A container type electric unmanned aerial vehicle packaging and transporting structure

Abstract

The utility model discloses a container type electric unmanned plane packaging and transportation structure, two floor fixed guide rails are arranged in the container and are parallel to each other, and the front end of each floor fixed guide rail is hingedly connected with loading and unloading guide rails, the loading and unloading guide rails are located in the container when folding and are located outside the container when opening, two unmanned plane trolley lock catches are arranged on the two sides of each floor fixed guide rail, and each unmanned plane trolley lock catch is used for positioning the unmanned plane trolley, two stop blocks are arranged on each floor fixed guide rail, the two stop blocks on the same floor fixed guide rail limit the unmanned plane trolley by cooperation, and each stop block is detachably connected with each floor fixed guide rail. The utility model has the advantages of simple operation steps, improved stability of the unmanned plane in transportation, avoided structure damage or electronic component failure caused by the collision between the fuselage and the inner wall of the container, solved the problem of no special placing structure for the airfoil components in traditional transportation, and avoided the problem of easy damage caused by mutual friction or collision.

Description

Technical Field

[0001] This utility model relates to the field of packaging and transportation, and more specifically, to a container-type electric drone packaging and transportation structure. Background Technology

[0002] In modern logistics, security monitoring, medical rescue and other fields, the LEU100 compound wing medium-sized UAV is widely used for key tasks such as forest protection, cargo transportation, logistics transfer, maritime monitoring, medical drug and organ transportation due to its multi-functionality.

[0003] This type of UAV mainly consists of a fuselage section (including the central wing and power arm), a vertical tail section, and outer wing sections. It uses a leaf spring laminated plate landing gear. While this landing gear provides good ground support, it also has significant drawbacks: Firstly, the UAV's unique structure and the difficulty in moving the landing gear, coupled with the lack of dedicated loading and unloading aids, make it susceptible to damage to the fuselage or components during transport due to improper handling. Secondly, the height difference between the transport vehicle and the ground further increases loading and unloading difficulty and reduces transport preparation efficiency. Thirdly, in existing transport solutions, the UAV and its components cannot be positioned within the transport vehicle, hindering their movement... During transportation, the drone may experience lateral and longitudinal swaying due to factors such as road bumps and vehicle start-stop cycles, and may even collide with the inner wall of the transport carrier, leading to deformation of the drone fuselage, malfunction of electronic components, or damage to vulnerable parts such as the outer wings and tail. In addition, the drone's various disassembled components (such as the outer wings and tail) lack dedicated placement structures, making them susceptible to damage from impacts and vibrations during transportation. Furthermore, existing transport structures are mostly designed for specific drone models or sizes, making it difficult to flexibly adapt to the structural characteristics of the LEU100 compound wing medium-sized drone, and also difficult to accommodate the needs of different transportation scenarios, such as the different requirements for fixing strength in road and rail transport.

[0004] Therefore, those skilled in the art are dedicated to providing a containerized electric drone packaging and transportation structure that can effectively solve the above-mentioned technical problems. Utility Model Content

[0005] To achieve the above objectives, this utility model provides a container-type packaging and transportation structure for electric unmanned aerial vehicles, including a container with container doors at both ends;

[0006] Two floor-fixed guide rails are arranged parallel to each other inside the container. Each floor-fixed guide rail is hinged to a loading and unloading guide rail at its front end. When the loading and unloading guide rail is folded, it is located inside the container and when it is unfolded, it is located outside the container. Together with the floor-fixed guide rails, they form a track for the drone vehicle to pass through.

[0007] Each of the floor fixing rails is provided with two drone car latches on both sides, and each drone car latch is used to position the drone car.

[0008] Each of the floor fixing rails is provided with two blocks. The two blocks on the same floor fixing rail cooperate to limit the movement of the drone vehicle. Each block is detachably connected to each floor fixing rail.

[0009] The drone trolley enters the container via the loading and unloading guide rail and is positioned on the floor fixed guide rail. It is also positioned by the drone trolley latch and the stop block. The drone trolley is used to load drones.

[0010] Furthermore, the container includes a body and a frame;

[0011] The container body includes a bottom plate mounted on the frame, and two side panels connected to the frame are provided on both sides of the bottom plate. The top ends of the two side panels are connected by a top plate, which is supported by the frame. The container doors are located on the left and right sides of each side panel. Foam layers are provided on the inner sides of the side panels, top plates, and container doors.

[0012] Furthermore, three support bars are provided at the lower end of the base plate, and each support bar is evenly distributed along the length of the container.

[0013] Furthermore, the drone vehicle latch includes a positioning part, the upper half of which is connected to the upper end of the arc part, and an opening is formed between the lower end of the arc part and the lower end of the positioning part. The inner sides of the positioning part and the arc part are arc-shaped, and the positioning part and the arc part are integrally formed.

[0014] The drone trolley locks located on both sides of the floor fixed guide rail are connected by pull ropes, which are wound around the drone trolley and tighten the drone trolley.

[0015] Furthermore, the stop block includes a fixed section, the fixed section is provided with a plurality of first positioning holes, the upper end of the fixed section is provided with an extension section, the lower end of the extension section has protrusions on both sides, the fixed section and the extension section are integrally formed, and the outer side is inclined and the inner side is arc-shaped, and an arc-shaped rubber pad is provided at the arc-shaped surface.

[0016] The floor fixing guide rail is provided with a second positioning hole, and the positioning pin passes through both the first positioning hole and the second positioning hole to detachably position the stop block on the floor fixing guide rail; the fixing section is located inside the floor fixing guide rail, and the two side protrusions of the extension section are attached to the upper end of the floor fixing guide rail;

[0017] One end of the loading and unloading guide rail is hinged to the floor fixing guide rail, and the other end can be fixed to the floor fixing guide rail by inserting a pin through the third positioning hole.

[0018] Furthermore, each of the loading and unloading guide rails is provided with a first floor latch and a second floor latch with the same structure on both sides;

[0019] The first floor latch includes a positioning piece connected to the container. The positioning piece is detachably connected by screws. The positioning piece is provided with a positioning platform, and a pull ring is hung on the positioning platform.

[0020] Each of the first floor latches is connected by a first locking rope, and each of the second floor latches is connected by a second locking rope. Both the first and second locking ropes are wrapped around the middle of the drone's fuselage and the root of its wings to position the drone.

[0021] Furthermore, the container is equipped with:

[0022] The outer wing transfer box, which is detachably connected to the container, is used to mount the two outer wings of the drone;

[0023] The vertical tail transfer container, which is detached and connected to the container, is used to install the tail fin of the drone.

[0024] Furthermore, the inner walls of both the outer wing transfer box and the vertical tail transfer box are lined with foam cotton.

[0025] The length of the floor fixing rail is equal to the length of the container, and both ends are flush with the two ends of the container.

[0026] Furthermore, the drone vehicle includes a frame;

[0027] The vehicle frame has two brake wheels at the front bottom and two travel wheels at the rear bottom; landing gear locks are installed at the four corners of the upper part of the vehicle frame.

[0028] Furthermore, the landing gear lock includes a mounting plate disposed on the vehicle frame, the rear end of the lock body is hinged to the mounting plate, the lower end of the lock body has a limiting port for fixing the leaf spring landing gear of the UAV, the front end of the lock body is provided with a locking fastener, and the vehicle frame is provided with a locking assembly that cooperates with the locking fastener.

[0029] This utility model has the following beneficial effects:

[0030] 1. The loading and unloading guide rail, which is hinged at the front end of the floor fixed guide rail inside the container, can be fastened to the floor fixed guide rail when folded, without occupying extra space and can close the container door smoothly; when opened, it can be tilted and extended outside the container to form a continuous track with the floor fixed guide rail. This utility model can effectively solve the height difference between the container and the ground through this design, and without the need for external lifting equipment, the drone trolley carrying the drone can be smoothly moved into the container by manual pushing.

[0031] 2. The landing gear locks at the four corners of the drone vehicle adopt a hinged lock body design. After opening the lock body, place the drone leaf spring landing gear on the mounting plate. Close the lock body to complete the initial positioning through the limit port. Then, lock it in place by cooperating with the locking assembly and locking fastener. The operation steps are simple and efficient, avoiding delays in transportation preparation caused by complicated fixing process.

[0032] 3. In this utility model, the drone trolley locks on both sides of the floor-fixed guide rail are secured by a pull rope wrapped around the trolley and tightened, which can restrict the trolley's swaying laterally; the detachable blocks on the guide rail cooperate with the guide rail through the fixed section, the extension section protrusion fits against the upper end of the guide rail, and the inner arc-shaped rubber pad can buffer the collision. Two blocks as a group can limit the trolley's front and rear movement longitudinally, providing double fixation in both the lateral and longitudinal directions. Through the above settings, this utility model further improves the stability of the drone during transportation.

[0033] 4. The first floor lock and the second floor lock on both sides of the loading and unloading guide rail are respectively wrapped around the drone body and connected and fixed by the first locking rope and the second locking rope. They are used in conjunction with the fixed structure of the drone trolley to further reduce the shaking amplitude of the drone body caused by vibration and avoid structural damage or electronic component failure caused by collision between the drone body and the inner wall of the container.

[0034] 5. The outer wing transfer box and vertical tail transfer box set inside the container are adapted to the shape and size of the drone's outer wing and tail respectively. The foam cotton on the inner wall of the box can form a flexible buffer layer to absorb the impact and vibration during transportation, solving the problem that the wing parts in traditional transportation do not have a dedicated placement structure and are easily damaged by mutual friction or collision.

[0035] 6. Three support bars are evenly installed at the bottom of the container, which not only provide ground support, but also facilitate forklift insertion during container transfer. Attached Figure Description

[0036] Figure 1 This is a structural schematic diagram of a specific embodiment of the present invention.

[0037] Figure 2 This is a three-dimensional structural diagram of the present invention without a container door.

[0038] Figure 3This is a schematic diagram of the structure of the container in this utility model without wall panels and a top panel.

[0039] Figure 4 yes Figure 3 Another three-dimensional structural diagram.

[0040] Figure 5 yes Figure 4 A magnified schematic diagram of the structure at point A in the middle.

[0041] Figure 6 This is a 3D structural diagram of the drone mounted on a drone vehicle.

[0042] Figure 7 This is a 3D structural diagram of the drone vehicle.

[0043] Figure 8 This is a schematic diagram of a drone vehicle set inside a frame, with one of the loading and unloading rails located outside the container when opened.

[0044] Figure 9 yes Figure 8 A magnified schematic diagram of the structure at point B in the middle.

[0045] Figure 10 yes Figure 8 A magnified schematic diagram of the structure at point C.

[0046] Figure 11 yes Figure 8 A magnified schematic diagram of the structure at point D.

[0047] Figure 12 This is a three-dimensional structural diagram of the stop block in this utility model.

[0048] Figure 13 This is a schematic diagram of the structure of the drone trolley lock in this utility model.

[0049] Figure 14 This is a schematic diagram of the structure of the drone mounted on the base plate via a drone trolley.

[0050] Figure 15 This is a three-dimensional structural diagram of the first floor lock in this utility model.

[0051] Figure 16 This is a schematic diagram of the structure where the loading and unloading guide rail is fastened to the floor fixed guide rail.

[0052] The attached diagram lists the components represented by each number as follows:

[0053] 1. Container; 2. Container door; 3. Floor fixing rail; 5. Loading and unloading rail; 6. Drone trolley; 7. Drone; 8. Drone trolley lock; 8a. Positioning part; 8b. Arc part; 8c. Opening; 9. Stop block; 9a. Fixing section; 9b. First positioning hole; 9c. Extension section; 9d. Boss; 9e. Inclined surface; 10. Frame; 11. Base plate; 12. Wall panel; 13. Top plate; 15. Support bar; 19. Pull rope; 20. Arc-shaped rubber pad; 21. The... 22. Second positioning hole; 23. Third positioning hole; 24. First floor latch; 25. Positioning plate; 26. Positioning platform; 27. Pull ring; 28. Second floor latch; 39. First locking rope; 30. Second locking rope; 51. Outer wing transfer box; 52. Tail transfer box; 53. Frame; 54. Brake wheel; 55. Running wheel; 56. Landing gear lock; 57. Mounting plate; 58. Lock body; 59. Leaf spring landing gear; 60. Limiting port; 61. Latch fixing component; 62. Latch assembly. Detailed Implementation

[0054] The present invention will be further described below with reference to the accompanying drawings and embodiments:

[0055] In the description of this utility model, it should be noted that the terms "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are used only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0056] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "setting," and "connection" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0057] like Figures 1 to 16 As shown, a container-type electric drone packaging and transportation structure includes a container 1, with container doors 2 at both ends of the container 1; the container doors 2 in this utility model are double-opening, which facilitates the pushing and pushing of drones in and out, as well as the entry and exit of personnel and other equipment and facilities.

[0058] The container 1 in this utility model has dimensions of 4.5 meters × 2.5 meters × 2 meters. It is entirely made of steel structure and uses Q235 hot-rolled plate with a thickness of 2 mm. The entire container can withstand an internal load of 1 ton.

[0059] The container 1 has two parallel floor fixing rails 3, and each floor fixing rail 3 has a loading and unloading rail 5 hinged to its front end. In this utility model, both the floor fixing rail 3 and the loading and unloading rail 5 are made of Q235 steel.

[0060] In this utility model Figures 2 to 4 and Figure 8 In the figure, the loading and unloading guide rail 5 has two working states, which correspond to different stages of the transportation process: the first is the open state, in which the loading and unloading guide rail 5 rotates outward and extends to the outside of the container 1; the second is the folded state, in which the loading and unloading guide rail 5 is folded inward and fits into the inside of the container 1. It should be noted that the split display of the two states in the attached figure is only to present the structural form and movement logic of the loading and unloading guide rail 5 more intuitively, and does not represent the actual operation scenario.

[0061] In real-world applications, operations must strictly adhere to functional requirements for state switching: when loading or unloading a drone into container 1 (loading operation) or removing it from container 1 (unloading operation), both loading / unloading guide rails 5 must be simultaneously adjusted to the open state, forming a continuous and stable passageway together with the floor-fixed guide rails 3 inside container 1, ensuring smooth entry and exit of the drone trolley 6 carrying the drone; when loading / unloading operations are completed and the transportation phase begins, both loading / unloading guide rails 5 must be simultaneously folded into container 1 and secured with the floor-fixed guide rails 3 using pins, preventing guide rail swaying during transportation and ensuring that container door 2 can close normally, meeting the requirements for sealed transportation.

[0062] When folded, the loading and unloading guide rail 5 is located inside the container 1; when opened, it is located outside the container 1, forming a track for the drone trolley 6 to pass through together with the floor-fixed guide rail 3. When folded, each of the loading and unloading guide rails 5 is fastened to the floor-fixed guide rail 3 and located inside the container 1. This is the transport state. After folding, the container door 2 can be closed smoothly. At the same time, since the loading and unloading guide rail 5 is fastened to the floor-fixed guide rail 3 after folding, it effectively avoids the loading and unloading guide rail 5 shaking inside the container 1 during transport, thus improving stability. When opened, the loading and unloading guide rail 5 is tilted and set in the container 1, forming a track for the drone trolley 6 to pass through together with the floor-fixed guide rail 3. Since there is a height difference between the container 1 and the ground, this setting facilitates the movement of the drone trolley 6 carrying the drone 7 (LEU100 compound wing medium-sized drone) into the container 1.

[0063] Two drone car latches 8 are provided on both sides of each floor fixing guide rail 3. Each drone car latch 8 is used to position the drone car 6. The guide rail 3 can not only guide the drone car 6, but also limit it, so that the drone car 6 can only move along the length direction of the guide rail 3.

[0064] Each of the floor fixing rails 3 is provided with two blocks 9. The two blocks 9 located on the same floor fixing rail 3 cooperate with each other to limit the position of the drone vehicle 6. Each block 9 is detached and connected to each of the floor fixing rails 3.

[0065] The drone trolley 6 enters the container 1 via the loading and unloading guide rail 5 and is positioned on the floor fixing guide rail 3. It is also positioned by the drone trolley latch 8 and the stop block 9. The drone trolley 6 is used to load the drone 7.

[0066] The container 1 includes a container body and a frame 10;

[0067] The container body includes a bottom plate 11 mounted on the frame 10. Two side panels 12 connected to the frame 10 are provided on both sides of the bottom plate 11. The top ends of the two side panels 12 are connected by a top plate 13, which is supported by the frame 10. The container doors 2 are located on the left and right sides of each side panel 12. A foam layer is provided on the inner sides of the side panels 12, the top plate 13, and the container doors 2. Furthermore, the foam layer in this invention is high-density foam. By providing the foam layer, it is ensured that the container will not cause damage to the aircraft, components, or personnel during use.

[0068] Three support bars 15 are provided at the lower end of the base plate 11, and the support bars 15 are evenly distributed along the length of the container 1. In this utility model, each support bar 15 is made of reinforced channel steel.

[0069] The drone vehicle latch 8 includes a positioning part 8a, the upper half of which is connected to the upper end of the arc part 8b, and an opening 8c is formed between the lower end of the arc part 8b and the lower end of the positioning part 8a. The inner sides of the positioning part 8a and the arc part 8b are arc-shaped, and the positioning part 8a and the arc part 8b are integrally formed.

[0070] The drone trolley locks 8 located on both sides of the floor fixed guide rail 3 are connected by pull ropes 19, which are wound around the drone trolley 6 and tighten the drone trolley 6.

[0071] The stop block 9 includes a fixed section 9a, which has a plurality of first positioning holes 9b. The upper end of the fixed section 9a is provided with an extension section 9c. The lower end of the extension section 9c has protrusions 9d on both sides. The fixed section 9a and the extension section 9c are integrally formed, with the outer side being an inclined surface 9e and the inner side being an arc-shaped surface. An arc-shaped rubber pad 20 is provided at the arc-shaped surface.

[0072] The floor fixing guide rail 3 has a second positioning hole 21. The positioning pin passes through both the first positioning hole 9b and the second positioning hole 21 to detachably position the stop block 9 on the floor fixing guide rail 3. The fixing section 9a is located inside the floor fixing guide rail 3, and the two side protrusions 9d of the extension section 9c are attached to the upper end of the floor fixing guide rail 3.

[0073] One end of the loading / unloading guide rail 5 is hinged to the floor fixing guide rail 3, and the other end can be fixed to the floor fixing guide rail 3 by means of a pin passing through the third positioning hole 22. With this configuration, the stability is higher when the loading / unloading guide rail 5 is located inside the container 1 and fastened to the floor fixing guide rail 3.

[0074] Each of the loading and unloading guide rails 5 is provided with a first floor latch 23 and a second floor latch 29 with the same structure on both sides;

[0075] The first floor latch 23 includes a positioning piece 26 connected to the container 1. The positioning piece 26 is connected and detached by screws. The positioning piece 26 is provided with a positioning platform 27, and a pull ring 28 is hung on the positioning platform 27.

[0076] Each of the first floor latches 23 is connected by a first locking rope 30, and each of the second floor latches 29 is connected by a second locking rope 31. The first locking rope 30 and the second locking rope 31 are both wrapped around the middle of the fuselage and the root of the wing of the drone 7 to position the drone 7. This setting can effectively ensure that the positioning force of the drone 7 is uniform and avoid excessive local force that could cause deformation of the fuselage.

[0077] The container 1 contains: an outer wing transfer box 50, detachably connected to the container 1, for mounting the two outer wings of the drone 7; and a tail transfer box 51, detachably connected to the container 1, for mounting the tail fin of the drone 7. The inner walls of both the outer wing transfer box 50 and the tail transfer box 51 are lined with conformal foam; this facilitates the insertion and removal of drone components while protecting the entire component. During transportation, the outer wing transfer box 50 and the tail transfer box 51 are fixed to the container to prevent slippage and damage to the components.

[0078] The length of the floor fixing rail 3 is equal to the length of the container 1, and both ends are flush with the two ends of the container 1.

[0079] The drone vehicle 6 includes a frame 52;

[0080] The frame 52 has two brake wheels 53 at the bottom front end and two travel wheels 55 at the bottom rear end; landing gear locks 56 are provided at the four corners of the upper end of the frame 52.

[0081] The landing gear lock 56 includes a mounting plate 57 disposed on the frame 52. The rear end of the lock body 58 is hinged to the mounting plate 57. The lower end of the lock body 58 has a limiting port 60 for fixing the leaf spring landing gear 59 of the UAV 7. The front end of the lock body 58 is provided with a locking fastener 61. The frame 52 is provided with a locking assembly 62 that cooperates with the locking fastener 61.

[0082] The optimal method of using this utility model is as follows:

[0083] Open the container doors 2 at both ends of container 1, release the loading / unloading guide rail 5 from the floor fixing guide rail 3, and rotate the loading / unloading guide rail 5 around the hinge point to an inclined state, so that the loading / unloading guide rail 5 is located outside the container 1, forming a continuous passage track for the drone vehicle 6 (see [reference]). Figure 8 , Figure 8 One of the loading and unloading rails 5 is already in the open state. When both loading and unloading rails 5 are in the open state, the drone can be moved into the container through the loading and unloading rails 5. Confirm that the stop 9 has been removed from the floor fixed rail 3 (if the stop has been installed on the floor fixed rail in advance) to avoid obstructing the drone trolley 6 from entering.

[0084] The locking body 58 is rotated around the mounting plate 57 to open it. Then, the four leaf spring landing gears 59 of the drone 7 are placed on the respective mounting plates 57, and the locking body 58 is closed. At this point, each leaf spring landing gear 59 is precisely positioned at its respective limit port 60 and is positioned using the locking body 58. The locking assembly 62 then engages with the locking fastener 61 to lock the locking body 58, thus completing the fixation of the drone 7 on the drone vehicle 6 (see...). Figure 6 Place the two outer wings of the UAV 7 into the outer wing transfer box 50 and the tail fin into the vertical tail transfer box 51.

[0085] The drone trolley 6 carrying the drone 7 is pushed into the container 1 along the loading and unloading guide rail 5. Then, each stop 9 is fixed to the floor fixing guide rail 3, so that the drone trolley 6 is positioned between the stops 9 and limited by the stops 9. The specific method of fixing the stops 9 is as follows: the fixing section 9a is placed into the floor fixing guide rail 3, so that the protrusions 9d on both sides of the extension section 9c are attached to the upper end of the floor fixing guide rail 3. The first positioning hole 9b is aligned with the second positioning hole 21 on the floor fixing guide rail 3, and the positioning pin is inserted to complete the fixation. Thus, the drone trolley 6 is limited in front and back by the cooperation of the stops 9. As a further preferred option, the two stops 9 in the front half can be positioned first, and the drone trolley 6 can move along the floor fixing guide rail 3 until it is limited by the two stops 9. Then, the two stops 9 in the rear half are fixed.

[0086] The pull rope 19 is wound around the drone trolley 6, and the two ends of the pull rope 19 are connected to the locking buckles 8 of each drone trolley. The pull rope 19 is then tightened to fix the drone trolley 6. The first locking rope 30 is then wrapped around the drone 7 and the two ends are connected to the first floor locking buckle 23. The second locking rope 31 is then wrapped around the drone 7 and connected to the second floor locking buckle 29 to further enhance the stability of the drone 7 installed in the container 1.

[0087] Rotate the loading / unloading guide rail 5 around the hinge point until it engages with the floor-fixed guide rail 3, ensuring that the loading / unloading guide rail 5 is completely inside the container 1. Then, insert a pin into the third positioning hole 22 to fix the loading / unloading guide rail 5 to the floor-fixed guide rail 3. This further improves stability. Then, close the container door 2 to complete the transport status switch.

[0088] Upon arrival at the destination, open container door 2 and reverse the steps described above. First, loosen the first locking rope 30 and the second locking rope 31, remove the stop block 9 from the floor fixed guide rail 3, and then remove the pull rope 19. Open the loading and unloading guide rail 5, and then push the drone trolley 6 to move on the floor fixed guide rail 3. Move container 1 out through the loading and unloading guide rail 5, take out the drone components from the outer wing transfer box 50 and the vertical tail transfer box 51, and finally release the landing gear lock 56. Take off the drone 7 and assemble the outer wing and tail. Retract the loading and unloading guide rail 5 and fasten it to the floor fixed guide rail 3. Close container door 2 to complete the entire unloading process.

[0089] The preferred embodiments of this utility model have been described in detail above. It should be understood that those skilled in the art can make numerous modifications and variations based on the concept of this utility model without creative effort. Therefore, all technical solutions that can be obtained by those skilled in the art based on the concept of this utility model through logical analysis, reasoning, or limited experimentation on the basis of existing technology should be within the scope of protection defined by the claims.

Claims

1. A container-type electric drone packaging and transportation structure, characterized in that: Includes a container (1), and both ends of the container (1) are provided with container doors (2); Two floor-fixed guide rails (3) are arranged parallel to each other inside the container (1). Each floor-fixed guide rail (3) is hinged to a loading and unloading guide rail (5) at its front end. When the loading and unloading guide rail (5) is folded, it is located inside the container (1) and when it is opened, it is located outside the container (1). Together with the floor-fixed guide rails (3), they form a track for the unmanned aerial vehicle (6) to pass through. Two drone car latches (8) are provided on both sides of each floor fixing guide rail (3), and each drone car latch (8) is used to position the drone car (6); two blocks (9) are provided on each floor fixing guide rail (3), and the two blocks (9) located on the same floor fixing guide rail (3) cooperate with each other to limit the drone car (6), and each block (9) is detached from each floor fixing guide rail (3); The drone trolley (6) enters the container (1) via the loading and unloading guide rail (5) and is positioned on the floor fixed guide rail (3). It is also positioned by the drone trolley latch (8) and the stop block (9). The drone trolley (6) is used to load the drone (7).

2. The containerized electric drone packaging and transportation structure as described in claim 1, characterized in that: The container (1) includes a container body and a frame (10); The container body includes a bottom plate (11) set on the frame (10), and two side panels (12) connected to the frame (10) are provided on both sides of the bottom plate (11). The top ends of the two side panels (12) are connected by a top plate (13), which is supported by the frame (10). The container door (2) is located on the left and right sides of each side panel (12). The inner sides of the side panels (12), the top plate (13) and the container door (2) are all provided with a foam layer.

3. The container-type electric drone packaging and transportation structure as described in claim 2, characterized in that: The bottom of the base plate (11) is provided with three support bars (15), and each support bar (15) is evenly distributed along the length of the container (1).

4. The container-type electric drone packaging and transportation structure as described in claim 1, characterized in that: The drone vehicle latch (8) includes a positioning part (8a), the upper half of which is connected to the upper end of the arc part (8b), and an opening (8c) is formed between the lower end of the arc part (8b) and the lower end of the positioning part (8a). The inner sides of the positioning part (8a) and the arc part (8b) are arc-shaped, and the positioning part (8a) and the arc part (8b) are integrally formed. The drone trolley latches (8) located on both sides of the floor fixed guide rail (3) are connected by pull ropes (19), which are wound around the drone trolley (6) and tighten the drone trolley (6).

5. The container-type electric drone packaging and transportation structure as described in claim 4, characterized in that: The stop block (9) includes a fixed section (9a), which has a plurality of first positioning holes (9b). The upper end of the fixed section (9a) is provided with an extension section (9c). The lower end of the extension section (9c) has protrusions (9d) on both sides. The fixed section (9a) and the extension section (9c) are integrally formed, with the outer side being an inclined surface (9e) and the inner side being an arc-shaped surface. An arc-shaped rubber pad (20) is provided at the arc-shaped surface. The floor fixing guide rail (3) is provided with a second positioning hole (21). The positioning pin passes through both the first positioning hole (9b) and the second positioning hole (21) to detachably position the stop block (9) on the floor fixing guide rail (3). The fixing section (9a) is located inside the floor fixing guide rail (3), and the two side bosses (9d) of the extension section (9c) are attached to the upper end of the floor fixing guide rail (3). One end of the loading and unloading guide rail (5) is hinged to the floor fixing guide rail (3), and the other end can be fixed on the floor fixing guide rail (3) by inserting a pin through the third positioning hole (22).

6. The containerized electric drone packaging and transportation structure as described in claim 5, characterized in that: Each of the loading and unloading guide rails (5) is provided with a first floor latch (23) and a second floor latch (29) with the same structure on both sides; The first floor latch (23) includes a positioning piece (26) connected to the container (1), the positioning piece (26) being detached and connected by screws, the positioning piece (26) being provided with a positioning platform (27), and the positioning platform (27) being provided with a pull ring (28); Each of the first floor latches (23) is connected by a first locking rope (30), and each of the second floor latches (29) is connected by a second locking rope (31). The first locking rope (30) and the second locking rope (31) are both wrapped around the middle of the fuselage and the root of the wing of the UAV (7) to position the UAV (7).

7. The containerized electric drone packaging and transportation structure as described in claim 6, characterized in that: The container (1) is equipped with: The outer wing transfer box (50) is detachably connected to the container (1) and is used to install the two outer wings of the drone (7); The vertical tail transfer container (51) is detachably connected to the container (1) and is used to install the tail fin of the drone (7).

8. The containerized electric drone packaging and transportation structure as described in claim 7, characterized in that: The inner walls of the outer wing transfer box (50) and the vertical tail transfer box (51) are both provided with foam cotton; The length of the floor fixing rail (3) is equal to the length of the container (1), and both ends are flush with the two ends of the container (1).

9. The containerized electric drone packaging and transportation structure as described in claim 8, characterized in that: The unmanned vehicle (6) includes a frame (52); The frame (52) has two brake wheels (53) at the bottom front end and two running wheels (55) at the bottom rear end; the frame (52) has landing gear locks (56) at the four corners of the upper end.

10. The containerized electric drone packaging and transportation structure as described in claim 9, characterized in that: The landing gear lock (56) includes a mounting plate (57) disposed on the frame (52), the rear end of the lock body (58) is hinged to the mounting plate (57), the lower end of the lock body (58) has a limiting port (60) for fixing the leaf spring landing gear (59) of the UAV (7), the front end of the lock body (58) is provided with a locking fastener (61), and the frame (52) is provided with a locking assembly (62) that cooperates with the locking fastener (61).

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