Unmanned vehicle cannon launching device

Abstract

The invention provides a cannon launching device for an unmanned vehicle. The cannon launching device comprises a gas cylinder unit and a shell ejecting mechanism. The gas cylinder unit comprises a gas chamber front part and a gas chamber rear part; the air chamber front part and the air chamber rear part are connected through sealing threads; the shell ejecting mechanism comprises a partition plate, a shell ejecting elastic piece, a locking ring and a bullet. The shell ejecting mechanism is connected with the gas cylinder unit through a partition plate, and when the shell ejecting mechanism is not unfolded, the shell ejecting mechanism comprises the partition plate, a shell ejecting elastic piece and a bullet from one end to the other end. The unmanned vehicle is wrapped in a cavity formed by the shell ejecting elastic pieces. Compared with a traditional unmanned vehicle transportation mode, the cannon-shooting unmanned vehicle can reach a designated place at a higher speed, the delivery time is greatly shortened, and the delivery timeliness is improved.

Description

Technical Field

[0001] The present application relates to the technical field of novel unmanned vehicles, and in particular to an unmanned vehicle artillery delivery device. Background Art

[0002] Unmanned vehicles, also known as autonomous or self-driving vehicles, are controlled by remote control devices or self-programmed systems. Conventional unmanned vehicles are often used in disaster relief and military operations due to time-consuming and energy-intensive long-distance missions and obstacles in unstructured terrain, hindering their effectiveness and timeliness.

[0003] With the rapid development of artificial intelligence (AI) technology, demand for it is increasing in the emergency rescue sector. A large number of intelligent unmanned equipment, such as "unmanned vehicles" and "unmanned ships," have emerged and are being used in national defense and civil defense. Currently, the deployment of unmanned equipment is mostly manual and relies on human mobility. Traditional unmanned vehicles typically deploy drones, which then fly to the precise destination and deliver the supplies directly there. If the destination is harsh or has other restrictions, both drones and unmanned vehicles will have difficulty reaching it. Furthermore, it takes a considerable amount of time for drones to reach their destination. In time-sensitive situations, such as emergencies, waiting for the drone to arrive can be a significant waste of time. Consequently, existing deployment methods present numerous challenges, including susceptibility to harsh environments, which can compromise drone flight stability, short flight times, high costs, and limited speed. These issues contribute to the current use of unmanned vehicles for rescue operations being slow, ineffective, energy-intensive, and ineffective. Summary of the Invention

[0004] The present application provides an unmanned vehicle artillery delivery device that can be used to solve the technical problem of being unable to reach the destination in a short time.

[0005] The present application provides an unmanned vehicle gun-launching device, comprising:

[0006] Gas cylinder unit and ejection mechanism;

[0007] The gas cylinder unit includes a gas chamber front portion and a gas chamber rear portion;

[0008] The front part of the air chamber and the rear part of the air chamber are connected by a sealing thread;

[0009] The ejection mechanism includes a partition, ejection shrapnel, locking ring, and warhead;

[0010] The ejection mechanism is connected to the gas cylinder unit through a bulkhead;

[0011] When the ejection mechanism is not deployed, from one end to the other, including the partition, ejection fragments and warhead;

[0012] The unmanned vehicle was encased in the cavity formed by the ejected shrapnel.

[0013] Furthermore, a balancing tail is installed at the bottom of the front part of the air chamber; the balancing tail is used to control and ensure the flight posture of the projectile.

[0014] Furthermore, an air inlet is left at the front port of the air chamber, which is filled with high-pressure air before launch to provide flight power for the projectile. When it flies to the preset area, the shell ejection mechanism is deployed.

[0015] Furthermore, the ejection fragment includes a plurality of single fragments with the same structure; the plurality of single fragments are evenly distributed around;

[0016] One end of the single spring piece is provided with a protruding hook-shaped portion; the locking ring is provided with a fixing device adapted to the hook-shaped portion; one end of each single spring piece is interlocked with the locking ring;

[0017] The other end of each single elastic piece is hinged to the partition plate by a spring hinge.

[0018] Furthermore, the end of the shell ejection mechanism is the warhead that controls the operation. The deployment angle and position of the shell ejection fragment are determined by a variety of methods. After the shell ejection mechanism reaches the predetermined position, it is deployed, and the end of the shell ejection fragment connected to the locking ring is unhooked. The shell ejection fragment opens, releasing the unmanned vehicle, and the unmanned vehicle is dropped to the predetermined position; at this point, the separation of the unmanned vehicle and it is completed, and the deployment of the unmanned vehicle is realized.

[0019] This application has the following advantages:

[0020] Fast delivery: Compared with traditional unmanned vehicle transportation methods, artillery-fired unmanned vehicles can reach designated locations at a faster speed, greatly shortening the delivery time and improving the timeliness of delivery;

[0021] Energy saving: The gun-launched unmanned vehicle uses air cannons to provide power, which can reduce the energy consumption of the unmanned vehicle itself, indirectly increase the endurance of the unmanned vehicle, and extend the time it stays in the target area;

[0022] Expanded operating range: Gun-launched unmanned vehicles can deliver at a longer distance, expanding their operating range. This is particularly beneficial for remote delivery or inaccessible dangerous areas.

[0023] Improved safety: Delivering unmanned vehicles by cannon-firing can reduce the risk of personnel directly contacting the target area, lowering the possibility of casualties and improving operational safety.

[0024] Enhanced response capabilities: The rapid delivery capability of the gun-launched unmanned vehicle makes it of great application value in emergency rescue and military operations. It can quickly enter the target area and provide necessary support and rescue, thus improving the ability to respond to emergencies. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] Figure 1 It is a schematic diagram of the overall structure of the present invention;

[0026] Figure 2 It is the outer shape of the projectile of the present invention;

[0027] Figure 3 It is an isometric view of the projectile body of the present invention;

[0028] Figure 4 It is the expanded diagram of the ejection shell of the present invention;

[0029] Figure 5 It is the expanded diagram of the ejection shell of the present invention;

[0030] Figure 6 This is a schematic diagram of the locking ring connection of the present invention;

[0031] In the figure, 1 is the balancing tail fin; 2 is the rear part of the air chamber; 3 is the front part of the air chamber; 4 is the partition; 5 is the ejection fragment; 6 is the unmanned vehicle; 7 is the locking ring; 8 is the warhead. DETAILED DESCRIPTION

[0032] In order to make the objectives, technical solutions and advantages of this application clearer, the implementation methods of this application will be further described in detail below with reference to the accompanying drawings.

[0033] In order to make the contents of the present invention more clearly understood, the present invention is further described in detail below based on specific embodiments in conjunction with the accompanying drawings.

[0034] An unmanned vehicle gunnery delivery device comprises:

[0035] Gas cylinder unit and ejection mechanism;

[0036] like Figures 2-3 As shown, a bullet-shaped shell structure, such as Figure 1 As shown, the main part of the projectile-shaped shell is the gas cylinder unit; the gas cylinder unit includes a front gas chamber 2 and a rear gas chamber 3; the front gas chamber 2 and the rear gas chamber 3 are connected by a sealing thread; the bottom of the front gas chamber 2 is installed with a balancing tail 1; the balancing tail 1 is used to control and ensure the flight posture of the projectile.

[0037] There are air inlets at the two ports in front of the air chamber, which are filled with high-pressure air before launch to provide the projectile with flight power. When the projectile reaches the preset area, the ejection mechanism is deployed.

[0038] The ejection mechanism includes a partition plate 4, an ejection shrapnel 5, a locking ring 7, and a warhead 8; the ejection mechanism is connected to the gas cylinder unit through the partition plate 4;

[0039] When the ejection mechanism is not deployed, from one end to the other, it includes the partition 4, the ejection shrapnel 5 and the warhead 8;

[0040] The ejection fragment 5 includes multiple single fragments with the same structure; the multiple single fragments are evenly distributed around; the unmanned vehicle is wrapped in the cavity formed by the ejection fragment 5;

[0041] One end of the single spring piece is provided with a protruding hook-shaped portion; the locking ring 7 is provided with a fixing device adapted to the hook-shaped portion; Figure 6 As shown, one end of each single elastic piece is interlocked with the locking ring 7 to close the chamber to carry the unmanned vehicle 6; the other end of each single elastic piece is hinged to the partition 4 by a spring hinge.

[0042] The ejection mechanism, which controls the operation of the warhead 8, determines the deployment angle and position of the ejection fragment 5 through various means. Once the ejection mechanism reaches the predetermined position, it deploys. The end of the ejection fragment 5 connected to the locking ring 7 is unhooked, and the ejection fragment 5 opens, releasing the unmanned vehicle, which is then deployed to the predetermined position. This completes the separation of the unmanned vehicle 6 from the ejection mechanism, allowing the unmanned vehicle 6 to be deployed.

[0043] The working principle of the present invention is as follows:

[0044] An air cannon launch platform is used, which is connected to the platform gas cylinder through the air inlet to provide power for projectile launch. According to the target location, launch direction, weather conditions and other factors, the launch angle and initial velocity are determined to complete the air cannon projectile launch; the projectile flies smoothly over the target area, and the ejection mechanism is controlled by the front-end warhead sensing. When the ejection conditions are met, the locking ring is first pushed out by the electric push rod to release the ejection fragments. The ejection fragments automatically unfold, thereby separating the ejection mechanism and realizing the unmanned vehicle shell removal; at the same time, the unmanned vehicle parachutes and is dropped to the target location with the help of a parachute.

[0045] In this specification, the same or similar parts between the various embodiments can be referred to each other. In particular, for the service construction device and service loading device embodiments, since they are basically similar to the method embodiment, the description is relatively simple, and the relevant parts can be referred to the description in the method embodiment.

[0046] The above-described embodiments of the present application do not constitute a limitation on the scope of protection of the present application.

Claims

1. An unmanned vehicle gun-launching device, characterized in that: The device comprises: Gas cylinder unit and ejection mechanism; The gas cylinder unit comprises a gas chamber front portion (2) and a gas chamber rear portion (3); The air chamber front part (2) and the air chamber rear part (3) are connected by a sealing thread; The shell ejection mechanism comprises a partition plate (4), a shell ejection shrapnel (5), a locking ring (7), and a warhead (8); The shell ejection mechanism is connected to the gas cylinder unit via a partition (4); When the ejection mechanism is not deployed, from one end to the other, it includes a partition (4), an ejection shrapnel (5) and a warhead (8); The unmanned vehicle is enclosed in the cavity formed by the ejected shell fragments (5).

2. The device according to claim 1, characterized in that A balancing tail (1) is installed at the bottom of the front part (2) of the air chamber; the balancing tail (1) is used to control and ensure the flight posture of the projectile.

3. The device according to claim 1, characterized in that An air inlet is left at the front port (2) of the air chamber, which is filled with high-pressure air before firing to provide the projectile with flight power. When the projectile flies to a preset area, the ejection mechanism is deployed.

4. The device according to claim 1, characterized in that The ejection fragment (5) comprises a plurality of single-body fragments with the same structure; the multiple single-body fragments are evenly distributed around; One end of the single elastic piece is provided with a protruding hook-shaped portion; the locking ring (7) is provided with a fixing device adapted to the hook-shaped portion; one end of each single elastic piece is interlocked with the locking ring (7); The other end of each single elastic piece is hinged to the partition plate (4) by a spring hinge.

5. The device according to claim 1, characterized in that The end of the ejection mechanism is a warhead (8) for controlling operation. The deployment angle and position of the ejection fragment (5) are determined by various methods. After the ejection mechanism reaches a predetermined position, the ejection fragment (5) is deployed, and the end connected to the locking ring (7) is unhooked. The ejection fragment (5) is opened, and the unmanned vehicle is released. The unmanned vehicle is then dropped to the predetermined position. At this point, the separation of the unmanned vehicle (6) and the ejection fragment is completed, and the dropping of the unmanned vehicle (6) is realized.

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