A vehicle-mounted unmanned aerial vehicle package box

By using segmented fixing components and foam materials, the design resolves the conflict between cost and stability in drone packaging, providing a low-cost and stable packaging solution that is particularly suitable for vehicle-mounted transportation of delta-wing propeller drones.

CN224376360UActive Publication Date: 2026-06-19ZHENGZHOU HONGYU SPECIAL VEHICLE CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
ZHENGZHOU HONGYU SPECIAL VEHICLE CO LTD
Filing Date
2025-06-24
Publication Date
2026-06-19

AI Technical Summary

Technical Problem

Existing drone packaging boxes, while reducing costs, lack stability and reliability, especially in providing insufficient protection for delta-wing propeller drones.

Method used

The design employs segmented fixing components, including fixing components for the head, fuselage, propellers, and side wings. Combined with foam materials and limiting columns, the support structure is enhanced to ensure stable packaging of all parts of the drone.

Benefits of technology

It achieves low-cost drone packaging boxes, improves packaging stability and reliability, prevents damage to drones during transportation, and is suitable for vehicle transport.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN224376360U_ABST
    Figure CN224376360U_ABST
Patent Text Reader

Abstract

This utility model relates to the field of packaging and transportation technology and is a vehicle-mounted drone packaging box, comprising a box slot and a box lid. A head fixing component, a fuselage fixing component, and a spiral fixing component are arranged sequentially from front to back in the center of the box slot. The head fixing component and the spiral fixing component respectively contact the front and rear walls of the box slot. Two symmetrical side wing fixing components are closely attached to the inner walls on both sides of the box slot. Each of the head fixing component, fuselage fixing component, spiral fixing component, and side wing fixing component includes an upper pressure unit slot and a lower support unit slot that respectively attach to the corresponding upper and lower surfaces of the drone. A rear support block is provided between the spiral fixing component and each side wing fixing component, and the rear support block respectively contacts the rear wall of the box slot and the corresponding rear fuselage of the drone. This drone packaging box reduces costs while improving packaging stability and reliability.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] This utility model relates to the field of packaging and transportation technology, and in particular to a drone packaging box for vehicle-mounted transportation. Background Technology

[0002] Currently, most drone packaging boxes on the market use a single piece of EVA foam to wrap the drone, but this structure has high manufacturing and processing costs and does not meet market demand. Chinese invention patent CN113460506B discloses a lightweight and high-strength drone packaging box and its assembly method, which adopts a segmented ring wrapping method in the packaging box to reduce material and processing costs. However, for delta-wing drones with large wingspans, this existing method lacks stability and reliability. Utility Model Content

[0003] In order to overcome the shortcomings of the prior art and solve the existing technical problems, this utility model discloses a drone packaging box for vehicle transportation, which improves packaging stability and reliability while reducing costs.

[0004] To achieve the above objectives, the present invention adopts the following technical solution:

[0005] A vehicle-mounted drone packaging box includes a box slot and a box lid. The box slot has a head fixing component, a fuselage fixing component, and a spiral fixing component arranged sequentially from front to back in its central section. The head fixing component and the spiral fixing component are respectively in contact with the front and rear walls of the box slot. Two symmetrical side wing fixing components are closely attached to the inner walls on both sides of the box slot. Each of the head fixing component, fuselage fixing component, spiral fixing component, and side wing fixing component includes an upper pressure unit slot block and a lower support unit slot block that respectively attach to the corresponding upper and lower surfaces of the drone. A rear support block is provided between the spiral fixing component and each side wing fixing component, and the rear support block is respectively in contact with the rear wall of the box slot and the corresponding rear side of the drone fuselage.

[0006] Furthermore, fixed limit columns are erected at the bottom of the slots corresponding to the head fixing component, fuselage fixing component, spiral fixing component and the two sides of the rear support block, as well as the front and rear positions of the side wing fixing component.

[0007] Furthermore, two side support columns are symmetrically fixed on both sides of the front end of the bottom of the box groove, and two central support columns are symmetrically fixed in the middle of the front end of the bottom of the box groove. The central support columns are fixedly connected to the limiting columns on the corresponding side of the body fixing assembly by cross bracing.

[0008] Furthermore, a nozzle fixing assembly is provided at the front end of the bottom of the tank, and the two ends of the nozzle fixing assembly are respectively in contact with the central support column and the side support column.

[0009] Furthermore, the head fixing component, fuselage fixing component, spiral fixing component, side wing fixing component, and rear support block are all made of foam material.

[0010] Furthermore, the rear side of the box cover is hinged to the top of the rear wall of the box groove, and the front side of the box cover is detachably connected to the top of the front wall of the box groove via a buckle.

[0011] Furthermore, multiple spaced reinforcing strips are fixed to the outer surfaces of both the box groove and the box cover.

[0012] By adopting the technical solution described above, this utility model has the following beneficial effects:

[0013] The vehicle-mounted transport drone packaging box disclosed in this utility model adopts a segmented packaging method for the central shaft of the delta-wing propeller drone and a side wing support packaging method to ensure protection of the main parts of the drone and to ensure that the entire body can be placed stably. By using various fixing components and rear support blocks to contact the inner wall of the box, the risk of movement in the packaging box is reduced, thereby meeting the product packaging requirements, having good storage performance, and being able to meet the transfer and transportation functions. It is particularly suitable for low-cost drone packaging.

[0014] In addition, the use of limiting columns, side support columns, central support columns, and cross braces not only supports the lid of the box, increases structural strength, and prevents the product from being squeezed by the weight of the stacked packaging boxes, but also allows for further positioning of each fixed component, increasing the convenience of packaging and the stability of vehicle transportation. Attached Figure Description

[0015] Figure 1 This is a three-dimensional schematic diagram of the embodiment structure of this utility model;

[0016] Figure 2 This is a top view of the structure of this utility model;

[0017] Figure 3 yes Figure 2 A schematic diagram of the AA-direction cross-section structure;

[0018] Figure 4 yes Figure 3 Schematic diagram of the BB-direction cross-section structure.

[0019] In the diagram: 1. Box slot; 2. Head fixing assembly; 3. Fuselage fixing assembly; 4. Spiral fixing assembly; 5. Side wing fixing assembly; 6. Rear support block; 7. Limiting column; 8. Side support column; 9. Central support column; 10. Horizontal support rod; 11. Nozzle fixing assembly. Detailed Implementation

[0020] The technical solution of this utility model will be described below with reference to the accompanying drawings of the embodiments of this utility model. In the description, it should be understood that if there are terms such as "upper", "lower", "front", "rear", "left", "right" indicating the orientation or positional relationship, they are only corresponding to the drawings of this utility model for the convenience of describing this utility model, and do not indicate or imply that the device or element referred to must have a specific orientation.

[0021] Combined with appendix Figure 1-4 The vehicle-mounted transport drone packaging box includes a box slot 1 and a box cover. The box cover is not shown in the attached drawing. The rear side of the box cover is hinged to the top of the rear wall of the box slot 1. The front side of the box cover is detachably connected to the top of the front wall of the box slot 1 via a buckle, which facilitates opening and closing the box cover. As needed, multiple spaced reinforcing strips are fixed to the outer surfaces of both the box slot 1 and the box cover to increase structural strength and facilitate forklift and hoisting transportation.

[0022] The center of the tank 1 contains, from front to back, a head fixing component 2, a fuselage fixing component 3, and a propeller fixing component 4. The head fixing component 2 primarily covers the drone's nose, the fuselage fixing component 3 primarily covers the drone's neck and wings, and the propeller fixing component 4 primarily covers the drone's tail. It requires ample space to accommodate the propeller and prevent damage. The head fixing component 2 and the propeller fixing component 4 contact the front and rear walls of the tank 1, respectively. Two symmetrical side wing fixing components 5 are closely attached to the inner walls of both sides of the tank 1. The side wing fixing components 5 primarily cover the wingtips to ensure stable support. Each of the head fixing component 2, fuselage fixing component 3, propeller fixing component 4, and side wing fixing components 5 includes components that correspondingly attach to the upper and lower surfaces of the drone. The upper pressure unit slot and lower support unit slot on the lower surface are divided into upper pressure unit slot and lower support unit slot for easy packaging and placement. The upper pressure unit slot and lower support unit slot can also be connected by bolts or strapping. A rear support block 6 is provided between the spiral fixing component 4 and each side wing fixing component 5. The rear support block 6 contacts the rear wall of the box slot 1 and the corresponding fuselage of the UAV. The rear support block 6 can prevent the UAV from moving forward and backward, protect the most important nose and tail propellers, and at the same time, it has a stabilizing effect on the large wing body. Specifically, the nose fixing component 2, fuselage fixing component 3, spiral fixing component 4, side wing fixing component 5 and rear support block 6 can all be made of EVA foam material, which has a cushioning effect and prevents damage to the UAV.

[0023] As needed, limiting columns 7 are erected and fixed at the bottom of the inner groove of the box groove 1 at the positions corresponding to the head fixing component 2, fuselage fixing component 3, spiral fixing component 4, and rear support block 6 on both sides, as well as at the positions corresponding to the front and rear of the side wing fixing component 5. The limiting columns 7 are used for positioning, which facilitates the installation of each fixing component and provides limiting support. In addition, two side support columns 8 are symmetrically fixed on both sides of the front end of the inner groove bottom of the box groove 1, and two central support columns 9 are symmetrically fixed in the middle of the front end of the inner groove bottom of the box groove 1. The central support columns 9 are limited by the corresponding sides of the fuselage fixing component 3. The columns 7 are fixedly connected by cross bracing rods 10. Since the packaging box provides less support to the corresponding drone head, the structural strength of the front of the packaging box can be increased by setting side support columns 8, central support columns 9 and cross bracing rods 10 to prevent the product from being squeezed. In addition, a nozzle fixing assembly 11 is provided at the front end of the bottom of the box trough 1. The nozzle fixing assembly 11 is mainly used to fix scattered parts that are not directly installed. The two ends of the nozzle fixing assembly 11 are respectively in contact with the central support column 9 and the side support column, and the central support column 9 and the side support column are used for limiting.

[0024] When using a vehicle-mounted drone packaging box, you need to first open the box and place the lower support unit slots of the head fixing component 2, body fixing component 3, spiral fixing component 4 and side wing fixing component 5 into place. Then, close the upper support unit slot, and then put in the rear support block 6. Finally, close the box to complete the packaging, which is very convenient.

[0025] The parts of this utility model not described in detail are prior art. It is obvious to those skilled in the art that this utility model is not limited to the details of the above exemplary embodiments, and that this utility model can be implemented in other specific forms without departing from the spirit or basic characteristics of this utility model. Therefore, the above embodiments should be regarded as exemplary and non-limiting in all respects. The scope of this utility model is defined by the appended claims rather than the foregoing description. Therefore, it is intended to include all changes that fall within the meaning and scope of the equivalents of the claims in this utility model, and no reference numerals in the claims should be regarded as limiting the content of the claims.

Claims

1. A vehicle-mounted unmanned aerial vehicle (UAV) packaging box, characterized in that: The device includes a box slot and a box cover. From front to back, a head fixing component, a fuselage fixing component, and a spiral fixing component are sequentially arranged in the center of the box slot. The head fixing component and the spiral fixing component respectively contact the front and rear walls of the box slot. Two symmetrical side wing fixing components are closely attached to the inner walls on both sides of the box slot. Each of the head fixing component, fuselage fixing component, spiral fixing component, and side wing fixing component includes an upper pressure unit slot and a lower support unit slot that respectively attach to the corresponding upper and lower surfaces of the drone. A rear support block is provided between the spiral fixing component and each side wing fixing component. The rear support block respectively contacts the rear wall of the box slot and the corresponding rear fuselage of the drone.

2. The vehicle-mounted transport drone packaging box according to claim 1, characterized in that: Fixed limit columns are erected at the bottom of the slots corresponding to the head fixing component, fuselage fixing component, spiral fixing component and the two sides of the rear support block, as well as the front and rear positions of the side wing fixing component.

3. The vehicle-mounted transport drone packaging box according to claim 2, characterized in that: Two side support columns are symmetrically fixed on both sides of the front end of the bottom of the box groove, and two central support columns are symmetrically fixed in the middle of the front end of the bottom of the box groove. The central support columns are fixedly connected to the limiting columns on the corresponding side of the body fixing assembly by cross bracing.

4. The vehicle-mounted transport drone packaging box according to claim 3, characterized in that: The front end of the bottom of the tank is provided with a nozzle fixing assembly, and the two ends of the nozzle fixing assembly are respectively in contact with the central support column and the side support column.

5. The vehicle-mounted transport drone packaging box according to claim 1, characterized in that: The head fixing component, fuselage fixing component, spiral fixing component, side wing fixing component, and rear support block are all made of foam material.

6. The vehicle-mounted transport drone packaging box according to claim 1, characterized in that: The rear side of the box cover is hinged to the top of the rear wall of the box groove, and the front side of the box cover is detachably connected to the top of the front wall of the box groove via a buckle.

7. The vehicle-mounted transport drone packaging box according to claim 1, characterized in that: The outer surfaces of both the box groove and the box cover are fixed with multiple spaced reinforcing strips.