Unmanned aerial vehicle cluster launching, storage and transportation integrated device

Abstract

The utility model relates to an unmanned aerial vehicle cluster launching, storing and transporting integrated device, belongs to the technical field of aircrafts, and solves the problems that unmanned aerial vehicle clusters are difficult to store and transport conveniently and multi-aircraft launching efficiency is low in the prior art. The device comprises a launching unit and a storage and transportation unit, the transmitting unit is arranged in the storage and transportation unit; a plurality of storage and transportation units are arranged; the transmitting unit comprises a conveying assembly; the conveying assembly is connected with the connecting part of the unmanned aerial vehicle and can convey the unmanned aerial vehicle to the end of the conveying assembly. The connecting part can be fixed to or separated from the conveying assembly; according to the utility model, convenient storage and transportation of the unmanned aerial vehicle cluster and rapid launching of the unmanned aerial vehicle cluster can be realized.

Description

Technical Field

[0001] This utility model relates to the field of aircraft technology, and in particular to an integrated device for launching, storing and transporting unmanned aerial vehicles (UAVs) in clusters. Background Technology

[0002] As micro-drone technology continues to mature, the application of drone swarms is becoming more and more widespread. Now, the flight maneuverability, one-stop multi-drone control, and swarm collaborative flight capabilities of multi-rotor, fixed-wing, and other micro-drones are constantly improving. In particular, the combination of drone swarms with vehicle-mounted platforms can realize applications such as swarm-style storage and transportation, launch, and large-scale deployment.

[0003] The large-scale and convenient application of drone swarms is currently hampered by storage and transportation methods, launch methods, and launch sites, which severely restricts the improvement of launch and storage efficiency. The storage, transportation, and launch of drone swarms need to comprehensively consider factors such as drone unit configuration, launch mode, and cost-effectiveness. At the same time, the storage and transportation of drones should be able to meet the transportation requirements of vehicles and other transportation platforms. Utility Model Content

[0004] Based on the above analysis, the present invention aims to provide an integrated device for the launch, storage and transportation of unmanned aerial vehicles (UAVs) swarms, in order to solve the problems of convenient storage and transportation of UAV swarms and low efficiency of multi-UAV launch.

[0005] The objective of this utility model is mainly achieved through the following technical solutions:

[0006] An integrated launch, storage, and transportation device for unmanned aerial vehicles (UAVs) swarms includes a launch unit and a storage and transportation unit; multiple storage and transportation units are provided.

[0007] The launching unit is disposed within the storage and transportation unit; the launching unit includes a transmission component;

[0008] The transmission component is connected to the connection part of the UAV, and the transmission component can transmit the UAV to the launch position; the connection part can be fixed to or detached from the transmission component;

[0009] The transmission assembly (22) includes a drive structure, a synchronous belt (221), and a drive wheel (222); or

[0010] The transmission assembly (22) includes a drive structure, a chain, and gears.

[0011] Furthermore, the drive wheel is connected to the drive structure, and the drive structure is capable of driving the drive wheel to rotate;

[0012] The timing belt is mounted on the drive wheel; the timing belt can rotate with the drive wheel.

[0013] Furthermore, a connection structure is provided on the synchronization belt; the connection part is connected to the connection structure.

[0014] Furthermore, the connecting part is provided with a through hole, and the connecting structure is a protrusion that can be inserted into the through hole.

[0015] Furthermore, the transmitting unit also includes a base, and the transmitting components are symmetrically arranged on both sides of the base.

[0016] Furthermore, the chain is provided with a connecting structure, and the connecting part is connected to the connecting structure.

[0017] Furthermore, multiple arrays of the aforementioned storage and transportation units are arranged.

[0018] Furthermore, the storage and transportation unit includes a box body and a box lid;

[0019] The lid is located at the end of the box body;

[0020] The upper part of the box is provided with a loading port, which is used for loading and unloading the drone.

[0021] Furthermore, the end of the enclosure relative to the enclosure cover is provided with power supply and communication interfaces.

[0022] Furthermore, the opening method of the box lid is one of side opening, double opening, or pull-out.

[0023] Compared with the prior art, the present invention can achieve at least one of the following beneficial effects:

[0024] (1) Compared with the prior art, this utility model includes a drone, a launch unit, and a storage and transportation unit. The storage and transportation unit is equipped with a launch unit capable of transporting drones. During storage and transportation, the drone is mounted on the launch unit via its own connecting part, and can be fixed and detached from the connecting part. When the drone is launched, it is transported to the launch position through the transmission component of the launch unit, and is launched after quickly detaching from the launch unit. The transmission component includes a synchronous belt and a drive wheel structure, and the synchronous belt is driven by the drive wheel for transmission. Multiple storage and transportation units are provided, which can realize the parallel operation of multiple sets of launch devices and can be deployed on vehicle-mounted, ship-mounted, ground and other platforms, thereby realizing the integration of storage, transportation and launch of drone clusters, solving the problems of inconvenient storage and transportation of drone clusters and low efficiency of multi-drone launch.

[0025] (2) Compared with the prior art, the transmission component of this utility model includes a drive structure, a drive wheel, and a synchronous belt. The drive structure in the transmission component drives the drive wheel to rotate, which in turn drives the synchronous belt on the drive wheel to run, transporting the UAV to the launch position. The UAV is launched after detaching from the launch unit. The connecting part of the UAV is provided with a fixing hole, and the synchronous belt is provided with a protrusion. The protrusion is inserted into the fixing hole for fixation. During launch, the protrusion detaches from the fixing hole for launch, thereby realizing the rapid fixation and rapid detachment of the UAV and rapid launch, improving the fixation efficiency and launch efficiency of the UAV swarm. This utility model uses a lightweight and efficient drive wheel transmission system, with fewer overall parts, making it easy to process and assemble.

[0026] (3) The storage and transportation unit adopts a modular sealed box to realize the storage and transportation of UAVs. It has the ability to protect the UAVs in the field and can quickly reach the work area with the help of vehicles, ships and other means of transportation and realize the rapid and continuous launch of UAVs, quickly form a cluster, and quickly carry out collaborative work tasks.

[0027] In this invention, the above-described technical solutions can be combined with each other to achieve more preferred combinations. Other features and advantages of this invention will be set forth in the following description, and some advantages will become apparent from the description or be learned by practicing this invention. The objectives and other advantages of this invention can be realized and obtained from the details specifically pointed out in the text and accompanying drawings. Attached Figure Description

[0028] The accompanying drawings are for illustrative purposes only and are not intended to limit the scope of the invention. Throughout the drawings, the same reference numerals denote the same parts.

[0029] Figure 1 A schematic diagram of an integrated launch, storage, and transportation device for unmanned aerial vehicles (UAVs) swarms.

[0030] Figure 2 This is a schematic diagram of the structure of the UAV fixed to the launch unit;

[0031] Figure 3 A schematic diagram showing the connection between the mounting hole of the drone and the protrusion of the timing belt;

[0032] Figure 4 This is a schematic diagram of the structure of a drone;

[0033] Figure 5 This is a schematic diagram of the transmitting unit.

[0034] Figure 6 This is a schematic diagram of the connection structure between the base and the transmission component.

[0035] Figure 7 Schematic diagram of the storage and transportation unit;

[0036] Figure 8 A schematic diagram of the structure of an integrated launch and storage device for unmanned aerial vehicles (UAVs) on a carrier platform.

[0037] Figure label:

[0038] 1-UAV, 11-Body section, 12-Payload section, 13-Connecting section, 131-Fixing hole, 2-Launch unit, 21-Base, 22-Transmission assembly, 221-Synchronous belt, 2211-Protrusion, 221-Drive wheel, 3-Storage and transportation unit, 31-Box, 311-Filling port, 312-Power supply and communication interface, 32-Box cover, 4-Carrier platform. Detailed Implementation

[0039] The preferred embodiments of the present invention will now be described in detail with reference to the accompanying drawings, which constitute a part of the present invention and are used together with the embodiments of the present invention to illustrate the principles of the present invention, but are not intended to limit the scope of the present invention.

[0040] A specific embodiment of this utility model is as follows: Figure 1 As shown, an integrated launch, storage and transportation device for unmanned aerial vehicles (UAVs) clusters is disclosed, including a launch unit 2 and a storage and transportation unit 3.

[0041] The launch unit 2 is located within the storage and transportation unit 3; multiple storage and transportation units 3 are provided.

[0042] The transmitting unit 2 includes a transmission component 22;

[0043] The transmission component 22 is connected to the connection part 13 of the drone 1, and the connection part 13 can be fixed or detached from the transmission component 22; the transmission component 22 can transmit the drone 1 to its end.

[0044] The transmission assembly 22 includes a drive structure, a timing belt 221, and a drive wheel 222.

[0045] Compared to existing technologies, this embodiment includes a launch unit 2 and a storage and transportation unit 3. The storage and transportation unit 3 houses the launch unit 2, which is capable of transporting the UAV 1. During storage and transportation, the UAV 1 is mounted on the launch unit 2 via its connecting part 13, allowing for both fixation and detachment from the connecting part 13. When launching, the UAV 1 is transported to the launch position via the transmission component 22 of the launch unit 2, and launches rapidly after detaching from the launch unit 2. Multiple storage and transportation units 3 are provided, which can be modularly assembled to enable parallel operation of multiple launch devices. They can be deployed on vehicle-mounted, ship-mounted, and ground platforms, thereby achieving integrated storage, transportation, and launch of UAV swarms and solving the problems of inconvenient storage and transportation, as well as efficient launch of UAV swarms.

[0046] Specifically, during storage and transportation, the UAV 1 and the launch unit 2 are housed inside the storage and transportation unit 3. Preferably, the UAV 1 and the launch unit 2 are arranged in an array.

[0047] When in storage and transport mode, the drone 1 is mounted on the launch unit 2. Preferably, to achieve the requirement of lightweight design, in this embodiment, the drone 1 is constructed from spliced ​​fiber composite materials. Figure 4 As shown, the UAV 1 includes an airframe 11, a payload 12, and a connecting section 13. The airframe 11 internally houses flight control and navigation systems, a structural platform, power and energy systems, aerodynamic components, etc., including but not limited to multi-rotor, fixed-wing, and loitering munitions; the power and energy systems are disposable and not recovered after launch. The payload 12 is used to perform specific tasks and internally houses, but is not limited to, optoelectronic, communication, and munitions payloads.

[0048] The connecting part 13 is fixed to the lower part of the body 11 and is used to connect with the launch unit 2. It secures the UAV 1 during storage and transportation and automatically detaches from the launch unit 2 during launch. Exemplarily, the connecting part 13 is provided with structures such as through holes, slots, and mounting brackets, which cooperate with the launch unit 2 to achieve horizontal transport on the launch unit 2 and automatic detachment and flight out under inertia at the end of the launch unit 2. In this embodiment, the connecting part 13 is provided with a fixing hole 131.

[0049] Launch unit 2 is used for the storage, transportation, and launch of UAV 1. For example... Figure 2 and Figure 5 As shown, the transmitting unit 2 includes a base 21 and a transmission component 22.

[0050] like Figure 2 As shown, the base 21 is disposed at the lower part of the launching unit 2 for fixing the transmission assembly 22 and fixing the launching unit 2 inside the storage and transportation unit 3. Exemplarily, the base 21 can be one of a truss, a profile frame, or a box structure.

[0051] The conveying assembly 22 is disposed on both sides of the base 21 and is used to convey the UAV 1 to its end for launch. The conveying assembly 22 can be one of a gear chain structure or a drive wheel synchronous belt structure. Figure 6 As shown, in this embodiment, the conveying component 22 is configured as a dual-track structure, including a synchronous belt 221, a drive wheel 222, and a drive structure. This embodiment uses a motor-driven dual-track system, which is lightweight and has high transmission efficiency, enabling rapid delivery and launch of the UAV 1.

[0052] The output end of the drive structure is connected to the drive wheel 222 and is used to drive the drive wheel 222 to rotate. The rotation speed is determined according to the launch and takeoff speed requirements of the UAV 1. Exemplarily, in this embodiment, the drive wheel is a pulley. The power source of the drive structure is an electric motor, and the drive form is a direct drive or a variable speed mechanism, which has the function of multi-motor cooperative control and speed synchronization.

[0053] The timing belt 221 is used to fix and transport the UAV 1 and support the UAV 1. The timing belt 221 and drive wheels 222 are disposed on both sides of the base 21. The timing belt 221 is disposed on the drive wheels 222 at both ends of the launching unit 2, and the upper and lower parts of the middle drive wheel 222 are in contact with the timing belt 221. Specifically, the distance between the two timing belts 221 is greater than the width of the load part 12 of the UAV 1 to prevent interference with the load part 12. In some possible embodiments, when the drive wheel 222 is a gear, the timing belt 221 can be replaced with a chain.

[0054] The connecting structure is used to connect the connecting part 13 of the UAV 1 and the timing belt 221, so that the UAV 1 is fixed to the timing belt 221 during storage and transportation, and automatically detaches from the timing belt 221 during launch. Exemplarily, the connecting structure is one of a clamp, a protrusion, a slot, and a seat. The connecting structure cooperates with the connecting part 13 to jointly achieve the connection and fixation of the UAV 1 and the timing belt 221. In this embodiment, the connecting structure is a protrusion 2211. Figure 3 As shown, the protrusion 2211 can be inserted into the fixing hole 131 of the connecting part 13 of the drone 1 to fix the drone 1. When the drone 1 is to be launched, the fixing hole 131 disengages from the protrusion 2211, and the launch can be realized.

[0055] Compared to existing technologies, the conveying assembly 22 in this embodiment includes a drive structure, a drive wheel 222, and a synchronous belt 221. The drive structure in the conveying assembly 22 rotates the drive wheel 222, driving the synchronous belt 221 on the drive wheel 222 to move, transporting the UAV 1 to the launch position. The UAV 1 is launched after detaching from the launch unit 2. The connecting part 13 of the UAV 1 is provided with a fixing hole 131, and the synchronous belt 221 is provided with a protrusion 2211. The protrusion 2211 is inserted into the fixing hole 131 for fixation. During launch, the fixing hole 131 disengages from the protrusion 2211 for launch, thereby realizing rapid fixation and rapid detachment of the UAV 1 and rapid launch, improving the fixation efficiency and launch efficiency of the UAV swarm. This embodiment uses a lightweight and efficient drive wheel transmission system, with fewer overall parts, making it easy to process and assemble.

[0056] For example, such as Figure 7As shown, the storage and transportation unit 3 has a box-type structure, including a box body 31 and a box cover 32. The box body 31 has the functions of lightweight, sealing and protection, and can be waterproof, dustproof, salt sprayproof, mildewproof, vibration-proof and impact-proof during transportation. The material is one of plastic, composite material board or metal plate. In this embodiment, the storage and transportation unit 3 adopts a modular sealed box body 31 to realize the conventional storage and transportation of UAV 1 and has the protection capability for field operations. In this embodiment, the storage and transportation unit 3 is spliced ​​with composite materials or metal plates to achieve lightweight.

[0057] One end of the housing 31 is provided with a power supply and communication interface 312 for interaction with external power supply and data communication, so as to realize power supply and control of storage and transportation unit 3 and launch unit 2; the upper part of the housing 31 is provided with a loading port 311 for loading and unloading of UAV 1.

[0058] The cover 32 is located at the other end of the housing 31, and is closed during storage and transportation, and open during launch. For example, the cover 32 can be opened from the side, top and bottom, in pairs, or by pulling. This embodiment allows for modular assembly of the entire system, enabling parallel operation of multiple launch devices, and can be deployed on vehicle-mounted, ship-mounted, or ground-based platforms to achieve rapid cluster launches.

[0059] In this embodiment, the storage and transportation unit 3 is modularly configured. For example... Figure 8 As shown, multiple storage and transportation units 3 are provided, and an array of multiple storage and transportation units 3 is arranged in the device to realize the parallel and concurrent operation of storage, transportation and launch of multiple UAVs 1 in the device.

[0060] This embodiment can be placed on the carrier platform 4, enabling fixed launch or launch during movement as needed. This embodiment allows for rapid launch of the UAV 1, and, combined with the flight control system, enables rapid launch and formation of flight formations for the UAV 1. This embodiment has wide applications and can be deployed on vehicle-mounted, ship-mounted, and ground platforms to achieve fixed launch or launch during movement.

[0061] In this embodiment, the storage and transportation unit 3 adopts a modular sealed box to realize the storage and transportation of drones, has the ability to protect against field operations, and can quickly reach the work area with the help of vehicles, ships and other means of transportation, and realize the rapid and continuous launch of drones, quickly form a cluster, and quickly carry out collaborative operation tasks.

[0062] This embodiment has the advantages of low cost and lightweight design. The structure of the UAV 1 is made of standardized fiber composite materials, the storage and transportation unit 3 is made of composite materials or metal plates, and the launch unit 2 adopts a lightweight pulley transmission system. The overall structure has fewer parts and is easy to process and assemble.

[0063] The above description is only a preferred embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in the present utility model should be included within the protection scope of the present utility model.

Claims

1. An integrated device for launching, storing, and transporting unmanned aerial vehicles (UAVs) in clusters, characterized in that, It includes a launch unit (2) and a storage and transportation unit (3); multiple storage and transportation units (3) are provided; The launching unit (2) is disposed within the storage and transportation unit (3); the launching unit (2) includes a transmission component (22); The transmission component (22) is connected to the connection part (13) of the UAV (1), and the transmission component (22) can transmit the UAV (1) to the launch position; the connection part (13) can be fixed or detached from the transmission component (22); The transmission assembly (22) includes a drive structure, a synchronous belt (221), and a drive wheel (222); or The transmission assembly (22) includes a drive structure, a chain, and gears.

2. The integrated launch, storage, and transportation device for unmanned aerial vehicle (UAV) swarms according to claim 1, characterized in that, The drive wheel (222) is connected to the drive structure, and the drive structure is capable of driving the drive wheel (222) to rotate; The timing belt (221) is disposed on the drive wheel (222); the timing belt (221) can run as the drive wheel (222) rotates.

3. The integrated launch, storage, and transportation device for unmanned aerial vehicle (UAV) swarms according to claim 2, characterized in that, A connection structure is provided on the synchronous belt (221); the connection part (13) is connected to the connection structure.

4. The integrated launch, storage, and transportation device for unmanned aerial vehicles (UAVs) swarms according to claim 3, characterized in that, The connecting part (13) is provided with a fixing hole (131), and the connecting structure is a protrusion (2211), which can be inserted into the fixing hole (131).

5. The integrated launch, storage, and transportation device for unmanned aerial vehicle (UAV) swarms according to claim 1, characterized in that, The transmitting unit (2) also includes a base (21), and the transmitting components (22) are symmetrically arranged on both sides of the base (21).

6. The integrated launch, storage, and transportation device for unmanned aerial vehicle (UAV) swarms according to claim 1, characterized in that, The chain is provided with a connecting structure; the connecting part (13) is connected to the connecting structure.

7. The integrated launch, storage, and transportation device for unmanned aerial vehicle (UAV) swarms according to claim 1, characterized in that, Multiple storage and transportation units (3) are arranged in an array.

8. The integrated launch, storage, and transportation device for unmanned aerial vehicle (UAV) swarms according to claim 1, characterized in that, The storage and transportation unit (3) includes a box (31) and a box cover (32); The lid (32) is located at the end of the box body (31); The upper part of the box (31) is provided with a loading port (311), which is used for loading and unloading the UAV (1).

9. The integrated launch, storage, and transportation device for unmanned aerial vehicle (UAV) swarms according to claim 8, characterized in that, The housing (31) is provided with a power supply and communication interface (312) at the end relative to the housing cover (32).

10. The integrated launch, storage, and transportation device for unmanned aerial vehicle (UAV) swarms according to claim 8, characterized in that, The opening method of the box cover (32) is one of the following: side opening, top and bottom opening, double opening, or pull-out type.

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