Transportation device for unmanned aerial vehicle idle running field

Abstract

The utility model provides a transportation device for an unmanned aerial vehicle idle running field, which relates to the technical field of unmanned aerial vehicle idle running field transportation and comprises a supporting structure, a first bracket structure and a second bracket structure which are sequentially arranged from bottom to top. A first accommodating space, a second accommodating space and a third accommodating space are respectively formed in the supporting structure, the first bracket structure and the second bracket structure; the first containing space, the second containing space and the third containing space can contain the fuselage, wings and empennages used for being installed on one side of the fuselage and wings and empennages used for being installed on the other side of the fuselage correspondingly. The problem of idling field transportation of wings and empennages of medium and large unmanned aerial vehicles in the prior art is solved.

Description

Technical Field

[0001] The utility model belongs to the technical field of transportation of unmanned aerial vehicle (UAV) air transport yards, and more specifically, relates to a transportation device for unmanned aerial vehicle (UAV) air transport yards. Background Art

[0002] Drone air transport devices are commonly used in drone transfer operations, facilitating drone transport, saving manpower, and improving the security of drone air transport. Currently, there is no commercially available transport device suitable for medium- to large-sized drone air transports. Existing transport devices occupy a large area, limiting the transfer capacity of air transports and failing to meet the air transport needs of medium- to large-sized drones, including fuselages, wings, and tails.

[0003] Therefore, there is an urgent need to design a transport device suitable for the air transport yard of medium and large UAVs to meet the storage and air transport yard requirements of wings, tails and even fuselages. Utility Model Content

[0004] The purpose of the utility model is to address the deficiencies in the prior art and provide a transportation device for unmanned aerial vehicle (UAV) air transport yards, thereby solving the problem of transporting wings and tail fins of medium and large UAVs to air transport yards in the prior art.

[0005] In order to achieve the above-mentioned purpose, the present invention provides a transport device for unmanned aerial vehicle (UAV) transport to an air transport yard, comprising:

[0006] A support structure, a first bracket structure and a second bracket structure are arranged in sequence from bottom to top, and a movable part is provided at the lower end of the support structure. The interior of the support structure, the interior of the first bracket structure and the interior of the second bracket structure respectively form a first accommodating space, a second accommodating space and a third accommodating space, and the first accommodating space, the second accommodating space and the third accommodating space can respectively accommodate a fuselage, wings and tail for installation on one side of the fuselage, and wings and tail for installation on the other side of the fuselage.

[0007] Optionally, the support structure includes multiple pairs of support legs, each pair of support legs includes two support legs, and the support legs are respectively arranged on both sides of the first bracket structure.

[0008] Optionally, two first reinforcing rods are cross-arranged between adjacent supporting legs on the same side.

[0009] Optionally, the first bracket structure includes a first rectangular frame connected above the supporting structure, a plurality of first vertical poles are spaced apart on both sides of the upper portion of the first rectangular frame, a first connecting rod is connected to the top of the plurality of first vertical poles on each side, a plurality of first cross beams are arranged inside the first rectangular frame, a first installation groove is formed on the upper side of the first cross beam, and the first installation groove is used to install a first buffer layer.

[0010] Optionally, the bottom surface of the first buffer layer is bonded to the bottom of the first mounting groove, and the top surface of the first buffer layer is provided with a first groove that matches the wing.

[0011] Optionally, a second buffer layer is further included, which is used to be arranged on the upper side of the wing. A first clipping groove is provided on the lower side of the second buffer layer, and the first clipping groove is clipped to the first buffer layer. The upper side of the second buffer layer is used to place the tail wing.

[0012] Optionally, the second bracket structure includes a second rectangular frame detachably connected to the top of the first bracket structure, a plurality of second vertical poles are arranged at intervals on both sides of the upper part of the second rectangular frame, a second connecting rod is connected to the top of the plurality of second vertical poles on each side, a plurality of second cross beams are arranged inside the second rectangular frame, a second installation groove is formed on the upper side of the second cross beam, and the second installation groove is used to install a third buffer layer.

[0013] Optionally, the bottom surface of the third buffer layer is bonded to the bottom of the second mounting groove, and the top surface of the third buffer layer is provided with a second groove that matches the wing.

[0014] Optionally, a fourth buffer layer is further included, which is used to be arranged on the upper side of the wing. A second snap-fitting groove is provided on the lower side of the fourth buffer layer, and the second snap-fitting groove is snap-fitted with the third buffer layer.

[0015] Optionally, a second reinforcing rod is detachably connected between each pair of support legs, a buckle is provided on the lower side of the first bracket structure, and the second reinforcing rod can be snap-connected with the buckle.

[0016] The utility model provides a transport device for an unmanned aerial vehicle (UAV) air transport yard, and its beneficial effects are as follows: the transport device for an unmanned aerial vehicle (UAV) air transport yard comprises a support structure, a first bracket structure, and a second bracket structure which are sequentially arranged from bottom to top; the support structure, the first bracket structure, and the second bracket structure can respectively accommodate a fuselage, wings and a tail for installation on one side of the fuselage, and wings and a tail for installation on the other side of the fuselage through their respective first accommodating spaces, second accommodating spaces, and third accommodating spaces. Under the premise of ensuring that the UAV occupies the minimum space during transportation, the transport of medium and large UAVs to an air transport yard is realized.

[0017] Other features and advantages of the present invention will be described in detail in the subsequent detailed description of the embodiments. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The above and other objects, features and advantages of the present invention will become more apparent through a more detailed description of exemplary embodiments of the present invention in conjunction with the accompanying drawings, wherein the same reference numerals generally represent the same components in the exemplary embodiments of the present invention.

[0019] Figure 1 A schematic diagram of the main structure of a transportation device for an unmanned aerial vehicle (UAV) air transport field according to an embodiment of the present invention is shown.

[0020] Figure 2 A schematic diagram of the exploded structure of a transport device for a drone air transport yard according to an embodiment of the present invention is shown.

[0021] Figure 3 A three-dimensional structural schematic diagram of a transportation device for a drone empty transport yard according to an embodiment of the present utility model is shown.

[0022] Description of reference numerals:

[0023] 1. Support structure; 2. First bracket structure; 3. Second bracket structure; 4. Moving part; 5. First reinforcing rod; 6. Second reinforcing rod; 7. First rectangular frame; 8. First vertical pole; 9. First connecting rod; 10. First crossbeam; 11. First buffer layer; 12. Second buffer layer; 13. Second rectangular frame; 14. Second vertical pole; 15. Second connecting rod; 16. Second crossbeam; 17. Third buffer layer; 18. Fourth buffer layer; 19. Fifth buffer layer; 20. Sixth buffer layer; 21. Buckle; 22. Locking part. DETAILED DESCRIPTION

[0024] The following describes preferred embodiments of the present invention in greater detail. Although preferred embodiments of the present invention are described below, it should be understood that the present invention can be implemented in various forms and should not be limited by the embodiments described herein. Rather, these embodiments are provided to make the present invention more thorough and complete, and to fully convey the scope of the present invention to those skilled in the art.

[0025] like Figures 1 to 3 As shown, the utility model provides a transport device for unmanned aerial vehicle (UAV) air transport field, comprising:

[0026] A support structure 1, a first bracket structure 2, and a second bracket structure 3 are arranged in sequence from bottom to top. A movable component 4 is provided at the lower end of the support structure 1. The interior of the support structure 1, the interior of the first bracket structure 2, and the interior of the second bracket structure 3 respectively form a first accommodating space, a second accommodating space, and a third accommodating space. The first accommodating space, the second accommodating space, and the third accommodating space can respectively accommodate a fuselage, wings and tail fins for installation on one side of the fuselage, and wings and tail fins for installation on the other side of the fuselage.

[0027] Specifically, in order to solve the problem of transporting wings and tails of medium and large UAVs to air transport airports in the prior art, the transportation device for UAVs to air transport airports provided by the utility model has a support structure 1, a first bracket structure 2 and a second bracket structure 3 arranged in sequence from bottom to top. The support structure 1, the first bracket structure 2 and the second bracket structure 3 can respectively accommodate the fuselage, the wings and tail for installation on one side of the fuselage and the wings and tail for installation on the other side of the fuselage through their respective first accommodating space, second accommodating space and third accommodating space. Under the premise of ensuring that the UAVs occupy the minimum space during transportation, the air transport airport transportation of medium and large UAVs is realized.

[0028] Optionally, the support structure 1 includes multiple pairs of support legs, each pair of support legs includes two support legs, and are respectively arranged on both sides of the first bracket structure 2.

[0029] Specifically, multiple supporting legs distributed on both sides of the first bracket structure 2 form a matrix arrangement to support the first bracket structure 2 and the second bracket structure 3, and a first accommodating space capable of accommodating the fuselage and fuselage transportation components is formed under the first bracket structure 2, which can coordinate with the transportation of the fuselage transportation components and the fuselage, and reduce the total footprint during the transportation of the fuselage, wings, and tail.

[0030] Optionally, two first reinforcing rods 5 are cross-arranged between adjacent supporting legs on the same side.

[0031] Specifically, adjacent supporting legs on each side of the first bracket structure 2 are connected by a first reinforcing rod 5 to enhance the supporting stability of the supporting structure 1. The cross-arrangement of the first reinforcing rods 5 can further improve the structural strength and stability of the supporting legs.

[0032] Optionally, a lockable universal wheel is provided at the lower end of each supporting leg.

[0033] In this embodiment, the locking universal wheel adopts a 10-inch universal wheel with a 4-directional limit slot lock; the support legs are made of high-strength alloy material to ensure extremely strong bearing capacity during the overhead transportation of the wings and tail; the surface of the universal wheel is wrapped with a layer of polyurethane material, which is quiet and passable during the movement; the 4-directional limit lock slots have a 90° limit function every time, and can also be switched to universal mode to meet the needs of directional movement and universal movement.

[0034] Optionally, the first bracket structure 2 includes a first rectangular frame 7 connected above the supporting structure 1, and a plurality of first vertical poles 8 are spaced apart on both sides of the upper portion of the first rectangular frame 7, and a first connecting rod 9 is connected to the top of the plurality of first vertical poles 8 on each side, and a plurality of first cross beams 10 are arranged inside the first rectangular frame 7, and a first installation groove is formed on the upper side of the first cross beam 10, and the first installation groove is used to install a first buffer layer 11.

[0035] Specifically, the first bracket structure 2 is formed by welding a 3mm thick profile tube and is welded to a plurality of supporting legs. On the basis of meeting the structural strength, the frame structure is simplified to meet the lightweight requirements; the first rectangular frame 7 and the first crossbeam 10 inside it form the supporting component of the first bracket structure 2, and the first buffer layer 11 is used to contact the wing to avoid scratches or bumps on the wing. The plurality of first vertical poles 8 and the first connecting rods 9 connected to their upper ends form the enclosure component of the first bracket structure 2, and a second accommodating space is formed inside the enclosure component and on the upper side of the supporting component.

[0036] In this embodiment, the cross section of the first crossbeam 10 is a U-shape with an upward opening, and is formed by bending a 5 mm steel plate.

[0037] Optionally, the bottom surface of the first buffer layer 11 is bonded to the bottom of the first mounting groove, and the top surface of the first buffer layer 11 is provided with a first groove that matches the wing.

[0038] Specifically, the first buffer layer 11 is strip-shaped, with its bottom surface bonded to the bottom of the first mounting groove, and a first groove provided on its top surface for accommodating at least part of the wing to improve the stability of the wing during transportation.

[0039] Optionally, a second buffer layer 12 is further included, which is used to be arranged on the upper side of the wing. A first snap-in groove is provided on the lower side of the second buffer layer 12, which is snap-fitted to the first buffer layer 11. The upper side of the second buffer layer 12 is used to place the tail wing.

[0040] Specifically, the second buffer layer 12 is strip-shaped. After the wing is placed, the second buffer layer 12 is placed on the upper side of the wing. Extensions are provided on the lower side of both ends of the second buffer layer 12. The extensions extend downward and a first snap-fit ​​groove is provided at the bottom. Part of the first buffer layer 11 is snapped into the first snap-fit ​​groove to achieve the snap-fit ​​between the first snap-fit ​​groove and the first buffer layer 11. The tail is placed on the upper side of the second buffer layer 12. The second buffer layer 12 can separate the wing and the tail to avoid collision between the two.

[0041] Optionally, the second bracket structure 3 includes a second rectangular frame 13 detachably connected to the top of the first bracket structure 2, and a plurality of second vertical poles 14 are spaced apart on both sides of the upper part of the second rectangular frame 13, and a second connecting rod 15 is connected to the top of the plurality of second vertical poles 14 on each side, and a plurality of second cross beams 16 are arranged inside the second rectangular frame 13, and a second installation groove is formed on the upper side of the second cross beam 16, and the second installation groove is used to install a third buffer layer 17.

[0042] Specifically, the second bracket structure 3 has the same specific structure as the first bracket structure 2 , and the second bracket structure 3 can be locked and connected to the first bracket structure 2 via a locking component 22 , so as to facilitate disassembly and assembly between the two.

[0043] In this embodiment, locking components 22 are installed on the first upright poles 8 at both ends of the first bracket structure 2 and the second upright poles 14 at both ends of the second bracket structure 3. The locking components 22 can be hook-type buckles.

[0044] In this embodiment, a lifting structure is provided on the top of the second bracket structure 3, and the lifting structure is used to cooperate with the hook of the crane during lifting.

[0045] Optionally, the bottom surface of the third buffer layer 17 is bonded to the bottom of the second mounting groove, and the top surface of the third buffer layer 17 is provided with a second groove that matches the wing.

[0046] Optionally, a fourth buffer layer 18 is further included. The fourth buffer layer 18 is used to be arranged on the upper side of the wing. A second snap-fitting groove is provided on the lower side of the fourth buffer layer 18 , and the second snap-fitting groove is snap-fitted with the third buffer layer 17 .

[0047] In this embodiment, a plate-shaped fifth buffer layer 19 and a sixth buffer layer 20 are also included. The fifth buffer layer 19 and the sixth buffer layer 20 are respectively used to be placed on the upper side of the tail wing in the first bracket structure 2 and the upper side of the tail wing in the second bracket structure 3, so as to protect the tail wing and the wing, and the wing and the tail wing will wrap the fifth buffer layer 19 during the process of strip tightening. The material of the first buffer layer 11, the second buffer layer 12, the third buffer layer 17, the fourth buffer layer 18, the fifth buffer layer 19 and the sixth buffer layer 20 is foam.

[0048] Optionally, a second reinforcing rod 6 is detachably connected between each pair of supporting legs, and a buckle 21 is provided on the lower side of the first bracket structure 2 , and the second reinforcing rod 6 can be snap-connected with the buckle 21 .

[0049] Specifically, the two ends of the second reinforcing rod 6 can be detachably connected to the supporting legs through a pin structure, that is, the second reinforcing rod 6 is a tubular structure, which passes through the supporting legs and is inserted into the second reinforcing rod 6 through a big-headed pin with a hole, and then the cotter pin passes through the second reinforcing rod 6 and the big-headed pin with a hole; in this way, when the empty transport yard is being transported, the second reinforcing rod 6 can be disassembled and installed in the buckle 21 at the bottom of the first bracket structure 2. The buckle 21 can be an open clamp. It is a buckle 21, and the second reinforcing rod 6 can be snapped into it. The second reinforcing rod 6 is removed to free up the first accommodation space, and the first accommodation space is used to accommodate the fuselage transportation components and the fuselage.

[0050] In summary, when the transport device for the UAV air transport yard provided by the present invention is used, take the air transport yard of the fuselage, wings and tail of a medium and large UAV as an example: push the transport device for the UAV air transport yard to the loading area, unlock the locking component 22 connecting the second bracket structure 3 and the first bracket structure 2; rely on the crane to lift the second bracket structure 3 to the ground, and remove the second buffer layer 12 and the fourth buffer layer 18; use the wing hanger to complete the wing loading work, including the wing loading work in the second storage space and the third storage space; The punching layers 18 are respectively installed on the upper side of the wing, and are respectively clamped with the first buffer layer 11 and the third buffer layer 17; the tail is placed on the second buffer layer 12 and the fourth buffer layer 18, and covered with the fifth buffer layer 19 and the sixth buffer layer 20; the second bracket structure 3 is lifted back to the first bracket structure 2 by a crane, and the locking component 22 is locked; the wing is rolled and fastened; the second reinforcing rod 6 is removed and placed in the buckle 21, and the transport device for the UAV air transport field is lifted by the crane of a large transport aircraft, and the first accommodation space accommodates the fuselage and the fuselage transport components.

[0051] While various embodiments of the present invention have been described above, the above description is intended to be illustrative, not exhaustive, and not limited to the disclosed embodiments. Many modifications and variations will be apparent to those skilled in the art without departing from the scope and spirit of the described embodiments.

Claims

1. A transport device for unmanned aerial vehicle (UAV) transport, characterized in that: include: A support structure, a first bracket structure and a second bracket structure are arranged in sequence from bottom to top, and a movable part is provided at the lower end of the support structure. The interior of the support structure, the interior of the first bracket structure and the interior of the second bracket structure respectively form a first accommodating space, a second accommodating space and a third accommodating space, and the first accommodating space, the second accommodating space and the third accommodating space can respectively accommodate a fuselage, wings and tail for installation on one side of the fuselage, and wings and tail for installation on the other side of the fuselage.

2. The transport device for unmanned aerial vehicle (UAV) empty transport yard according to claim 1, characterized in that: The support structure includes multiple pairs of support legs, each pair of support legs includes two support legs, and the support legs are respectively arranged on both sides of the first bracket structure.

3. The transport device for unmanned aerial vehicle (UAV) empty transport yard according to claim 2, characterized in that: Two first reinforcing rods are cross-arranged between adjacent support legs on the same side.

4. The transport device for unmanned aerial vehicle (UAV) empty transport yard according to claim 1, characterized in that: The first bracket structure includes a first rectangular frame connected above the supporting structure, a plurality of first vertical poles are spaced apart on both sides of the upper part of the first rectangular frame, a first connecting rod is connected to the top of the plurality of first vertical poles on each side, a plurality of first cross beams are arranged inside the first rectangular frame, a first installation groove is formed on the upper side of the first cross beam, and the first installation groove is used to install the first buffer layer.

5. The transport device for unmanned aerial vehicle (UAV) empty transport yard according to claim 4, characterized in that: The bottom surface of the first buffer layer is bonded to the bottom of the first installation groove, and the top surface of the first buffer layer is provided with a first groove that matches the wing.

6. The transport device for unmanned aerial vehicle (UAV) empty transport yard according to claim 4, characterized in that: It also includes a second buffer layer, which is used to be arranged on the upper side of the wing. A first clipping groove is provided on the lower side of the second buffer layer, and the first clipping groove is clipped with the first buffer layer. The upper side of the second buffer layer is used to place the tail wing.

7. The transport device for unmanned aerial vehicle (UAV) empty transport yard according to claim 1, characterized in that: The second bracket structure includes a second rectangular frame detachably connected to the top of the first bracket structure, a plurality of second vertical poles are arranged at intervals on both sides of the upper part of the second rectangular frame, a second connecting rod is connected to the top of the plurality of second vertical poles on each side, a plurality of second cross beams are arranged inside the second rectangular frame, a second installation groove is formed on the upper side of the second cross beam, and the second installation groove is used to install a third buffer layer.

8. The transport device for unmanned aerial vehicle (UAV) empty transport yard according to claim 7, characterized in that: The bottom surface of the third buffer layer is bonded to the bottom of the second mounting groove, and the top surface of the third buffer layer is provided with a second groove that matches the wing.

9. The transport device for unmanned aerial vehicle (UAV) empty transport yard according to claim 7, characterized in that: It also includes a fourth buffer layer, which is used to be arranged on the upper side of the wing. The lower side of the fourth buffer layer is provided with a second clamping groove, and the second clamping groove is clamped with the third buffer layer.

10. The transport device for unmanned aerial vehicle (UAV) empty transport yard according to claim 2, characterized in that: A second reinforcing rod is detachably connected between each pair of support legs, and a buckle is provided on the lower side of the first bracket structure, and the second reinforcing rod can be buckled with the buckle.

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