Transport frame for a drone body structure

CN224899942UActive Publication Date: 2026-10-27WEIHAI GUANGWEI COMPOSITE MATERIALS TECH CO LTD
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Patent Information

Application Number
CN202522429170.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-11-17
Publication Date
2026-10-27
Estimated Expiration
2035-11-17

AI Technical Summary

Technical Problem

[0003]但无人机运输多依赖人工拆卸机翼、尾撑等部件,再通过吊车等设备将机体吊至简易托架,不仅需大量人力协同,且拆装耗时久,同时部分运输架无移动部件和便捷装卸结构,转运时需额外借助其他设备,缺乏一体化的装卸 - 转运技术设计,严重影响部署效率

Benefits of technology

[0014]1.本实用新型所述的一种无人机机体结构的运输架,通过采用四角固定的方式,增加无人机与装置的连接紧密性,减少无人机固定于装置时的抖动问题,提升装置的实用性。

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model belongs to the transport frame technical field, concretely is a kind of transport frame of unmanned aerial vehicle body structure, including bearing plate, bearing plate top consolidation clamping seat, the clamping seat is equipped with four, clamping seat side wall rotation connection first fixed block, first fixed block side wall rotation connection first fixed link, first fixed block side wall consolidation first handle, bearing plate top consolidation lock catch, lock catch is located opposite first fixed block and is connected with bearing plate, bearing plate top is provided with slot, bearing plate bottom consolidation base frame, the both ends of base frame side wall are slidably connected sliding rod, two the sliding rod side wall consolidation second fixed link, by above-mentioned structure, adopt the mode of four corners fixed, increase the connection tightness of unmanned aerial vehicle and device, reduce the shaking problem when unmanned aerial vehicle is fixed in device, improve the practicability of device.
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Description

Technical Field

[0001] This utility model belongs to the field of transport frame technology, specifically a transport frame for the body structure of an unmanned aerial vehicle (UAV). Background Technology

[0002] Drones are increasingly used in logistics, surveying, power line inspection, disaster prevention and other fields. Drones are also developing towards larger size and more multifunctionality. Generally, when drones are delivered to customers, due to limitations in technology such as range and communication, they are disassembled and transported to the customer by ground transportation before being reassembled.

[0003] However, drone transportation relies heavily on manual disassembly of components such as wings and tail booms, followed by hoisting the drone onto a simple support frame using cranes or other equipment. This not only requires a large amount of manpower but also takes a long time to disassemble and assemble. Furthermore, some transport frames lack moving parts and convenient loading and unloading structures, requiring additional equipment for transfer. The lack of an integrated loading, unloading, and transfer technology design severely impacts deployment efficiency.

[0004] Therefore, this utility model provides a transport frame for the body structure of an unmanned aerial vehicle (UAV). Utility Model Content

[0005] To overcome the shortcomings of existing technologies and address the issues raised in the background section regarding the lack of moving parts and convenient loading / unloading structures, the need for additional equipment during transport, the absence of integrated loading / unloading and transport technology design, and the resulting serious impact on deployment efficiency.

[0006] The technical solution adopted by this utility model to solve its technical problem is as follows: The transport frame of the drone body structure of this utility model includes a bearing plate, a bracket fixed to the top of the bearing plate, four brackets are provided, a first fixing block is rotatably connected to the side wall of the bracket, a first fixing rod is rotatably connected to the side wall of the first fixing block, a first handle is fixed to the side wall of the first fixing block, a lock is fixed to the top of the bearing plate, the lock is located opposite the first fixing block and engages with the bearing plate, and a slot is opened on the top of the bearing plate. Through the above structure, the connection between the drone and the device is increased by using a four-corner fixing method, the shaking problem when the drone is fixed to the device is reduced, and the practicality of the device is improved.

[0007] Preferably, the bottom of the support plate is fixed to the base frame, and each end of the side wall of the base frame is slidably connected to a sliding rod. The two sliding rods are fixed to the side walls of the second fixed rod. Through the above structure, the lever principle is adopted, which enables the device to be operated by a single person, reduces the manpower consumption of drone transfer, makes the device faster and more convenient in the loading and unloading process, and improves the practicality of the device.

[0008] Preferably, a second fixing block is fixed to each side of the base frame, and a locking component is fixedly and rotatably connected to both sides of the second fixing rod. Through the above structure, a locking function is added, which reduces the component unfolding caused by bumps during the transfer of the device, thereby improving the integrity of the device and enhancing its practicality.

[0009] Preferably, the second handle is fixed to the side wall of the second fixing rod. Through the above structure, the auxiliary components are added to enable the device to be quickly and conveniently unfolded when it needs to be unfolded, thereby improving the practicality and ease of operation of the device.

[0010] Preferably, omnidirectional wheels are fixed to both ends of the bottom of the base frame and omnidirectional wheels are fixed to both ends of the bottom of the second fixing rod. Through the above structure, the addition of the moving component allows the device to be moved by one person during the transfer process, reducing the manpower required to move the drone and improving the practicality and flexibility of the device.

[0011] Preferably, the base frame, sliding rod, second fixed rod, and bearing plate are made of stainless steel. Through the above structure, the use of stainless steel increases the metal hardness of the device components, improves the load-bearing capacity of the device, increases the load capacity of the device, reduces device damage, and improves the practicality and durability of the device.

[0012] Preferably, the base frame, sliding rod, second fixed rod, and bearing plate are coated with a wear-resistant coating. Through the above structure and the use of a wear-resistant coating, the wear of the device during daily use is reduced, thereby extending the service life of the device. The wear-resistant coating also increases the aesthetic appearance of the device and enhances its practicality and durability.

[0013] The beneficial effects of this utility model are as follows:

[0014] 1. The transport frame for the drone body structure described in this utility model increases the tightness of the connection between the drone and the device by using a four-corner fixing method, reduces the shaking problem when the drone is fixed to the device, and improves the practicality of the device.

[0015] 2. The transport frame for the drone body structure described in this utility model adopts a lever principle, which enables the device to be operated by a single person, reduces the manpower consumption for drone transfer, makes the device faster and more convenient during loading and unloading, and improves the practicality of the device. Attached Figure Description

[0016] The present invention will be further described below with reference to the accompanying drawings.

[0017] Figure 1 This is a perspective view of the present invention;

[0018] Figure 2 This is a schematic diagram of the structure of the bearing plate in this utility model;

[0019] Figure 3 This is a schematic diagram of the base frame structure in this utility model;

[0020] Figure 4 This is a schematic diagram of the universal wheel in this utility model;

[0021] In the diagram: 1. Support plate; 11. Card holder; 12. First fixing block; 13. First fixing rod; 14. Lock; 15. First handle; 16. Slot; 2. Base frame; 21. Sliding rod; 22. Second fixing rod; 3. Locking assembly; 31. Second fixing block; 4. Second handle; 5. Caster wheel. Detailed Implementation

[0022] 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 skilled in the art without creative effort are within the protection scope of the present utility model.

[0023] Specific implementation examples are given below.

[0024] like Figures 1 to 4 As shown in the figure, a transport frame for a drone body structure according to an embodiment of the present invention includes a support plate 1, a mounting bracket 11 fixed to the top of the support plate 1, four mounting brackets 11, a first fixing block 12 rotatably connected to the side wall of the mounting bracket 11, a first fixing rod 13 rotatably connected to the side wall of the first fixing block 12, a first handle 15 fixed to the side wall of the first fixing block 12, and a locking buckle 14 fixed to the top of the support plate 1. The locking buckle 14 is located opposite the first fixing block 12 and engages with the support plate 1. A slot 16 is provided on the top of the support plate 1. During operation, the drone is placed on the top of the support plate 1, and then the first fixing block 12 is rotated to make the first fixing rod 13 engage with the first fixing rod 14. The fixed block 12 drives the first fixed rod 13, which engages with the latch 14. The drone frame is placed between the first fixed rod 13 and the latch 14. Then, the first handle 15 is pressed down to lock the first fixed block 12. The four-corner design increases the stability of the device for the drone and reduces the shaking of the drone during transportation. At the same time, the slot 16 reduces the manufacturing cost of the device and improves its practicality. Through the above structure, the four-corner fixing method increases the tightness of the connection between the drone and the device, reduces the shaking problem when the drone is fixed to the device, and improves the practicality of the device.

[0025] like Figures 1 to 4As shown, the base frame 2 is fixed to the bottom of the support plate 1. Sliding rods 21 are slidably connected to both ends of the side wall of the base frame 2. The side walls of the two sliding rods 21 are fixed to second fixed rods 22. During operation, pulling the second fixed rods 22 causes the sliding rods 21 to slide, thus unfolding the device. The second fixed rods 22 are then lifted and placed in the rear compartment of the vehicle. The base frame 2 is then lifted and pushed, causing the sliding rods 21 to engage with the base frame 2 through the sliding assembly, completing the transfer of the device and improving its practicality. Through the above structure, using the lever principle, the device can be operated by a single person, reducing the manpower consumption of drone transfer and making the loading and unloading process faster and more convenient, thus improving the practicality of the device.

[0026] like Figures 1 to 4 As shown, a second fixing block 31 is fixed to each side of the base frame 2, and a locking component 3 is fixedly and rotatably connected to both sides of the second fixing rod 22. During operation, to prevent the base frame 2 from unfolding and separating from the sliding rod 21 due to bumps during the transfer of the device on the vehicle, after the device is placed on the vehicle, the second fixing rod 22 is fitted to the side wall of the base frame 2, and then the locking component 3 is rotated so that the opening of the side wall of the locking component 3 is engaged with the second fixing block 31. The bottom frame of the device is fixed by the locking components 3 on both sides in cooperation with the second fixing block 31, thereby improving the stability of the device. Through the above structure, a locking function is added to reduce the unfolding of components due to bumps during the transfer of the device, thereby improving the integrity of the device and enhancing its practicality.

[0027] like Figures 1 to 4 As shown, the second handle 4 is fixed to the side wall of the second fixing rod 22. During operation, the locking component 3 is unlocked from the second fixing block 31, and then the second handle 4 is pulled to make the second handle 4 drive the second fixing rod 22 to slide quickly, so that the device can be quickly unfolded, making it easy to transfer the device from the vehicle to the ground and improving the practicality of the device. Through the above structure, the auxiliary component is added to enable the device to be unfolded quickly and conveniently when it needs to be unfolded, improving the practicality and ease of operation of the device.

[0028] like Figures 1 to 4 As shown, universal wheels 5 are fixed to both ends of the bottom of the base frame 2, and universal wheels 5 are fixed to both ends of the bottom of the second fixing rod 22. During operation, when the drone needs to be moved, the drone is pushed, and the device is fixed to the drone through the fixing components, so that the drone drives the carrier plate 1 to move. The carrier plate 1 drives the base frame 2 to move, so that the bottom universal wheels 5 rotate, allowing the device to be moved quickly. At the same time, the universal design allows the device to turn freely, improving the practicality and flexibility of the device. Through the above structure, the addition of the moving components allows the device to be moved by one person during the transfer process, reducing the manpower consumed in moving the drone and improving the practicality and flexibility of the device.

[0029] like Figures 1 to 4 As shown, the base frame 2, sliding rod 21, second fixed rod 22, and bearing plate 1 are made of stainless steel. During operation, the stainless steel material increases the metal hardness of the device components, improves the load-bearing capacity of the device, increases the load capacity of the device, and at the same time reduces the damage to the device, thus improving the practicality and durability of the device. Through the above structure, the use of stainless steel material increases the metal hardness of the device components, improves the load-bearing capacity of the device, increases the load capacity of the device, and at the same time reduces the damage to the device, thus improving the practicality and durability of the device.

[0030] like Figures 1 to 4 As shown, the base frame 2, sliding rod 21, second fixed rod 22, and bearing plate 1 are coated with a wear-resistant coating. During operation, the wear-resistant coating reduces wear on the device during daily use, thus extending its service life. The wear-resistant coating also enhances the aesthetics of the device, improving its practicality and durability.

[0031] During operation, the drone is placed on top of the support plate 1. Then, the first fixing block 12 is rotated, causing it to drive the first fixing rod 13, which engages with the latch 14. The drone frame is then placed between the first fixing rod 13 and the latch 14. Finally, the first handle 15 is pressed down to lock the first fixing block 12. The four-corner design increases the stability of the device for the drone, reducing shaking during transportation. Simultaneously, the slot 16 reduces manufacturing and usage costs, improving the device's practicality. Pulling the second fixing rod 22 further secures the second fixing block. Rod 22 drives sliding rod 21 to slide, causing the device to unfold. The second fixing rod 22 is then lifted and placed in the vehicle's rear compartment. The base frame 2 is then lifted and pushed, causing the sliding component to engage the sliding rod 21 with the base frame 2, completing the device's transfer and improving its practicality. To prevent the base frame 2 from separating from the sliding rod 21 due to bumps during vehicle transfer, after the device is placed in the vehicle, the second fixing rod 22 is fitted against the side wall of the base frame 2. Then, the locking component 3 is rotated, causing the opening on the side wall of the locking component 3 to engage with the second fixing block 31. The device is secured by locking components 3 on both sides and the second fixing block 31, improving stability. Unlocking the locking components 3 and the second fixing block 31, and then pulling the second handle 4, causes the second fixing rod 22 to slide quickly, allowing the device to unfold rapidly and be easily transferred from the vehicle to the ground, enhancing its practicality. When transferring the drone, push it forward and secure the device to it using the fixing components. The drone then moves the support plate 1, which in turn moves the base frame 2, causing the bottom casters 5 to rotate, enabling rapid transfer. The omnidirectional design allows for free steering, enhancing practicality and flexibility. Stainless steel materials increase the metal hardness of the components, improving load-bearing capacity and reducing damage, thus enhancing practicality and durability. A wear-resistant coating reduces wear during daily use, extending the device's lifespan. The wear-resistant coating also enhances the device's appearance, improving its practicality and durability.

[0032] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely illustrative of the principles of this utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claimed utility model. The scope of protection of this utility model is defined by the appended claims and their equivalents.

Claims

1. A transport frame for a UAV fuselage structure, comprising a support plate (1); characterized in that: The top of the bearing plate (1) is fixed with a bracket (11); four brackets (11) are provided; the side wall of the bracket (11) is rotatably connected to a first fixing block (12); the side wall of the first fixing block (12) is rotatably connected to a first fixing rod (13); the side wall of the first fixing block (12) is fixed with a first handle (15); the top of the bearing plate (1) is fixed with a latch (14); the latch (14) is located opposite the first fixing block (12) and engages with the bearing plate (1); the top of the bearing plate (1) is provided with a slot (16).

2. The transport frame for a UAV fuselage structure according to claim 1, characterized in that: The bottom of the bearing plate (1) is fixed to the base frame (2); each end of the side wall of the base frame (2) is slidably connected to a sliding rod (21); the side walls of the two sliding rods (21) are fixed to a second fixing rod (22).

3. The transport frame for a UAV fuselage structure according to claim 2, characterized in that: The base frame (2) has a second fixing block (31) fixed on each side; the second fixing rod (22) has a locking assembly (3) fixedly and rotatably connected on both sides.

4. The transport frame for a UAV fuselage structure according to claim 3, characterized in that: The second handle (4) is fixed to the side wall of the second fixing rod (22).

5. The transport frame for a UAV fuselage structure according to claim 4, characterized in that: The bottom ends of the base frame (2) are each fixed with a caster wheel (5); the bottom ends of the second fixing rod (22) are each fixed with a caster wheel (5).

6. The transport frame for a UAV fuselage structure according to claim 5, characterized in that: The base frame (2), sliding rod (21), second fixing rod (22), and bearing plate (1) are made of stainless steel.

7. The transport frame for a UAV fuselage structure according to claim 6, characterized in that: The base frame (2), sliding rod (21), second fixing rod (22), and bearing plate (1) are coated with a wear-resistant coating.