Cover opening structure and aircraft transport case

Abstract

The utility model discloses an uncovering structure and an aircraft transport case, the aircraft transport case comprises the uncovering structure, the uncovering structure comprises a case body, an upper cover and a hinge structure, the case body is connected with the upper cover through the hinge structure, under the action of the hinge structure, the upper cover can slide relative to the case body, and the upper cover can be unfolded at an angle perpendicular to the case body; the uncovering structure and the aircraft transport case provided by the utility model can be quickly unfolded in a limited space and keep a stable state; through the design of the hinge structure, the upper cover can slide relative to the box body under the action of the hinge structure, and the upper cover can be unfolded at an angle perpendicular to the box body. The upper cover and the box body are connected more compactly, the space needed by the transport box in the ununfolded state is reduced, and therefore effective transport and storage can be conducted in the limited space. The extra space required for unfolding the upper cover is reduced, so that the transport case can be quickly deployed even in a space-limited environment.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to an opening structure and an aircraft transport box. Background Technique

[0002] Unmanned aerial vehicle technology plays an increasingly important role in modern applications, especially in situations that require quick response, such as emergency rescue, rapid logistics distribution, and environmental monitoring. These application scenarios require unmanned aerial vehicles to be quickly deployed and execute tasks. However, the existing unmanned aerial vehicle transportation and deployment systems have obvious limitations in actual operation.

[0003] In the design of existing unmanned aerial vehicle transport boxes, the unfolding process of the transport box usually requires a large amount of space, which becomes a significant problem in space-constrained environments. For example, in urban environments, or in situations where it is necessary to quickly deploy unmanned aerial vehicles from vehicles, ships, or aircraft, existing transport boxes are often difficult to use because of the large amount of space required for their unfolding. In addition, the unfolded transport box needs to maintain a stable state to ensure the safety and readiness of the unmanned aerial vehicle, but existing designs often cannot effectively maintain this state in limited space.

[0004] In order to achieve the rapid deployment of unmanned aerial vehicles, the design of the transport box must consider the optimal utilization of space. After the current transport box is unfolded, it often occupies too much space, which not only limits the usage scenarios of the transport box but also affects the deployment efficiency of unmanned aerial vehicles. Especially in situations that require quick response, the space required for the unfolding and maintaining the state of the transport box becomes a key limiting factor. Content of the Utility Model

[0005] The technical problem to be solved by the utility model is: to provide an opening structure and an aircraft transport box that can be quickly unfolded in limited space.

[0006] To solve the above technical problem, the technical solution adopted by the utility model is: an opening structure, including a box body, an upper cover, and a hinge structure. The box body and the upper cover are connected by the hinge structure. Under the action of the hinge structure, the upper cover can slide relative to the box body, and the upper cover can be unfolded at an angle perpendicular to the box body.

[0007] Further, the hinge structure includes a hinge, a sliding connection member, and a slide rail. The hinge is installed on the box body and connected to the sliding connection member. The sliding connection member is slidably installed on the slide rail, and the slide rail is installed on the upper cover.

[0008] Further, the upper cover is provided with an installation protrusion, and the slide rail is installed on the installation protrusion.

[0009] Further, the upper cover is provided with a positioning groove, and one end of the sliding rail is installed in the positioning groove.

[0010] Further, a limiting block is provided on the sliding rail, and the limiting block is located on the sliding track of the sliding connector.

[0011] To solve the above technical problems, the present utility model also provides an aircraft transport box, including the above-mentioned opening structure.

[0012] Further, two upper covers are provided on the box body, and the two upper covers are arranged above the box body in a split-open form.

[0013] Further, a lock catch is provided at the edge of the upper cover.

[0014] Further, a plurality of storage grooves are provided in the box body, and the storage grooves are in an inverted conical shape for placing unmanned aircraft.

[0015] Further, the inner side of the upper cover has a support portion, and the support portion protrudes toward the storage groove.

[0016] The beneficial effects of the present utility model are as follows: The opening structure and the aircraft transport box provided by the present utility model can be quickly deployed and maintained in a stable state within a limited space; through the design of the hinge structure, under the action of the hinge structure, the upper cover can slide relative to the box body, and the upper cover can be deployed at an angle perpendicular to the box body. This makes the connection between the upper cover and the box body more compact, reduces the space required by the transport box in the undeployed state, so that effective transportation and storage can be carried out even in a limited space; reduces the additional space required for the upper cover to deploy, enabling the transport box to be quickly deployed even in an environment with limited space. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 is the assembly drawing of the opening structure and the aircraft transport box of Embodiment 1 of the present utility model;

[0018] Figure 2 is the exploded view of the opening structure and the aircraft transport box of Embodiment 1 of the present utility model.

[0019] Reference Numerals Explanation:

[0020] 1. Box body; 11. Storage groove; 2. Upper cover; 21. Installation protrusion; 22. Positioning groove; 23. Support portion; 3. Hinge structure; 31. Hinge; 32. Sliding connector; 33. Sliding rail; 34. Limiting block. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0021] To describe in detail the technical content, the achieved objectives and the effects of the present utility model, the following is described in conjunction with the embodiments and with reference to the accompanying drawings.

[0022] Please refer to Figure 1 and Figure 2 , an opening structure, comprising a box body 1, an upper cover 2, and a hinge structure 3. The box body 1 is connected to the upper cover 2 via the hinge structure 3. Under the action of the hinge structure 3, the upper cover 2 can slide relative to the box body 1, and the upper cover 2 can be unfolded at an angle perpendicular to the box body 1.

[0023] As can be seen from the above description, the beneficial effects of the present utility model are as follows: Through the design of the hinge structure 3, under the action of the hinge structure 3, the upper cover 2 can slide relative to the box body 1, and the upper cover 2 can be unfolded at an angle perpendicular to the box body 1. This makes the connection between the upper cover 2 and the box body 1 more compact, reduces the space required for the transport box in the unfolded state, so that effective transportation and storage can be carried out even in a limited space; reduces the additional space required for the unfolding of the upper cover 2, enabling the transport box to be quickly deployed even in an environment with limited space.

[0024] Furthermore, the hinge structure 3 includes a hinge 31, a sliding connection member 32, and a slide rail 33. The hinge 31 is installed on the box body 1 and is connected to the sliding connection member 32. The sliding connection member 32 is slidably installed on the slide rail 33, and the slide rail 33 is installed on the upper cover 2.

[0025] As can be seen from the above description, the design of the hinge 31 and the slide rail 33 enables the upper cover 2 to descend along the slide rail 33 through a pressing action after being lifted. This design reduces the additional space required for the unfolding of the upper cover 2, enabling the transport box to be quickly deployed even in an environment with limited space; the simplified design of the hinge structure 3 makes the lifting and descending actions of the upper cover 2 faster and simpler, reducing the time consumption during the deployment process and improving the response speed of the drone; the connection method between the hinge 31 and the sliding connection member 32 and the design of the slide rail 33 ensure the stability of the upper cover 2 during the lifting and descending processes, reducing the accidental risks caused by space limitations or improper operations and improving the safety of the operation.

[0026] Furthermore, the upper cover 2 is provided with a mounting protrusion 21, and the slide rail 33 is installed on the mounting protrusion 21.

[0027] As can be seen from the above description, the design of the mounting protrusion 21 provides a fixed point for the slide rail 33, making the installation of the slide rail 33 more stable, reducing the shaking during transportation, and improving the overall stability of the transport box.

[0028] Furthermore, the upper cover 2 is provided with a positioning groove 22, and one end of the slide rail 33 is installed in the positioning groove 22.

[0029] As described above, the design of the positioning groove 22 ensures the precise alignment of the slide rail 33 during installation, prevents the offset of the slide rail 33, and guarantees the smoothness and stability when the upper cover 2 descends.

[0030] Further, a limit block 34 is provided on the slide rail 33, and the limit block 34 is located on the sliding track of the sliding connection member 32.

[0031] As described above, the design of the limit block 34 prevents the excessive sliding of the sliding connection member 32 on the slide rail 33, ensures the stability when the upper cover 2 descends to a predetermined position, and prevents damage caused by excessive descent.

[0032] An aircraft transport box includes the above-mentioned opening structure.

[0033] Further, two upper covers 2 are provided on the box body 1, and the two upper covers 2 are arranged above the box body 1 in a split-open form.

[0034] As described above, arranging two upper covers 2 on the box body 1 in a split-open form can increase the storage capacity of the transport box while maintaining the compactness and portability of the transport box.

[0035] Further, a lock catch is provided at the edge of the upper cover 2.

[0036] As described above, the setting of the lock catch enhances the security of the transport box, ensures that the upper cover 2 will not be accidentally opened during transportation, and protects the unmanned aircraft from damage.

[0037] Further, a plurality of storage grooves 11 are provided in the box body 1, and the storage grooves 11 are in an inverted conical shape for placing the unmanned aircraft.

[0038] As described above, by providing the inverted conical storage grooves 11 in the box body 1, the unmanned aircraft can be stably placed, providing good support and protection.

[0039] Further, the inner side of the upper cover 2 has a support portion 23, and the support portion 23 protrudes toward the storage groove 11.

[0040] As described above, the support portion 23 is provided on the inner side of the upper cover 2 and protrudes toward the storage groove 11, which can effectively fix the unmanned aircraft and prevent it from moving or being damaged due to vibration or impact during transportation.

[0041] Please refer to Figure 1 and Figure 2, Embodiment 1 of the present utility model is: An opening structure, including a box body 1, an upper cover 2, and a hinge structure 3. The box body 1 is connected to the upper cover 2 through the hinge structure 3. Under the action of the hinge structure 3, the upper cover 2 can slide relative to the box body 1, and the upper cover 2 can be unfolded at an angle perpendicular to the box body 1. It is easy to understand that through the design of the hinge structure 3, under the action of the hinge structure 3, the upper cover 2 can slide relative to the box body 1, and the upper cover 2 can be unfolded at an angle perpendicular to the box body 1. This makes the connection between the upper cover 2 and the box body 1 more compact, reduces the space required for the transport box in the unfolded state, so that effective transportation and storage can be carried out even in a limited space; reduces the additional space required for the upper cover 2 to unfold, so that the transport box can be quickly deployed even in an environment with limited space.

[0042] Preferably, the hinge structure 3 includes a hinge 31, a sliding connector 32, and a slide rail 33. The hinge 31 is installed on the box body 1 and connected to the sliding connector 32. The sliding connector 32 is slidably installed on the slide rail 33, and the slide rail 33 is installed on the upper cover 2. The design of the hinge 31 and the slide rail 33 enables the upper cover 2 to descend along the slide rail 33 through a pressing action after being lifted. This design reduces the additional space required for the upper cover 2 to unfold, so that the transport box can be quickly deployed even in an environment with limited space; the simplified design of the hinge structure 3 makes the lifting and descending actions of the upper cover 2 faster and simpler, reduces the time consumption during the deployment process, and improves the response speed of the drone; the connection method between the hinge 31 and the sliding connector 32 and the design of the slide rail 33 ensure the stability of the upper cover 2 during the lifting and descending processes, reduce the accidental risks caused by space limitations or improper operations, and improve the safety of the operation.

[0043] In this embodiment, the upper cover 2 is provided with a mounting protrusion 21, and the slide rail 33 is installed on the mounting protrusion 21. The design of the mounting protrusion 21 provides a fixed point for the slide rail 33, making the installation of the slide rail 33 more stable, reducing the shaking during transportation, and improving the overall stability of the transport box; specifically, the upper cover 2 is provided with a positioning groove 22, and one end of the slide rail 33 is installed in the positioning groove 22. The design of the positioning groove 22 ensures the accurate alignment of the slide rail 33 during installation, prevents the offset of the slide rail 33, and ensures the smoothness and stability of the upper cover 2 during descent; more specifically, the slide rail 33 is provided with a limit block 34, and the limit block 34 is located on the sliding track of the sliding connector 32. The design of the limit block 34 prevents the sliding connector 32 from sliding excessively on the slide rail 33, ensures the stability of the upper cover 2 when it descends to a predetermined position, and prevents damage caused by excessive descent.

[0044] Embodiment 2 of the present utility model is: An aircraft transport box, including an opening structure, and the opening structure is the opening structure described in Embodiment 1. Two upper covers 2 are arranged on the box body 1, and the two upper covers 2 are arranged above the box body 1 in a split-open form. It can be understood that arranging two upper covers 2 on the box body 1 in a split-open form can increase the storage capacity of the transport box while maintaining the compactness and portability of the transport box.

[0045] Optionally, a lock catch (not shown in the figure) is provided at the edge of the upper cover 2, and the lock catch is used to lock with the box body 1. The setting of the lock catch enhances the safety of the transport box, ensuring that the upper cover 2 will not be accidentally opened during transportation and protecting the unmanned aircraft from damage.

[0046] Preferably, a plurality of storage grooves 11 are provided in the box body 1, and the storage grooves 11 are in an inverted conical shape for placing the unmanned aircraft. By providing the inverted conical storage grooves 11 in the box body 1, the unmanned aircraft can be stably placed, providing good support and protection. Specifically, a support portion 23 is provided on the inner side of the upper cover 2, and the support portion 23 protrudes towards the storage groove 11. The support portion 23 is provided on the inner side of the upper cover 2 and protrudes towards the storage groove 11, which can effectively fix the unmanned aircraft and prevent it from moving or being damaged due to vibration or impact during transportation.

[0047] In summary, the opening structure and the aircraft transport box provided by the present utility model can be quickly deployed and maintained in a stable state within a limited space; through the design of the hinge structure 3, the connection between the upper cover 2 and the box body 1 is made more compact, reducing the space required for the transport box in the undeployed state, so that effective transportation and storage can also be carried out within a limited space; the design of the hinge 31 and the slide rail 33 enables the upper cover 2 to descend along the slide rail 33 by pressing after being lifted, which reduces the additional space required for the deployment of the upper cover 2, enabling the transport box to be quickly deployed even in a space-constrained environment; the simplified design of the hinge structure 3 makes the lifting and descending actions of the upper cover 2 faster and simpler, reducing the time consumption during the deployment process and improving the response speed of the unmanned aircraft; the connection method of the hinge 31 and the sliding connection member 32 and the design of the slide rail 33 ensure the stability of the upper cover 2 during the lifting and descending processes, reducing the accidental risks caused by space limitations or improper operations and improving the safety of operation.

[0048] The above are only the embodiments of the present utility model, and do not limit the patent scope of the present utility model accordingly. All equivalent transformations made by using the content of the specification and drawings of the present utility model, or directly or indirectly applied in the relevant technical fields, are similarly included in the patent protection scope of the present utility model.

Claims

1. An open lid structure, comprising a box body, an upper lid, and a hinge structure, characterized in that, The box body and the upper cover are connected through the hinge structure. Under the action of the hinge structure, the upper cover can slide relative to the box body, and the upper cover can be unfolded at an angle perpendicular to the box body.

2. The opening structure according to claim 1, wherein, The hinge structure includes a hinge, a sliding connector, and a slide rail. The hinge is installed on the box body and connected to the sliding connector. The sliding connector is slidably installed on the slide rail, and the slide rail is installed on the upper cover.

3. The opening structure according to claim 2, characterized in that The upper cover is provided with an installation protrusion, and the slide rail is installed on the installation protrusion.

4. The opening structure according to claim 2, wherein The upper cover is provided with a positioning groove, and one end of the slide rail is installed in the positioning groove.

5. The open lid structure according to claim 2, characterized in that, A limiting block is provided on the slide rail, and the limiting block is located on the sliding track of the sliding connector.

6. An aircraft transport box, characterized in that, It includes the open cover structure according to any one of claims 1-5.

7. The aircraft transport box according to claim 6, wherein, Two upper covers are arranged on the box body, and the two upper covers are arranged above the box body in a form of being opened oppositely.

8. The aircraft transport box according to claim 7, characterized in that, A lock catch is arranged at the edge of the upper cover.

9. The aircraft transport box according to any one of claims 6 to 8, characterized in that, A plurality of storage grooves are arranged in the box body, and the storage grooves are in an inverted conical shape for placing unmanned aerial vehicles.

10. The aircraft transport box according to claim 9, characterized in that, The inner side of the upper cover has a supporting part, and the supporting part protrudes towards the storage groove.

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