A vehicle-mounted container for drone swarm transmission and reception

Abstract

This utility model discloses a vehicle-mounted container for drone swarm launch and reception, relating to the field of drone launch and reception technology. It includes a container body with symmetrical side panels on both the front and rear sides. Inside the container is a first opening and closing assembly for opening and closing the two pairs of side panels. The outer top surface of the container has symmetrically arranged top panels, and a second opening and closing assembly for opening and closing the two top panels is also provided on the outer top surface. This utility model, through the first and second opening and closing assemblies, enables the top and side panels to open and close synchronously, thereby achieving simultaneous take-off and landing of drones from the top and sides of the container. Simultaneous take-off and landing do not interfere with each other, allowing for a large number of drones to take off and land simultaneously in a swarm, resulting in shorter deployment time and higher efficiency.

Description

Technical Field

[0001] This utility model relates to the field of drone transceiver technology, and in particular to a vehicle-mounted container for drone swarm transceiver applications. Background Technology

[0002] The launch and reception of general-purpose drone swarms are carried out with the help of manual labor or auxiliary equipment, and their deployment and execution time is relatively long. However, for special-purpose drones such as military and police drones, it is necessary to complete the mission in a short time and with high efficiency, including rapid deployment / closure of the cabin, rapid take-off and landing of drone swarms, rapid departure from the mission site, and rapid relocation of the mission site. In response to this situation, drone vehicle-mounted platforms have emerged.

[0003] However, existing vehicle-mounted cabins only open the top or one side for drone take-off and landing, resulting in relatively low space utilization in drone swarm scenarios and thus limiting their application. Therefore, those skilled in the art have provided a vehicle-mounted cabin for drone swarm launch and reception to address the problems mentioned in the background. Utility Model Content

[0004] To address the shortcomings of existing technologies, this utility model provides a vehicle-mounted container for drone swarm launch and reception, which solves the problem mentioned in the background technology that only the top or a single side space is opened for drone take-off and landing, resulting in relatively low space utilization in drone swarm scenarios and thus certain limitations in use.

[0005] To achieve the above objectives, this utility model is implemented through the following technical solution: a vehicle-mounted container for receiving and transmitting drone clusters, comprising a container body, with side plates symmetrically arranged on both the front and rear sides of the container body, an opening and closing assembly 1 for driving the two pairs of side plates to open and close inside the container body, a top plate symmetrically arranged on the outer top surface of the container body, and an opening and closing assembly 2 for driving the two top plates to open and close on the outer top surface of the container body.

[0006] The opening and closing assembly includes a square cavity inside the cabin. Horizontal grooves communicating with the square cavity are formed at both ends of the bottom surface of the cabin. Symmetrical through-type vertical grooves are formed on the outer walls of the left and right sides of the cabin. Two pairs of side plates are slidably connected to the inner sides of the two pairs of vertical grooves. Connecting plates are fixed to one end of the corresponding outer bottom surface of each pair of side plates. One end of each pair of connecting plates slides along the horizontal grooves into the interior of the square cavity. A rotating shaft is rotatably installed at the center of the inner side wall of the square cavity. Gears are fixed to both ends of the outer periphery of the rotating shaft. Straight plates are fixed to the corresponding outer side walls of each pair of connecting plates. Racks are fixed to the corresponding outer side walls of each pair of straight plates. The two pairs of racks are meshed with two gears.

[0007] As a further technical solution of this utility model, the second opening and closing component includes a second rotating shaft that is symmetrically and rotatably installed at the center of the top of the inner side wall of the cabin. The corresponding ends of the two top plates are respectively fixedly sleeved on the outer peripheral side walls of the two rotating shafts. Grooves are provided on both the left and right sides of the outer top surface of the cabin. The opposite ends of the two top plates are fixed with a card plate that matches the two grooves.

[0008] As a further technical solution of this utility model, the two ends of the two rotating shafts extend to the outer walls of the front and rear sides of the cabin, respectively. Gears are fixed on the rear outer wall of the cabin and on the outer peripheral side wall of the two rotating shafts. The two gears mesh with each other. A drive motor is fixedly installed on the front outer wall of the cabin. The output end of the drive motor is fixedly connected to one of the rotating shafts.

[0009] As a further technical solution of this utility model, the inner top surfaces of the two pairs of vertical grooves are provided with mutually penetrating sliding grooves, and the outer top surfaces of the two pairs of side plates are fixedly installed with U-shaped square plates that are adapted to the sliding grooves. The inner sides of the two pairs of U-shaped square plates are rotatably installed with several round wheels.

[0010] As a further technical solution of this utility model, one end of the rotating shaft extends rotatably to the rear outer wall of the cabin, and a second drive motor is fixedly installed on the rear outer wall of the cabin corresponding to the rotating shaft. The output end of the second drive motor is fixedly connected to the rotating shaft.

[0011] As a further technical solution of this utility model, guide rods are fixed on the opposite outer walls of the two pairs of connecting plates, and the opposite ends of the two pairs of guide rods slide through the square cavity and extend to the left and right outer walls of the cabin respectively.

[0012] As a further technical solution of this utility model, mounting blocks are fixed at the bottom center positions of the outer walls on both the left and right sides of the cabin.

[0013] This utility model provides a vehicle-mounted container for drone swarm transmission and reception, which has the following advantages compared with the prior art:

[0014] 1. This design provides a vehicle-mounted container for drone swarm launch and reception. Through the setting of opening and closing components one and two, the top and side panels can be driven to open and close synchronously, thereby enabling drones to take off and land synchronously from the top and sides of the container. The take-off and landing do not interfere with each other, allowing a large number of drones to take off and land simultaneously in the drone swarm, with short deployment time and high efficiency, thus improving practicality.

[0015] 2. This design provides a vehicle-mounted container for drone swarm launch and reception. The top and side panels open and close independently without interfering with each other, allowing them to operate simultaneously, thereby saving drone swarm deployment time and improving operational flexibility. Attached Figure Description

[0016] Figure 1 A schematic diagram of the first three-dimensional structure of a vehicle-mounted container for use in drone swarm transmission and reception;

[0017] Figure 2 This is a schematic diagram of the second three-dimensional structure of a vehicle-mounted container used for drone swarm transmission and reception;

[0018] Figure 3 A schematic diagram of the three-dimensional structure of a vehicle-mounted container used for drone swarm transmission and reception;

[0019] Figure 4 A cross-sectional three-dimensional structural diagram of a vehicle-mounted container used for drone swarm transmission and reception;

[0020] Figure 5 A three-dimensional structural diagram of the opening and closing component of a vehicle-mounted container used for drone swarm transmission and reception.

[0021] Figure 6 This is a two-dimensional structural diagram of the opening and closing components of a vehicle-mounted container used for drone swarm transmission and reception.

[0022] In the picture:

[0023] 1. Hull; 101. Side panel; 102. Top panel;

[0024] 2. Opening and closing assembly one; 201. Square cavity; 202. Horizontal groove; 203. Vertical groove; 204. Connecting plate; 205. Rotating shaft one; 206. Gear one; 207. Straight plate; 208. Rack; 209. Drive motor two;

[0025] 3. Opening and closing assembly two; 301. Rotating shaft two; 302. Groove; 303. Clamping plate; 304. Gear two; 305. Drive motor one;

[0026] 4. Slide groove; 401. U-shaped square plate; 402. Round wheel; 403. Guide rod;

[0027] 5. Installation block. Detailed Implementation

[0028] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort are within the protection scope of the present utility model.

[0029] Please see Figure 1-6 This utility model provides a vehicle-mounted container technology solution for drone swarm launch and reception: it includes a container body 1, and mounting blocks 5 are fixed at the bottom center of the outer walls on both sides of the container body 1. The mounting blocks 5 are threaded onto the vehicle by tightening the fastening bolts. Then, the tractor is started to pull the vehicle and move the container body 1. After reaching the designated position, the vehicle is unloaded and the container body 1 can be used.

[0030] The cabin 1 has symmetrical side plates 101 on both its front and rear sides. Inside the cabin 1 is an opening and closing assembly 2 for opening and closing the two pairs of side plates 101. The opening and closing assembly 2 includes a square cavity 201 inside the cabin 1. Horizontal grooves 202, communicating with the square cavity 201, are formed at both the front and rear ends of the bottom surface of the cabin 1. Vertical grooves 203, forming a through-hole, are symmetrically formed on the outer walls of the left and right sides of the cabin 1. The two pairs of side plates 101 are slidably connected to the inner sides of the two pairs of vertical grooves 203. One end of each pair of connecting plates 204 is fixed to one of the corresponding ends of the outer bottom surface. One end of each pair of connecting plates 204 slides along the transverse groove 202 into the interior of the square cavity 201. A rotating shaft 205 is rotatably installed at the center of the inner sidewall of the square cavity 201. Gears 206 are fixed at both ends of the outer peripheral sidewall of the rotating shaft 205. Straight plates 207 are fixedly installed on the corresponding outer sidewalls of each pair of connecting plates 204. Racks 208 are fixed on the corresponding outer sidewalls of each pair of straight plates 207. The racks 208 are divided into two pairs of racks. The two gears 206 are not meshed together. One end of the rotating shaft 205 extends to the rear outer wall of the cabin 1. A drive motor 209 is fixedly installed on the rear outer wall of the cabin 1 at the location corresponding to the rotating shaft 205. The output end of the drive motor 209 is fixedly connected to the rotating shaft 205. In use, the controller controls and starts the drive motor 209 to drive the rotating shaft 205 to rotate the two gears 206 in a circular motion inside the square cavity 201. Under the meshing connection characteristics of 206, the rack 208 on the straight plate 207 drives the connecting plate 204 to move the side plate 101 along the inner side of the vertical groove 203, moving closer or further apart, thereby realizing the opening and closing effect of the two pairs of side plates 101 on the front and rear sides of the cabin 1, which facilitates the UAV to be launched and dropped from both sides of the cabin 1. (When the side plate 101 is opened or closed, the rotating shaft 205 is locked by the shaft locking device installed on the rear outer wall of the cabin 1 to prevent self-spinning).

[0031] The inner top surfaces of the two pairs of vertical grooves 203 are provided with interconnected sliding grooves 4. The outer top surfaces of the two pairs of side plates 101 are fixedly installed with U-shaped square plates 401 that are adapted to the sliding grooves 4. Several round wheels 402 are rotatably installed on the inner sides of the two pairs of U-shaped square plates 401. Guide rods 403 are fixed on the opposite outer walls of the two pairs of connecting plates 204. The opposite ends of the two pairs of guide rods 403 pass through the square cavity 201 and slide to the left and right outer walls of the cabin 1 respectively. When the two pairs of side plates 101 are opened and closed, the round wheels 402 slide along the inner side of the sliding grooves 4 and the guide rods 403 slide inside the square cavity 201 simultaneously, thereby ensuring the stability of the side plates 101 when opening and closing, thus increasing practicality.

[0032] The outer top surface of the cabin 1 is symmetrically provided with top plates 102. The outer top surface of the cabin 1 is provided with an opening and closing assembly 3 for driving the two top plates 102 to open and close. The opening and closing assembly 3 includes a rotating shaft 301 symmetrically rotatably mounted at the center of the top of the inner side wall of the cabin 1. One end of each of the two top plates 102 is fixedly sleeved on the outer peripheral side wall of the two rotating shafts 301. Grooves 302 are provided on both the left and right sides of the outer top surface of the cabin 1. A locking plate 303 that matches the two grooves 302 is fixed to the opposite ends of each of the two top plates 102. The two ends of the two rotating shafts 301 extend rotatably to the outer walls of the front and rear sides of the cabin 1. Gears 304 are fixed to the rear outer wall of the cabin 1, located on the outer peripheral side wall of the two rotating shafts 301. The two gears 304 mesh with each other. The front outer wall of the cabin 1 is fixed... A drive motor 305 is installed, and the output end of the drive motor 305 is fixedly connected to one of the rotating shafts 301. In use, the controller controls and starts the drive motor 305 to drive one of the rotating shafts 301 to rotate with the gear 304. Under the meshing connection characteristics of the gear 304, the other gear drives the other rotating shaft 301 to rotate synchronously, thereby driving the two top plates 102 to open and close on the outer top surface of the cabin 1. This facilitates the UAV to be launched and retrieved from the top surface of the cabin 1, increasing flexibility. With the assistance of the slot and the locking plate 303, the stability of the top plate 102 when closed can be ensured. (When the top plate 102 is opened or closed, the rotating shaft 301 is locked by the shaft locking device installed on the front outer wall of the cabin 1 to prevent self-spinning).

[0033] The working principle of this utility model is as follows: In use, the cabin 1 is first moved to the designated position. Then, the drive motor 209 is started to drive the rotating shaft 205, which in turn rotates the gear 206. This causes the rack 208 on the straight plate 207 to move away from each other along the inner side of the vertical groove 203 via the connecting plate 204, allowing the two pairs of side plates 101 to open from the front and rear sides of the cabin 1. Simultaneously, the drive motor 305 is started to drive the rotating shaft 301, which in turn rotates the gear 304, thereby driving the two top plates 102 to open on the outer top surface of the cabin 1. Then, the drones can take off and land simultaneously from the top and sides of the cabin 1. The take-off and landing are simultaneous and do not interfere with each other, enabling the drone swarm to take off and land at the same time, with a large number of drones, short deployment time, and high efficiency. (It should be noted that all electrical components mentioned in the text are electrically connected to an external power source, and the control method in this utility model is controlled by a PLC controller. The control circuit of the PLC controller can be implemented by those skilled in the art through programming, and thus can operate normally according to the above steps. The power supply is also common knowledge in the art, so the control method and circuit connection will not be explained in detail.)

[0034] The above description is merely a preferred embodiment of this utility model. It should be noted that those skilled in the art can make various improvements and modifications without departing from the principles of this utility model, and these improvements and modifications should also be considered within the scope of protection of this utility model. Structures, devices, and operating methods not specifically described or explained in this utility model are implemented according to conventional methods in the art, unless otherwise specified or limited.

Claims

1. A vehicle-mounted container for use in drone swarm transmission and reception, characterized in that, Includes a cabin (1), with side plates (101) symmetrically arranged on both the front and rear sides of the cabin (1), and an opening and closing assembly (2) for driving the two pairs of side plates (101) to open and close inside the cabin (1). A top plate (102) is symmetrically arranged on the outer top surface of the cabin (1), and an opening and closing assembly (3) for driving the two top plates (102) to open and close is arranged on the outer top surface of the cabin (1). The opening and closing assembly 1 (2) includes a square cavity (201) inside the cabin (1). Both ends of the bottom surface of the cabin (1) have transverse grooves (202) that communicate with the square cavity (201). The outer walls of the left and right sides of the cabin (1) have symmetrically arranged through-type vertical grooves (203). Two pairs of side plates (101) are slidably connected to the inner sides of the two pairs of vertical grooves (203). A connecting plate (204) is fixed to one end of the corresponding outer bottom surface of each pair of side plates (101). One end of each pair of connecting plates (204)... All slide along the transverse groove (202) to the interior of the square cavity (201). A rotating shaft (205) is rotatably installed at the center of the inner sidewall of the square cavity (201). Gears (206) are fixed at both ends of the outer peripheral sidewall of the rotating shaft (205). Straight plates (207) are fixedly installed on the corresponding outer sidewalls of the two pairs of connecting plates (204). Racks (208) are fixed on the corresponding outer sidewalls of the two pairs of straight plates (207). The two pairs of racks (208) are respectively meshed with the two gears (206).

2. The vehicle-mounted container for UAV swarm transmission and reception according to claim 1, characterized in that, The second opening and closing component (3) includes a second rotating shaft (301) symmetrically rotated and installed at the center of the top of the inner side wall of the cabin (1). The corresponding ends of the two top plates (102) are respectively fixedly sleeved on the outer peripheral side walls of the two rotating shafts (301). The left and right sides of the outer top surface of the cabin (1) are provided with grooves (302). The opposite ends of the two top plates (102) are fixed with a card plate (303) that matches the two grooves (302).

3. The vehicle-mounted container for UAV swarm transmission and reception according to claim 2, characterized in that, The two ends of the two rotating shafts (301) extend to the outer walls of the front and rear sides of the cabin (1). Gears (304) are fixed on the rear outer wall of the cabin (1) and on the outer peripheral side wall of the two rotating shafts (301). The two gears (304) mesh with each other. A drive motor (305) is fixedly installed on the front outer wall of the cabin (1). The output end of the drive motor (305) is fixedly connected to one of the rotating shafts (301).

4. The vehicle-mounted container for UAV swarm transmission and reception according to claim 1, characterized in that, The inner top surfaces of the two pairs of vertical grooves (203) are provided with mutually penetrating sliding grooves (4), and the outer top surfaces of the two pairs of side plates (101) are fixedly installed with U-shaped square plates (401) that are compatible with the sliding grooves (4). Several round wheels (402) are rotatably installed on the inner sides of the two pairs of U-shaped square plates (401).

5. A vehicle-mounted container for UAV swarm transmission and reception according to claim 1, characterized in that, One end of the first rotating shaft (205) extends rotatably to the rear outer wall of the cabin (1). A second drive motor (209) is fixedly installed on the rear outer wall of the cabin (1) at the location corresponding to the first rotating shaft (205). The output end of the second drive motor (209) is fixedly connected to the first rotating shaft (205).

6. The vehicle-mounted container for UAV swarm transmission and reception according to claim 1, characterized in that, Guide rods (403) are fixed on opposite outer walls of the two pairs of connecting plates (204). The opposite ends of the two pairs of guide rods (403) slide through the square cavity (201) and extend to the left and right outer walls of the cabin (1).

7. A vehicle-mounted container for UAV swarm transmission and reception according to claim 1, characterized in that, Mounting blocks (5) are fixed at the bottom center of the outer walls on both sides of the cabin (1).

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