CN219368553U

CN219368553U - Artificial hail-suppression rocket projectile information acquisition mechanism

Info

Publication number: CN219368553U
Application number: CN202223234598.XU
Authority: CN
Inventors: 沙修竹; 丁建芳
Original assignee: Individual
Current assignee: Individual
Priority date: 2022-12-01
Filing date: 2022-12-01
Publication date: 2023-07-18
Anticipated expiration: 2032-12-01

Abstract

The utility model relates to the technical field of artificial hail prevention rocket bullets, and particularly discloses an artificial hail prevention rocket bullet information acquisition mechanism which comprises a transmitting cylinder, a mounting plate, a base and a high-speed digital camera arranged on the transmitting cylinder, wherein the transmitting cylinder is integrally arranged into a cylindrical structure, one end of the transmitting cylinder is provided with a transmitting opening, and a transmitting assembly is arranged in the transmitting cylinder; annular connecting frames are respectively arranged at two ends of the transmitting cylinder, and the connecting frames are fixedly connected with the mounting plate; the mounting plate and the base are both in a strip-shaped structure, a sinking groove is formed in the base, and the mounting plate is arranged in the sinking groove; an angle adjusting component is arranged in the base, the angle adjusting structure drives the base to turn over, and the high-speed digital camera is connected with a controller; according to the information acquisition mechanism provided by the utility model, the transmitted picture is acquired by the high-speed digital camera for subsequent analysis and processing, and the transmitting angle of the transmitting cylinder is acquired by the angle adjusting structure.

Description

Artificial hail-suppression rocket projectile information acquisition mechanism

Technical Field

The utility model relates to the technical field of artificial hail prevention rocket projectiles, in particular to an artificial hail prevention rocket projectile information acquisition mechanism.

Background

In recent years, because human activities exacerbate the change of climate environment and disastrous weather frequently occurs, artificial weather is playing an increasingly important role in the fields of disaster prevention and reduction, ecological environment protection construction, important social activity guarantee and the like. At present, the artificial influence weather operation on the ground is to launch hail-suppression and rain-enhancement rocket bullets into target clouds to catalyze through a hail-suppression and rain-enhancement rocket launching device, so that the purposes of artificial precipitation and hail suppression are achieved. The hail-suppression and rain-enhancement rocket launching device consists of a rocket launching frame and a rocket launching controller and is divided into a ground fixed rocket launching device and a vehicle-mounted mobile rocket launching device.

The currently used hail-suppression and rain-enhancement rocket launching device has lower automation degree, most of the rocket launching device is operated manually, and the launching information of the rocket cannot be analyzed by collecting data; meanwhile, in the process of emission, the structure is easy to shake due to the emitted backseat force, so that the effect of emission is affected.

Disclosure of Invention

The utility model aims to provide an artificial hail-suppression rocket projectile information acquisition mechanism so as to solve the problems in the background technology.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the artificial hail-suppression rocket projectile information acquisition mechanism comprises a transmitting cylinder, a mounting seat, a base and a high-speed digital camera arranged on the transmitting cylinder, wherein the whole transmitting cylinder is of a cylindrical structure, a transmitting port is arranged at one end of the transmitting cylinder in an open manner, and a transmitting assembly is arranged in the transmitting cylinder; annular connecting frames are respectively arranged at two ends of the transmitting cylinder and fixedly connected with the mounting seat; the mounting seat and the base are both in a strip-shaped structure, a sinking groove is formed in the base, and the mounting seat is arranged in the sinking groove; the high-speed digital camera is characterized in that an angle adjusting assembly is arranged in the sinking groove of the base and drives the base to overturn, and the controller is connected with the high-speed digital camera.

Preferably, the angle adjusting assembly comprises a servo motor, the servo motor is fixed on a rotating frame on the side wall of the base, an adjusting block is arranged in the rotating frame, and the adjusting block is fixedly connected with a driving shaft of the servo motor; the mounting panel bottom is provided with the connecting block, the connecting block links to each other with the regulating block is fixed, servo motor is connected with the controller.

Preferably, a horizontal supporting belt is arranged in the base, and the supporting belt is arranged at one end far away from the servo motor.

Preferably, a fixed seat is arranged at the bottom of the base, a sleeve is arranged in the fixed seat through a rotating shaft, a telescopic rod is sleeved in the sleeve, and the end part of the telescopic rod is rotationally connected with a connecting seat at the bottom of the mounting seat; an electric push rod is arranged in the sleeve, the electric push rod is connected with the end part of the telescopic rod, and the electric push rod is electrically connected with the controller.

Preferably, the outside of high-speed digital camera is provided with the lantern ring, the lantern ring bottom is fixed each other with the link that is close to emitter one end through the bracing piece of metal.

Preferably, the connecting rod is arranged at the lower side of the connecting frame, the mounting seats are respectively arranged at two ends of the upper surface of the mounting seat, and the connecting rods are correspondingly arranged in the mounting seats and are connected with each other through pin shafts.

Compared with the prior art, the utility model has the beneficial effects that: according to the information acquisition mechanism provided by the utility model, the transmitted picture is acquired by the high-speed digital camera for subsequent analysis and processing, and the transmitting angle of the transmitting cylinder is acquired by the angle adjusting structure; simultaneously, still through setting up sleeve and telescopic link structure, utilize the electric push rod to provide the support to the churn to guarantee the stability of churn.

Drawings

FIG. 1 is a schematic diagram of the structure of the present utility model;

FIG. 2 is a schematic diagram of a mounting plate drive of the present utility model;

reference numerals in the drawings: 1. a launch canister; 11. an emission port; 12. a connecting frame; 13. a connecting rod; 2. a mounting plate; 21. a mounting base; 22. a connecting seat; 23. a connecting block; 3. a base; 31. a fixing seat; 32. a rotating frame; 33. an adjusting block; 34. a support belt; 4. a high-speed digital camera; 41. a collar; 5. a sleeve; 51. a telescopic rod; 6. a servo motor.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

In the description of the present utility model, it should be noted that the azimuth or positional relationship indicated by the terms "vertical", "upper", "lower", "horizontal", etc. are based on the azimuth or positional relationship shown in the drawings, and are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the apparatus or element referred to must have a specific azimuth, be constructed and operated in a specific azimuth, and thus should not be construed as limiting the present utility model.

In the description of the present utility model, it should also be noted that, unless explicitly specified and limited otherwise, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.

Referring to fig. 1-2, the present utility model provides a technical solution: the artificial hail suppression rocket projectile information acquisition mechanism comprises a transmitting cylinder 1, a mounting plate 2, a base 3 and a high-speed digital camera 4 arranged on the transmitting cylinder 1, wherein the whole transmitting cylinder 1 is of a cylindrical structure, one end of the transmitting cylinder is provided with a transmitting port 11, and a transmitting assembly is arranged in the transmitting cylinder; annular connecting frames 12 are respectively arranged at two ends of the transmitting cylinder 1, and the connecting frames 12 are fixedly connected with the mounting plate 2; the mounting plate 2 and the base 3 are both in a strip-shaped structure, a sinking groove is formed in the base 3, and the mounting plate 2 is arranged in the sinking groove; the angle adjusting assembly is arranged in the sinking groove of the base 3 and drives the base 3 to overturn, and the high-speed digital camera 4 is connected with the controller.

Further, the angle adjusting assembly comprises a servo motor 6, the servo motor 6 is fixed on a rotating frame 32 on the side wall of the base 3, an adjusting block 33 is installed in the rotating frame 32, and the adjusting block 33 is fixedly connected with a driving shaft of the servo motor 6; the mounting panel 2 bottom is provided with connecting block 23, connecting block 23 and regulating block 33 fixed link to each other, servo motor 6 is connected with the controller.

Further, a horizontal supporting belt 34 is disposed in the base 3, and the supporting belt 34 is disposed at an end far from the servo motor 6.

Further, a fixed seat 31 is arranged at the bottom of the base 3, a sleeve 5 is arranged in the fixed seat 31 through a rotating shaft, a telescopic rod 51 is sleeved in the sleeve 5, and the end part of the telescopic rod 51 is rotationally connected with a connecting seat 22 at the bottom of the mounting plate 2; an electric push rod is arranged in the sleeve 5 and is connected with the end part of the telescopic rod 51, and the electric push rod is electrically connected with the controller.

Further, a collar 41 is provided outside the high-speed digital camera 4, and the bottom end of the collar 41 is fixed with the connecting frame 12 near one end of the transmitting port 11 through a metal supporting rod.

Further, a connecting rod 13 is arranged at the lower side of the connecting frame 12, mounting seats 21 are respectively arranged at two ends of the upper surface of the mounting plate 2, and the connecting rods 13 are correspondingly arranged in the mounting seats 21 and are connected with each other through pin shafts.

Working principle: in the actual use process, the rocket projectile launching picture can be directly shot through the high-speed digital camera 4, the launched video picture is obtained, and the video picture is transmitted to the controller for subsequent use and analysis. The servo motor 6 is controlled by the controller to work so as to drive the adjusting block 33 to rotate, and the adjusting block 33 drives the connecting block 23 to rotate, so that the mounting plate 2 rotates along with the adjusting block; the turning angle of the mounting plate 2 is controlled by controlling the number of turns of the servo motor 6. During the overturning process of the mounting plate 2, the telescopic rod 51 can extend out of the sleeve 5, and the telescopic rod and the sleeve can respectively rotate around the fixed seat 31 and the connecting seat 22 to match the telescopic process; the telescopic rod 51 is connected with the electric push rod, and the electric push rod is controlled by the controller to support the telescopic rod 51, so that the telescopic rod 51 supports the bottom of the mounting plate 2, the stability of the telescopic rod is improved, and the backseat force in the launching process is reduced.

The supporting belt 34 can provide support when the mounting plate 2 is horizontally placed, so that the mounting plate is convenient to place; the transmitting cylinder 1 is arranged on the mounting seat 21 through the connecting rods 13 on the connecting frames 12 at the two ends, and the transmitting cylinder and the connecting rods can be detached and separated, so that the transmitting cylinder is convenient to overhaul, replace and use.

Notably, are: the whole device controls the realization of the device through the total control button, and because the equipment matched with the control button is common equipment, the device belongs to the prior art, and the electrical connection relation and the specific circuit structure of the device are not repeated here.

Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. Manual hail suppression rocket projectile information acquisition mechanism, its characterized in that: the high-speed digital camera shooting device comprises a shooting barrel (1), a mounting plate (2), a base (3) and a high-speed digital camera (4) arranged on the shooting barrel (1), wherein the shooting barrel (1) is integrally arranged into a cylindrical structure, a shooting port (11) is arranged at one end of the shooting barrel in an open manner, and a shooting assembly is arranged in the shooting barrel; annular connecting frames (12) are respectively arranged at two ends of the transmitting cylinder (1), and the connecting frames (12) are fixedly connected with the mounting plate (2); the mounting plate (2) and the base (3) are both in a strip-shaped structure, a sinking groove is formed in the base (3), and the mounting plate (2) is arranged in the sinking groove; the high-speed digital camera is characterized in that an angle adjusting assembly is arranged in the sinking groove of the base (3), the angle adjusting assembly drives the base (3) to overturn, and the high-speed digital camera (4) is connected with a controller.

2. The artificial hail suppression rocket projectile information acquisition mechanism of claim 1, wherein: the angle adjusting assembly comprises a servo motor (6), the servo motor (6) is fixed on a rotating frame (32) on the side wall of the base (3), an adjusting block (33) is arranged in the rotating frame (32), and the adjusting block (33) is fixedly connected with a driving shaft of the servo motor (6); the bottom of the mounting plate (2) is provided with a connecting block (23), the connecting block (23) is fixedly connected with an adjusting block (33), and the servo motor (6) is connected with a controller.

3. The artificial hail suppression rocket projectile information acquisition mechanism of claim 2, wherein: the base (3) is internally provided with a horizontal supporting belt (34), and the supporting belt (34) is arranged at one end far away from the servo motor (6).

4. The artificial hail suppression rocket projectile information acquisition mechanism of claim 1, wherein: the bottom of the base (3) is provided with a fixed seat (31), a sleeve (5) is arranged in the fixed seat (31) through a rotating shaft, a telescopic rod (51) is sleeved in the sleeve (5), and the end part of the telescopic rod (51) is rotationally connected with a connecting seat (22) at the bottom of the mounting plate (2); an electric push rod is arranged in the sleeve (5), the electric push rod is connected with the end part of the telescopic rod (51), and the electric push rod is electrically connected with the controller.

5. The artificial hail suppression rocket projectile information acquisition mechanism of claim 1, wherein: the high-speed digital camera (4) is externally provided with a lantern ring (41), and the bottom end of the lantern ring (41) is mutually fixed with a connecting frame (12) close to one end of the transmitting port (11) through a metal supporting rod.

6. The artificial hail suppression rocket projectile information acquisition mechanism of claim 1, wherein: connecting rods (13) are arranged on the lower side of the connecting frame (12), mounting seats (21) are respectively arranged at two ends of the upper surface of the mounting plate (2), and the connecting rods (13) are correspondingly arranged in the mounting seats (21) and are connected with each other through pin shafts.