A convenient, solderless, and quick-plug-in UAV payload structure

Abstract

This utility model relates to the field of payload structure technology and discloses a convenient, weld-free, and quick-plug-in UAV mission payload structure, including a transport box, and further comprising: a plug-in part mounted on the transport box; an mounting part disposed on the transport box; and a throwing part mounted on the transport box. The plug-in part includes a cover plate slidably connected to the transport box, the cover plate having a limiting groove. A connector is provided on the transport box, wherein the transport box and the cover plate are slidably connected by a slot. The connector includes an insertion port on the transport box and the cover plate. A buckle is provided on the left side of the transport box, the buckle being adapted to the limiting groove. This utility model, by setting up a plug-in part, solves the problem of inconsistency in payload connection and use caused by the need for secondary adaptation after changing the flight platform, which is time-consuming, labor-intensive, inefficient, and unable to achieve high efficiency in field operations.

Description

Technical Field

[0001] This utility model relates to the field of load structure technology, specifically a convenient, solder-free, and quick-plug-in UAV mission load structure. Background Technology

[0002] With the continuous advancement of drone technology, drones are becoming increasingly common in daily life. Drone payload modules, through modular design, significantly shorten flight preparation time for specific scenarios such as material transportation and performance activities. They simplify and integrate wiring connections, eliminating the need for flight cables and adopting a modular quick-connect method that supports rapid plugging and unplugging, enabling quick changes to flight missions. This reduces the burden on drone operators. The development of drone payloads is synchronized with the development of drone technology. The flight mission of each drone is determined by its payload. In specific application scenarios, payload changes are often complex and cumbersome, while modular payloads provide convenience for quick changes to flight missions, greatly improving operational efficiency.

[0003] However, traditional drones come in a wide variety of models, requiring secondary adaptation with multiple aircraft, thus presenting several drawbacks, including:

[0004] 1. After changing the flight platform, a second adaptation is required, which leads to inconsistencies in the connection and use of the payload, which is time-consuming, labor-intensive, and inefficient, and cannot achieve the high efficiency of field operation tasks.

[0005] 2. Although there are many types of drones, their flight missions are similar, and a single payload is difficult to achieve universal compatibility with multiple models;

[0006] 3. Changing traditional UAV flight missions depends on changing the mission payload, which is not only time-consuming but also costly. This shortcoming can be made up for by modular integration design of the payload. Utility Model Content

[0007] The purpose of this utility model is to provide a convenient, solderless, and quick-plug-in UAV mission payload structure. By setting up a plug-in part, it solves the problem that after changing the flight platform, secondary adaptation is required, which leads to inconsistency in payload connection and use, is time-consuming, labor-intensive, inefficient, and unable to achieve high efficiency in field operations.

[0008] To solve the above-mentioned technical problems, this utility model is achieved through the following technical solution:

[0009] This utility model relates to a convenient, solderless, and quick-plug-in UAV mission payload structure, comprising a transport box, and further comprising: a plug-in part mounted on the transport box; an mounting part disposed on the transport box; and a throwing part mounted on the transport box. The plug-in part includes a cover plate slidably connected to the transport box, the cover plate having a limiting groove, and a connector being provided on the transport box. The transport box and the cover plate are slidably connected via a slot. The connector includes an insertion port on the transport box and the cover plate. A buckle is provided on the left side of the transport box, the buckle being adapted to the limiting groove. Both the limiting groove and the buckle are frosted, and the limiting groove is adapted to the buckle.

[0010] Furthermore, the mounting part includes a mounting plate disposed inside the transport box, and a plurality of pressure blocks are fixedly connected to the bottom of the mounting plate. A second connector is provided on the pressure blocks. The lengths of the plurality of pressure blocks are arranged from high to low, and each pressure block is provided with an adaptation groove. The second connector includes a fixing groove formed on the plurality of pressure blocks.

[0011] Furthermore, the throwing unit includes a hinge plate disposed at the bottom of the transport box. The hinge plate and the transport box are provided with two mounting slots and two hinges. The two mounting slots are adapted to the two hinges. The hinge plate is provided with a slot. The mounting slots are used to place the hinges, and the hinge plate and the transport box are hinged together by the hinges.

[0012] This utility model has the following beneficial effects:

[0013] 1. This utility model achieves solderless connection and quick plug-in / plug-out functionality by setting up a plug-in / plug-out part and using a slot structure designed in the middle part of the module. It is convenient to manage and portable, and supports quick replacement. This effectively avoids the complicated wiring connection and mechanical installation process.

[0014] 2. This utility model has an installation part with a semi-circular groove at the bottom. This design is intended to accommodate a large number of cylindrical munitions, and can be used with various UAV models and munition models, thereby avoiding the decline in mission performance caused by incompatibility between the UAV models or the munition sizes.

[0015] 3. This utility model features a throwing unit where all loads are connected via slide rails. The slide rails are permanently fixed to the aircraft body, and the convenient slide rail module can be permanently linked to the fuselage with minimal impact on flight performance.

[0016] Of course, any product implementing this utility model does not necessarily need to achieve all of the advantages described above at the same time. Attached Figure Description

[0017] To more clearly illustrate the technical solutions of the embodiments of this utility model, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0018] Figure 1 This is a partial cross-sectional view of the overall structure of this utility model;

[0019] Figure 2 This is a schematic diagram of the overall structure of this utility model;

[0020] Figure 3 This utility model Figure 2 A magnified structural diagram of A in the middle;

[0021] Figure 4 This is a partial cross-sectional view of the rear side of the present invention.

[0022] Figure 5 This utility model Figure 4 A magnified structural diagram of B in the diagram;

[0023] Figure 6 This is an exploded structural diagram of the throwing part of this utility model;

[0024] Figure 7 This utility model Figure 6 A magnified structural diagram of C;

[0025] Figure 8 This is a partial cross-sectional view of the mounting section of this utility model.

[0026] The attached diagram lists the components represented by each number as follows:

[0027] In the diagram: 111, transport box; 2, insertion / removal part; 211, cover plate; 212, limiting groove; 213, insertion port; 214, buckle; 3, mounting part; 311, mounting plate; 312, pressure block; 313, fixing groove; 4, throwing part; 411, hinge plate; 412, mounting groove; 413, hinge; 414, slot; 415, limiting plate. 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. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0029] Please see Figures 1-8 As shown, this utility model is a convenient, solderless, and quick-plug-in UAV mission payload structure, including a transport box 111, and further including: a plug-in part 2, which is installed on the transport box 111; a mounting part 3, which is disposed on the transport box 111; and a throwing part 4, which is installed on the transport box 111.

[0030] The plug-in / plug-out part 2 includes a cover plate 211 slidably connected to the transport box 111. The cover plate 211 has a limiting groove 212. The transport box 111 is provided with a connector. The transport box 111 and the cover plate 211 are slidably connected by a slot. The connector includes an insertion port 213 on the transport box 111 and the cover plate 211. A buckle 214 is provided on the left side of the transport box 111. The buckle 214 is adapted to the limiting groove 212. Both the limiting groove 212 and the buckle 214 are frosted. The plug-in / plug-out part 2 provides convenient management and portability, and supports quick replacement. This effectively avoids the complicated wiring connection and mechanical installation process.

[0031] The mounting part 3 includes a mounting plate 311 disposed inside the transport box 111. Several pressure blocks 312 are fixedly connected to the bottom of the mounting plate 311, and a second connector is provided on the pressure blocks 312. The lengths of the pressure blocks 312 are arranged from high to low, and each pressure block 312 is provided with an adaptation groove. The second connector includes a fixing groove 313 provided on the pressure blocks 312. By setting the mounting part 3, the decrease in mission performance caused by incompatibility of machine type or ammunition size is avoided.

[0032] The throwing unit 4 includes a hinge plate 411 located at the bottom of the transport box 111. The hinge plate 411 and the transport box 111 are provided with two mounting slots 412 and two hinges 413. The two mounting slots 412 are adapted to the two hinges 413. The hinge plate 411 is provided with a slot 414. The mounting slots 412 are used to place the hinges 413. The hinge plate 411 and the transport box 111 are hinged together by the hinges 413. By providing the throwing unit 4, the portable slide rail module can be permanently connected to the fuselage with minimal impact on flight performance.

[0033] In use, the transport box 111 can be opened by pulling the cover plate 211. When pulled, the limiting groove 212 on the cover plate 211 will generate a certain friction with the buckle 214. Thus, through the limiting groove 212 and the buckle 214 designed on the module, the solderless connection of the circuit and the quick plug-in and plug-out function are realized. The buckle 214 is designed to realize the quick plug-in and plug-out and fixing function of the mechanical connection. After opening the transport box 111, the ammunition is placed in the transport box 111, and then the mounting plate 311 is installed on top of the ammunition. At this time, the pressure block 312 on the mounting plate 311 will fix the ammunition, thus achieving the fixing effect. After fixing, the cover plate 211 is closed. Then the cover plate 211 is inserted into the transport box 111. When inserted, the limiting groove 212 will wrap around the buckle 214. The inner wall of the limiting groove 212 and the buckle 214 are in contact with each other. 4. Upon contact, a certain frictional force will be generated. As the cover plate 211 is continuously inserted, the frictional force will increase, thereby achieving the effect of fixing the cover plate 211. After fixing, the transport box 111 can be fixed on the drone. The slide rail module is connected to the aircraft fuselage through its middle part. After fixing, it can take off. When it is necessary to eject the ammunition, the electric servo mechanism on the slot 414 will open the hinge plate 411. When the hinge plate 411 is open, the hinge 413 will open and close. After opening and closing, the hinge plate 411 will be open. At this time, the ammunition will fall, thereby achieving the effect of ejecting the ammunition. After ejecting the ammunition, the electric servo mechanism on the slot 414 will be activated to close the hinge plate 411. When closing, the limit plate 415 will limit the closing position of the hinge plate 411 to prevent the hinge 413 from excessively contracting during the movement.

[0034] The preferred embodiments of this utility model disclosed above are merely illustrative of the present utility model. These preferred embodiments do not exhaustively describe all details, nor do they limit the utility model to the specific implementations described. Clearly, many modifications and variations can be made based on the content of this specification. This specification selects and specifically describes these embodiments to better explain the principles and practical applications of this utility model, thereby enabling those skilled in the art to better understand and utilize it. This utility model is limited only by the claims and their full scope and equivalents.

Claims

1. A convenient, solderless, and quick-plug-in UAV mission payload structure, comprising a transport box (111), characterized in that, Also includes: A plug-in part (2) is mounted on a transport box (111); Mounting part (3), which is provided on transport box (111); Throwing part (4), said throwing part (4) is mounted on transport box (111); The plug-in part (2) includes a cover plate (211) slidably connected to the transport box (111), the cover plate (211) having a limiting groove (212), and the transport box (111) being provided with a connector. The transport box (111) and the cover plate (211) are slidably connected by a slot.

2. The convenient, solderless, and quick-plug-in UAV mission payload structure according to claim 1, characterized in that, The mounting part (3) includes a mounting plate (311) disposed in the transport box (111), and a plurality of pressure blocks (312) are fixedly connected to the bottom of the mounting plate (311), and a connecting piece 2 is provided on the pressure block (312); Among them, several pressure blocks (312) are arranged from high to low in length, and each pressure block (312) is provided with an adapter groove.

3. The convenient, solderless, and quick-plug-in UAV mission payload structure according to claim 2, characterized in that, The throwing part (4) includes a hinge plate (411) disposed at the bottom of the transport box (111). The hinge plate (411) and the transport box (111) are provided with two mounting slots (412). The hinge plate (411) and the transport box (111) are provided with two hinges (413). The two mounting slots (412) are adapted to the two hinges (413). The hinge plate (411) is provided with a slot (414). The mounting slot (412) is used to place the hinge (413), and the hinge plate (411) and the transport box (111) are hinged together by the hinge (413).

4. The convenient, solderless, and quick-plug-in UAV mission payload structure according to claim 3, characterized in that, The connector includes an insertion port (213) on the transport box (111) and the cover plate (211), and a buckle (214) is provided on the left side of the transport box (111), which is adapted to the limiting groove (212). The limiting groove (212) and the buckle (214) are both frosted, and the limiting groove (212) and the buckle (214) are compatible.

5. The convenient, solderless, and quick-plug-in UAV mission payload structure according to claim 4, characterized in that, The second connector includes fixing grooves (313) formed on a plurality of pressure blocks (312).

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