Vehicle-mounted intelligent rocket launcher for weather modification

Abstract

The utility model discloses a vehicle-mounted artificial weather rocket intelligent launcher which comprises a launcher body capable of being installed on an operation vehicle and a remote self-locking assembly arranged on the surface of the launcher body. The remote self-locking assembly can receive signals from a headquarters in real time under the action of the main control unit and the wireless signal receiving and transmitting unit in the remote self-locking assembly, and controls the power device to drive the traction piece to move after the signals that the headquarters can launch rockets are obtained, so that the traction piece drives the plugging plate to move, and the remote self-locking assembly can launch the rockets in real time. The channel opening in the rocket mounting frame is exposed, an operator can load the rocket into the launcher at the moment, ignition and angle adjustment of the rocket are controlled by the control unit, the operator does not need to judge by himself, and overall operation is more accurate and faster.

Description

Technical Field

[0001] The utility model relates to the technical field of human shadow equipment, in particular to a vehicle-mounted artificial weather modification rocket intelligent launch stand. Background Art

[0002] Artificial weather modification rockets are a technology that uses rockets to launch relevant reagents into the clouds, causing small water droplets in the clouds to quickly combine with each other and thus achieve rapid rainfall. Common artificial weather modification rockets must be launched from a vehicle-mounted launcher. The operator can only continue to launch after the work vehicle is driven to the appropriate location according to the weather conditions of the day, so as to ensure the specific effect of artificial weather modification.

[0003] During the launch of the human shadow rocket, the launch site needs to be surveyed in advance, and the cloud layer, wind speed and ground environment are all uncontrollable to a certain extent. Therefore, the operators are required to follow the instructions of the headquarters and constantly change their positions. However, in the actual operation process, most of the time, the operators can only take the initiative to establish contact with the headquarters. When the operators are inexperienced and the weather conditions change, it is easy for the communication to be untimely and the rocket to be launched at an inappropriate location due to errors, which will affect the effect of artificial rainfall. Utility Model Content

[0004] In order to solve the above problems, the utility model provides the following technical solutions:

[0005] A vehicle-mounted artificial weather modification rocket intelligent launcher, comprising:

[0006] The launcher body includes a main frame, a rocket mounting frame arranged on the surface of the main frame, and an adjustment mechanism connecting the rocket mounting frame and the main frame, wherein the rocket mounting frame is provided with a passage for loading the meteorological rocket;

[0007] A remote self-locking assembly, comprising a protective shell disposed on the surface of a rocket mounting frame, a connecting mechanism capable of mounting the protective shell on the surface of a launch frame body, a self-locking portion disposed on the surface of the protective shell, and a main control unit disposed inside the protective shell, wherein the main control unit is capable of controlling an electronic unit in the remote self-locking assembly;

[0008] The surface of the protective shell is provided with a wireless signal transceiver unit, which is connected to the main control unit. The main control unit can control the activity of the self-locking part to block the rocket channel exit on the surface of the launcher body.

[0009] On the basis of the above technical solution, the present invention can also be improved as follows.

[0010] Furthermore, a control unit capable of controlling the adjustment mechanism is provided on the surface of the main frame, and the control unit can be connected to an external operation panel.

[0011] Furthermore, a voice broadcast module connected to the control unit and the main control unit is provided on the surface of the main frame, and the voice broadcast module can play corresponding voice according to the operation of the command center.

[0012] Furthermore, the self-locking part includes a blocking plate arranged on the surface of the rocket mounting frame, and a movable mechanism arranged on the surface of the protective shell and capable of controlling the movement of the blocking plate, and the blocking plate can block the channel outlet on the surface of the rocket mounting frame.

[0013] Furthermore, a support member for supporting a movable mechanism is provided on the surface of the protective shell, and the movable mechanism includes a movable shaft provided on the surface of the support member, a traction member provided on the surface of the movable shaft, and a power device capable of driving the traction member to move, and the traction member can drive the sealing plate to move.

[0014] Furthermore, the surface of the rocket mounting frame is provided with a movable track for the sealing plate to move inside it.

[0015] Furthermore, the traction member is a gear-shaped structure, and the surface of the blocking plate is provided with teeth and grooves adapted to the traction member.

[0016] Furthermore, a limiting piece is provided on the surface of the blocking plate to limit its movement from the inside of the movable track to the outside of the movable track, and a movable groove adapted to the limiting piece is provided inside the movable track.

[0017] Furthermore, the protective shell is arranged at the bottom of the rocket mounting frame, and the blocking plate is located at the bottom of the rocket mounting frame when the passage of the rocket mounting frame is not blocked.

[0018] Furthermore, the support member can be removed from the surface of the protective shell together with the traction member and the power device.

[0019] Beneficial Effects

[0020] Compared with the prior art, the utility model, through the remote self-locking component, can receive signals from the headquarters in real time under the action of its internal main control unit and wireless signal transceiver unit. After obtaining the signal from the headquarters that the rocket can be launched, the power device is controlled to drive the traction part to move, and then the traction part drives the blocking plate to move, so that the channel opening on the rocket mounting frame is exposed. The operator can then load the rocket into the launch frame, and the control unit will control the ignition of the rocket and the adjustment of the angle, without the need for the operator to make judgments by themselves, and the overall operation is more accurate and quick. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] In order to more clearly illustrate the technical solutions of the embodiments of the utility model, the drawings required for describing the embodiments are briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0022] Figure 1 It is a schematic diagram of the front section structure of the utility model;

[0023] Figure 2 It is a schematic diagram of the utility model's top-down section structure;

[0024] Figure 3 It is a three-dimensional structural diagram of the passageway exit and track of the utility model rocket mounting frame;

[0025] Figure 4 It is a three-dimensional structural schematic diagram of the utility model plugging plate;

[0026] Figure 5 for Figure 1 The enlarged structural diagram at A in the middle;

[0027] Figure 6 for Figure 1 The enlarged structural diagram at B in the middle;

[0028] In the accompanying drawings, the components represented by the reference numerals are listed as follows:

[0029] 1. Launching frame body; 11. Main frame; 12. Rocket mounting frame; 13. Adjustment mechanism; 2. Remote self-locking assembly; 21. Protective shell; 22. Connecting mechanism; 23. Self-locking part; 231. Sealing plate; 232. Support member; 233. Movable shaft; 234. Traction member; 235. Power unit. DETAILED DESCRIPTION

[0030] In order to facilitate the understanding of the present invention, the present invention will be described more fully below with reference to the relevant drawings. Several embodiments of the present invention are given in the drawings. However, the present invention can be implemented in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the present invention more thorough and comprehensive.

[0031] It should be noted that when an element is referred to as being "fixed to" another element, it may be directly on the other element or there may be a central element. When an element is considered to be "connected to" another element, it may be directly connected to the other element or there may be a central element at the same time. The terms "vertical", "horizontal", "left", "right" and similar expressions used herein are for illustrative purposes only.

[0032] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as those commonly understood by those skilled in the art in the technical field of the present invention. The terms used herein in the specification of the present invention are only for the purpose of describing specific embodiments and are not intended to limit the present invention. The term "and / or" used herein includes any and all combinations of one or more related listed items.

[0033] It should be noted that similar reference numerals and letters denote similar items in the following drawings, and therefore, once an item is defined in one drawing, further definition and explanation thereof is not required in subsequent drawings.

[0034] In addition, the terms "horizontal", "vertical", "overhanging" and the like do not mean that the components are required to be absolutely horizontal or overhanging, but can be slightly tilted. For example, "horizontal" only means that its direction is more horizontal than "vertical", and does not mean that the structure must be completely horizontal, but can be slightly tilted.

[0035] See also Figure 1-6 A vehicle-mounted artificial weather modification rocket intelligent launcher includes a launcher body 1 that can be installed on a work vehicle, and a remote self-locking component 2 arranged on the surface of the launcher body 1.

[0036] Among them, the launcher body 1 is a common structure in the existing human shadow rocket launcher, which includes a main frame body 11, a rocket mounting frame 12 arranged on the surface of the main frame body 11, and an adjustment mechanism 13 connecting the rocket mounting frame 12 and the main frame body 11. The rocket mounting frame 12 is provided with a channel inside for loading meteorological rockets.

[0037] The remote self-locking component 2 includes a protective shell 21 arranged on the surface of the rocket mounting frame 12, a connecting mechanism 22 capable of installing the protective shell 21 on the surface of the launch frame body 1, a self-locking part 23 arranged on the surface of the protective shell 21, and a main control unit arranged inside the protective shell 21. The main control unit can control the electronic unit in the remote self-locking component 2. A wireless signal transceiver unit is provided on the surface of the protective shell 21, which is connected to the main control unit. The main control unit can control the activity of the self-locking part 23 to block the rocket channel exit on the surface of the launch frame body 1.

[0038] Taking into account the remote control of the main frame 11 and the on-site control of the operators, a control unit capable of controlling the adjustment mechanism 13 is provided on the surface of the main frame 11, and the control unit can be connected to an external operation panel. A voice broadcast module connected to the control unit and the main control unit is provided on the surface of the main frame 11, and the voice broadcast module can play corresponding voice according to the operation of the command center.

[0039] Specifically, the self-locking part 23 includes a blocking plate 231 arranged on the surface of the rocket mounting frame 12, and a movable mechanism arranged on the surface of the protective shell 21 and capable of controlling the movement of the blocking plate 231. The blocking plate 231 can block the channel outlet on the surface of the rocket mounting frame 12, and the surface of the protective shell 21 is provided with a support member 232 for supporting the movable mechanism. The movable mechanism includes a movable shaft 233 arranged on the surface of the support member 232, a traction member 234 arranged on the surface of the movable shaft 233, and a power device 235 capable of driving the traction member 234 to move. The traction member 234 can drive the blocking plate 231 to move.

[0040] See also Figure 1 The surface of the rocket mounting frame 12 is provided with a movable track for the blocking plate 231 to move inside it, and the traction member 234 is a gear-like structure. The surface of the blocking plate 231 is provided with a tooth groove adapted to the traction member 234. The power device 235 can be a common motor structure, which can drive the traction member 234 to move through its rotation, so that the blocking plate 231 can move in a straight line, and through the gear meshing method, the overall mechanical structure is simpler, less prone to damage, and more practical.

[0041] In order to ensure the stable movement of the blocking plate 231, a limiting piece is provided on the surface of the blocking plate 231 to limit its movement from the inside of the movable track to the outside of the movable track, and a movable groove adapted to the limiting piece is provided inside the movable track.

[0042] In some embodiments, the protective shell 21 is arranged at the bottom of the rocket mounting frame 12, and the blocking plate 231 is located at the bottom of the rocket mounting frame 12 when the passage of the rocket mounting frame 12 is not blocked, so as to prevent the rocket tail flame from causing damage to the equipment.

[0043] At the same time, when an accident occurs and the blocking plate 231 cannot be opened normally, the support member 232 can be removed from the surface of the protective shell 21 together with the traction member 234 and the power device 235.

[0044] In the description of this technology, it is also necessary to explain that, unless otherwise clearly specified and limited, the terms "set", "install", "connect", and "connect" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in this technology can be understood according to specific circumstances.

[0045] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes within the technical scope disclosed by the present invention according to the technical scheme and the utility model concept of the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A vehicle-mounted artificial weather modification rocket intelligent launcher, characterized in that: include: A launcher body (1) comprises a main frame (11), a rocket mounting frame (12) arranged on the surface of the main frame (11), and an adjustment mechanism (13) connecting the rocket mounting frame (12) and the main frame (11), wherein a passage is provided inside the rocket mounting frame (12) for loading a meteorological rocket; A remote self-locking assembly (2), comprising a protective shell (21) arranged on the surface of a rocket mounting frame (12), a connecting mechanism (22) capable of mounting the protective shell (21) on the surface of a launch frame body (1), a self-locking portion (23) arranged on the surface of the protective shell (21), and a main control unit arranged inside the protective shell (21), wherein the main control unit is capable of controlling an electronic unit in the remote self-locking assembly (2); The surface of the protective shell (21) is provided with a wireless signal transceiver unit, which is connected to the main control unit. The main control unit can control the activity of the self-locking part (23) to block the rocket channel outlet on the surface of the launcher body (1).

2. The vehicle-mounted weather modification rocket intelligent launcher according to claim 1, characterized in that: A control unit capable of controlling the adjustment mechanism (13) is provided on the surface of the main frame (11), and the control unit can be connected to an external operation panel.

3. The vehicle-mounted weather modification rocket intelligent launcher according to claim 2 is characterized in that: The surface of the main frame (11) is provided with a voice broadcast module connected to the control unit and the main control unit, and the voice broadcast module can play corresponding voice according to the operation of the command center.

4. The vehicle-mounted weather modification rocket intelligent launcher according to claim 3 is characterized in that: The self-locking portion (23) comprises a blocking plate (231) disposed on the surface of the rocket mounting frame (12), and a movable mechanism disposed on the surface of the protective shell (21) capable of controlling the movement of the blocking plate (231), wherein the blocking plate (231) is capable of blocking a channel outlet on the surface of the rocket mounting frame (12).

5. The vehicle-mounted weather modification rocket intelligent launcher according to claim 4, characterized in that: A support member (232) for supporting a movable mechanism is provided on the surface of the protective shell (21); the movable mechanism comprises a movable shaft (233) provided on the surface of the support member (232), a traction member (234) provided on the surface of the movable shaft (233), and a power device (235) capable of driving the traction member (234) to move; the traction member (234) can drive the blocking plate (231) to move.

6. The vehicle-mounted weather modification rocket intelligent launcher according to claim 5, characterized in that: The surface of the rocket mounting frame (12) is provided with a movable track for the sealing plate (231) to move inside the track.

7. The vehicle-mounted weather modification rocket intelligent launcher according to claim 6, characterized in that: The traction member (234) is a gear-shaped structure, and the surface of the blocking plate (231) is provided with tooth grooves that match the traction member (234).

8. The vehicle-mounted weather modification rocket intelligent launcher according to claim 7, characterized in that: The surface of the blocking plate (231) is provided with a limiting piece for limiting its movement from the inside of the movable track to the outside of the movable track, and the inside of the movable track is provided with a movable groove adapted to the limiting piece.

9. The vehicle-mounted weather modification rocket intelligent launcher according to claim 8, characterized in that: The protective shell (21) is arranged at the bottom of the rocket mounting frame (12), and the blocking plate (231) is located at a position of the rocket mounting frame (12) close to the bottom thereof when the passage of the rocket mounting frame (12) is not blocked.

10. The vehicle-mounted weather modification rocket intelligent launcher according to claim 9, characterized in that: The support member (232) can be removed from the surface of the protective shell (21) together with the traction member (234) and the power device (235).

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