342-Second Inner Actuating Body; 3343-Second Outer Actuating Body; 3344-Second Connecting Rod; 335-Second Auxiliary Rod; 336-Second Locking Pin; 304-Ejection Device; 341-Ignition Tube; 342-Ejection Medium; 305-Linkage Rod; 400-Sub-launcher. Detailed Implementation

[0038] The technical solution of this utility model will be clearly and completely described below with reference to the embodiments. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of this utility model.

[0039] In the description of this utility model, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", etc., indicating the orientation or positional relationship are based on the orientation or positional relationship shown in the accompanying drawings, and are only for the convenience of describing this utility model and simplifying the description, and are not intended to indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model.

[0040] Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more features. In the description of this utility model, "a plurality of" means two or more, unless otherwise explicitly specified. Furthermore, the terms "installed," "connected," and "linked" should be interpreted broadly; for example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0041] like Figure 1-2 As shown, the present invention proposes an artificial weather interference device, comprising:

[0042] The cluster capsule 200 is equipped with an installation and adjustment mechanism, on which several sub-launchers 400 are mounted. During use, the angles of the sub-launchers 400 are adjusted by the installation and adjustment mechanism. Specifically, the installation and adjustment mechanism can operate within the cluster capsule 200 and change the angles of the sub-launchers 400 during the operation, so that the sub-launchers 400 are at a set angle after adjustment. After ignition, the sub-launchers 400 separate from the installation and adjustment mechanism and fly to a set position, where they disperse catalysts such as silver iodide or dry ice through explosion or spraying. It should be noted that the set angle varies depending on different launch requirements, and the specific angle shall prevail. This utility model will not provide further details.

[0043] In addition, at least two doors are provided on the cluster cabin 200 that can be opened before the installation and adjustment mechanism is activated, so that several sub-launchers 400 are in an unobstructed state; in this way, several sub-launchers 400 can be launched to the designated position without obstruction under the action of the installation and adjustment mechanism; the preferred door is the prior art, and the opening and other structures are also the prior art, which will not be further described.

[0044] It should be noted that the launch body 100 is equipped with a power module 101 and a guidance module 102, which are respectively located at both ends of the cluster module 200. The power module 101 provides lift-off power, and the guidance module 102 controls the flight path to ensure accuracy. The door opening structure is connected to the guidance module 102 via wires, and the door opening and closing is controlled by the guidance module 102 during use. In this utility model, preferably, the power module 101 and the guidance module 102 are existing technologies, and will not be further described here.

[0045] The installation and adjustment mechanism includes: a main shaft 301 disposed within the cluster compartment 200; a first adjustment group 302 and a second adjustment group 303 respectively disposed at both ends of the main shaft 301, and several sub-launchers 400 disposed on the first adjustment group 302 and the second adjustment group 303; an ejection device 304 disposed on the main shaft 301 and positioned between the first adjustment group 302 and the second adjustment group 303; during use, the ejection device 304 is activated, which drives the first adjustment group 302 and the second adjustment group 303 to move, and drives several sub-launchers 400 to move simultaneously. After the several sub-launchers 400 move, the guidance compartment 102 controls the several sub-launchers 400 to launch, and at the same time as the several sub-launchers 400 are launched, the first adjustment group 302 and the second adjustment group 303 separate from the several sub-launchers 400.

[0046] The technical solution of this utility model involves setting an installation and adjustment mechanism within the cluster compartment 200 on the launch body 100, and setting a plurality of sub-launchers 400 on the installation and adjustment mechanism. During use, the angles of the plurality of sub-launchers 400 are changed by controlling the first adjustment group 302 and the second adjustment group 303 on the installation and adjustment mechanism, and the plurality of sub-launchers 400 are launched to a predetermined position by the ejection device 304. The sub-launchers 400 are launched after the launch body 100 flies to the designated position. Compared with the prior art, the technical solution of this utility model can launch multiple sub-launchers 400 simultaneously after one launch, ensuring that a sufficient area can be reached after one launch. It avoids the multiple launches in the prior art, thereby reducing the launch difficulty and risk factor while saving manpower and time costs.

[0047] like Figure 2 As shown, a linkage rod 305 is provided between the first adjustment group 302 and the second adjustment group 303; this allows the first adjustment group 302 to drive the second adjustment group 303 to move when the first adjustment group 302 and the second adjustment group 303 are activated. Of course, a catapult device 304 can also be provided at the bottom of the second adjustment group 303. Through the cooperation of the two catapult devices 304, the first adjustment group 302 and the second adjustment group 303 can be operated respectively, ensuring that the first adjustment group 302 and the second adjustment group 303 can be controlled separately during operation, thereby improving the flexibility of operation. Specifically, the angles of the first adjustment group 302 and the second adjustment group after the adjustment action can be controlled by the two catapult devices 304 respectively, thereby better adjusting the angles of the sub-launchers 400.

[0048] like Figure 2As shown, the first adjustment group 302 includes a first fixed plate 321 and a plurality of first main rods 322. The first fixed plate 321 is disposed at one end of the main shaft 301 and is fixedly connected to one end of the main shaft 301. One end of each of the plurality of first main rods 322 is disposed on the first fixed plate 321, and the other end is respectively connected to one end of a plurality of first support rods 323. One end of each of the plurality of first main rods 322 is rotatably connected to the first fixed plate 321, so that during the operation phase, the plurality of first main rods 322 can rotate on the first fixed plate 321. The other ends of each of the plurality of first support rods 323 are connected to a first drive device 324 disposed on the main shaft 301. During use, under the action of the ejection device 304, the first drive device 324 is activated. The first driving device 324 drives several first main rods 322 to move, and when the several first main rods 322 move, the other end of the several first main rods 322 separates from the several first support rods 323. In this way, under the action of the first driving device 324, the several first main rods 322 rotate around the connection position with the first fixed plate 321 as the axis. Specifically, several first auxiliary rods 325 are also provided. One end of each of the several first auxiliary rods 325 is connected to the several first main rods 322, and the other end is connected to the first driving device 324. In this way, under the push of the first driving device 324, the several first auxiliary rods 325 respectively push the several first main rods 322 to rotate, and the several first main rods 322 drive the several sub-launchers 400 to change their angle.

[0049] In this configuration, one end of several first support rods 323 is connected to several first main rods 322 via first locking pins 326. These first locking pins 326 are electronic and connected to the guidance cabin 102. The guidance cabin 102 can control the opening of the first locking pins 326, thus opening them when the first drive device 324 is activated. Because they are electronic, they can be released quickly, separating the first support rods 323 from the first main rods 322. It should be noted that a mechanical locking pin for mounting the sub-launcher 400 is also provided on the first locking pin 326. After the first support rods 323 and the first main rods 322 separate, the first locking pin 326 is placed on the first main rods 322, and the sub-launcher 400 moves simultaneously with the first main rods 322 via the mechanical locking pin. When a certain angle is reached, the locking block in the mechanical locking pin separates from the sliding groove, completing the separation between the sub-launcher 400 and the first main rod 322.

[0050] The first driving device 324 includes: a first actuating cylinder 3241, a first inner actuating body 3242, and a first outer actuating body 3243; the first actuating cylinder 3241 is disposed on the main shaft 301; and the first inner actuating body 3242 is disposed inside the first actuating cylinder 3241; the first outer actuating body 3243 is disposed outside the first actuating cylinder 3241 and is connected to the first inner actuating body 3242 through a first connecting rod 3244; and the other ends of a plurality of first support rods 323 are disposed on the first outer actuating body 3243. In actual use, the first inner moving body 3242 moves linearly within the first moving cylinder 3241 via the ejection device 304. Since the first inner moving body 3242 and the first outer moving body 3243 are connected by the first connecting rod, the first inner moving body 3242 can drive the first outer moving body 3243 to move simultaneously when it moves. The first outer moving body 3243 can also drive the movement of several first auxiliary rods 325, thereby changing the angle of several sub-launchers 400 after the rotation of several first main rods 322.

[0051] like Figure 2As shown, the second adjustment group 303 includes a second fixed disk 331 and a plurality of second main rods 332. The second fixed disk 331 is disposed at one end of the main shaft 301. One end of each of the plurality of second main rods 332 is disposed on the second fixed disk 331, and the other end is respectively connected to one end of a plurality of second support rods 333. The other end of each of the plurality of second support rods 333 is connected to a second drive device 334 disposed on the main shaft 301. In actual use, the second drive device 334 drives the second main rods 332 to rotate on the second fixed disk 331, and the rotation of the second main rods 332 changes the angle of a plurality of sub-launchers 400. Each of the plurality of second auxiliary rods 335 has one end connected to a plurality of first main rods 322, and the other end connected to the second drive device 334. When the second drive device 334 is activated, it drives the plurality of second auxiliary rods 335 to move, and the plurality of second auxiliary rods 335 drive the plurality of second main rods 332 to rotate, thereby adjusting the angle of the plurality of sub-launchers 400. 0-degree angle adjustment; specifically, one end of several second support rods 333 is connected to several second main rods 332 via second locking pins 336; in this utility model, the second locking pins 336 are electronic locking pins and are connected to the guidance cabin 102. When the second drive device 334 is activated, the second locking pins 336 are disconnected by the guidance cabin 102; due to the use of electronic locking pins, they can be released in a short time, realizing the disconnection between the second support rods 333 and the second main rods 332; it should be noted that a mechanical locking pin for installing the sub-launcher 400 is also provided on the second locking pins 336; after the second support rods 333 and the second main rods 332 are separated, the second locking pins 336 are placed on the second main rods 332, and the sub-launcher 400 moves simultaneously with the second main rods 332 through the mechanical locking pins; when a certain angle is reached, the locking block in the mechanical locking pin separates from the slide groove, completing the separation between the sub-launcher 400 and the second main rods 332;

[0052] Additionally, the second drive device 334 includes a second actuating cylinder 3341 and a second outer actuating body 3343. The second actuating cylinder 3341 is mounted on the main shaft 301; a second inner actuating body 3342 is disposed inside the second actuating cylinder 3341; the second outer actuating body 3343 is disposed outside the second actuating cylinder 3341 and connected to the second inner actuating body 3342 via a second connecting rod 3344; and the other ends of several second support rods 333 are all disposed on the second outer actuating body 3343. In this invention, the second outer actuating body 3343 and the first outer actuating body 3243 can be connected via a linkage rod 305 and via an ejection device 30. After the first internal action device is driven, the second external action device 3343 will move simultaneously when the first external action body 3243 moves. The linkage rod 305 can also be disassembled. The first drive device 324 and the second drive device 334 are driven by the two ejection devices 304 respectively. In this way, by setting the ejection device 304, the action distance of the first drive device 324 and the second drive device 334 can be adjusted, thereby controlling the rotation angle of the first main rod 322 and the second main rod 332. This allows the upper and lower parts of the sub-launchers 400 to be adjusted to different angles, thereby achieving precise control of the angle of the sub-launchers 400.

[0053] It should be noted that in this utility model, the ejection device 304 includes an ignition tube 341 and an ejection medium 342. The ignition tube 341 is respectively disposed at the bottom of the first actuating cylinder 3241 and the second actuating cylinder 3341, and both the first actuating cylinder 3241 and the second actuating cylinder 3341 are filled with the ejection medium 342. During adjustment, the ignition tube 341 is ignited by the guidance chamber 102, so that the ejection medium 342 is burned, and the first inner actuating body 3242 and the second inner actuating body 3342 move in the first actuating cylinder 3241 and the second actuating cylinder 3341 respectively, thereby driving the first outer actuating body 3243 and the second outer actuating body 3343 to perform actions respectively. The preferred ejection medium 342 is gas.

[0054] When the ejection device 304 is activated, the first main rod 322 and the second main rod 332 can be activated simultaneously via the linkage rod 305; and the sub-launchers 400 on the first main rod 322 and the second main rod 332 can be rapidly ejected, thereby enabling the sub-launchers 400 to acquire initial velocity and creating a certain distance between the sub-launchers 400 and the cluster cabin 200 after being ejected; and ignition is performed 1-2 seconds after the sub-launchers 400 are ejected, and they fly to the set position after ignition.

[0055] After the angles of several sub-launchers 400 are adjusted, under the control of the guidance cabin 102, the several sub-launchers 400 are launched. At the same time as the several sub-launchers 400 are launched, the locking pins on several first main rods 322 and several second main rods 332 are opened by the guidance cabin 102, so that the several sub-launchers 400 are separated from the several first main rods 322 and several second main rods 332, thus completing the launch operation of several sub-launchers 400. Of course, different numbers of sub-launchers 400 can be set according to the size of the cluster cabin 200. In this utility model, it is preferred to set 6 sub-launchers 400. At the same time, the number of first main rods 322, second main rods 332, first support rods 323, second support rods 333, first auxiliary rods 325 and second auxiliary rods 335 are all 6.

[0056] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of this utility model, and are not intended to limit it. Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some or all of the technical features therein. Such modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of this utility model.

Claims

1. An artificial weather interference device, characterized in that, include: Launching main body (100) and cluster compartment (200) disposed on the launching main body (100); The cluster compartment (200) is provided with an installation and adjustment mechanism, and a number of sub-electrodes (400) are mounted on the installation and adjustment mechanism; during use, the angles of the sub-electrodes (400) are adjusted by the installation and adjustment mechanism. The installation and adjustment mechanism includes: a main shaft (301) disposed within the cluster compartment (200); a first adjustment group (302) and a second adjustment group (303) disposed at both ends of the main shaft (301), and a plurality of sub-launchers (400) disposed on the first adjustment group (302) and the second adjustment group (303); and a catapult device (304) disposed on the main shaft (301) and positioned between the first adjustment group (302) and the second adjustment group (303).

2. The artificial weather interference device according to claim 1, characterized in that, A linkage rod (305) is provided between the first adjustment group (302) and the second adjustment group (303).

3. The artificial weather interference device according to claim 1, characterized in that, The first adjustment group (302) includes: The first fixed plate (321) is disposed at one end of the main shaft (301); A plurality of first main rods (322) are respectively mounted on the first fixed plate (321) at one end and connected to one end of a plurality of first support rods (323) at the other end; The other end of each of the first support rods (323) is connected to a first drive device (324) mounted on the main shaft (301).

4. The artificial weather interference device according to claim 3, characterized in that, The first adjustment group (302) also includes: Several first auxiliary rods (325) are connected at one end to several first main rods (322) and at the other end to the first drive device (324).

5. The artificial weather interference device according to claim 4, characterized in that, One end of one of the first support rods (323) is connected to one of the first main rods (322) via a first locking pin (326).

6. The artificial weather interference device according to claim 3, characterized in that, The first drive device (324) includes: A first action cylinder (3241) is disposed on the main shaft (301); and a first inner action body (3242) is disposed inside the first action cylinder (3241); The first external actuator (3243) is disposed outside the first actuator cylinder (3241) and connected to the first internal actuator (3242) via the first connecting rod (3244); and the other ends of several first support rods (323) are disposed on the first external actuator (3243).

7. The artificial weather interference device according to claim 1, characterized in that, The second adjustment group (303) includes: The second fixed plate (331) is disposed at one end of the main shaft (301); Several second main rods (332) are mounted on the second fixed plate (331) at one end, and the other end is connected to one end of several second support rods (333); The other end of several of the second support rods (333) is connected to a second drive device (334) mounted on the main shaft (301).

8. The artificial weather interference device according to claim 7, characterized in that, The second adjustment group (303) also includes: Several second auxiliary rods (335) are connected at one end to several first main rods (322) and at the other end to the second drive device (334).

9. The artificial weather interference device according to claim 8, characterized in that, One end of one of the second support rods (333) is connected to one of the second main rods (332) via a second locking pin (336).

10. The artificial weather interference device according to claim 7, characterized in that, The second drive unit (334) includes: A second action cylinder (3341) is disposed on the main shaft (301); and a second inner action body (3342) is disposed inside the second action cylinder (3341); The second external actuator (3343) is disposed outside the second actuator cylinder (3341) and connected to the second internal actuator (3342) via the second connecting rod (3344); and the other ends of several second support rods (333) are disposed on the second external actuator (3343).

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