Aviation case convenient to assemble and disassemble
Through the modularly designed airbox, the problems of complex assembly and disassembly of traditional airboxes are solved, and flexible assembly and disassembly are achieved, reducing transportation costs, improving management efficiency, and adapting to a variety of transportation needs.
Patent Information
- Application Number
- CN202422357244.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-26
- Publication Date
- 2025-07-01
- Estimated Expiration
- 2034-09-26
AI Technical Summary
The traditional airbox has a complex structure and is not easy to disassemble, which leads to difficulty in assembly, inconvenient maintenance and large space, making it difficult to adapt to different transportation needs.
It adopts a modular design, including the base, front panel, side panel, rear panel, cover panel, vertical corner parts and corner parts, and can be flexibly assembled and disassembled through plug slots and screw connections, combining casters and lock bodies to improve convenience.
It realizes flexible assembly and disassembly of air boxes, facilitates efficient stacking and space utilization, reduces transportation costs, improves management efficiency, adapts to a variety of transportation needs, and enhances economics and flexibility.
Smart Images

Figure CN223046159U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of flight cases, in particular to a flight case that is convenient for assembly and disassembly. Background Technique
[0002] In the field of air transportation, flight cases, as important packaging tools, are used to protect goods from damage during transportation. Traditional flight cases mostly adopt an integrally formed monolithic structure. Although the structure is stable, there are problems such as complex assembly, difficult disassembly, hard maintenance or component replacement, and it is not conducive to saving space during transportation, which brings a lot of inconvenience to users. Therefore, it is of great practical significance to develop a flight case that is easy to disassemble and assemble simply. Content of the Utility Model
[0003] The purpose of the utility model is to provide a flight case that is convenient for assembly and disassembly to solve the problems raised in the above background technique. To achieve the above purpose, the utility model provides the following technical solutions:
[0004] A flight case that is convenient for assembly and disassembly includes a base, a front panel, side panels, a rear panel, a cover plate, vertical corner fittings, and corner wrapping fittings; plug-in slots are provided around the base; the front panel, rear panel, and side panels are correspondingly plugged into the plug-in slots; the front panel and the rear panel are respectively connected to the side panels through the vertical corner fittings; the cover plate is rotatably connected to the rear panel; each corner of the flight case is connected and fixed through the corner wrapping fittings.
[0005] Further, the base includes a bottom plate and bottom corner fittings, the bottom corner fittings are connected around the periphery of the bottom plate, and plug-in slots are provided on the bottom corner fittings.
[0006] Further, the corner wrapping fittings are respectively connected and fixed to the bottom plate, the front panel, the side panels, and the rear panel through screws.
[0007] Further, the flight case further includes casters, and the casters are arranged at the bottom of the base.
[0008] Further, the bottom corner fittings are angle aluminum profiles.
[0009] Further, the vertical corner fittings are angle aluminum profiles.
[0010] Further, the flight case further includes flat-edge wrapping fittings, the flat-edge wrapping fittings are arranged on the front panel and the side panels, and the cover plate covers the inside of the flat-edge wrapping fittings.
[0011] Further, the flat-edge wrapping fittings are flat-edge winged wrapping aluminum materials.
[0012] Further, a lock body is provided on the cover plate.
[0013] Furthermore, a handle is provided on the side plate.
[0014] The beneficial effects of the present utility model are as follows: By introducing a modular design, the flight case of the present utility model enables flexible assembly and disassembly; it is convenient for efficient stacking and space utilization, reduces the storage space requirement, facilitates inventory management, and improves management efficiency; it can adapt to different transportation spaces, reduces transportation costs; it is also convenient for maintenance and module replacement; greatly improves the flexibility and economy of the flight case, meets the packaging and transportation requirements of various modern products, adapts to market changes, and provides an efficient and economic solution. BRIEF DESCRIPTION OF THE DRAWINGS
[0015] In order to more clearly illustrate the technical solutions in the embodiments of the present utility model, the following will briefly introduce the drawings required to be used in the embodiments. Obviously, the drawings described below are only some embodiments of the present utility model. For those of ordinary skill in the art, without creative efforts, other drawings can be obtained based on these drawings.
[0016] Figure 1 It is a schematic diagram of the disassembled structure of the present utility model.
[0017] Figure 2 It is a schematic diagram of the open state of the cover plate of the present utility model.
[0018] Figure 3 It is a schematic diagram of the closed state of the cover plate of the present utility model.
[0019] Figure 4 It is an installation schematic diagram of the vertical corner fitting of the present utility model.
[0020] Figure 5 It is a schematic diagram of the structure of the base of the present utility model.
[0021] Figure 6 It is a schematic diagram of the structures of the vertical corner fitting, the corner protector, and the flat-edge trim of the present utility model.
[0022] It should be noted that the drawings are not necessarily drawn to scale, but are only shown in a schematic manner that does not affect the understanding of the reader. DETAILED DESCRIPTION OF THE EMBODIMENTS
[0023] The following will clearly and completely describe the technical solutions in the embodiments of the present utility model with reference to the drawings in the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, rather than all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts belong to the scope of protection of the present utility model.
[0024] In the present utility model, the orientation or positional relationship indicated by terms such as "upper", "lower", "left", "right", "front", "rear", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal", etc. is based on the orientation or positional relationship shown in the drawings. These terms are mainly used to better describe the present utility model and its embodiments, and are not intended to limit that the indicated devices, elements or components must have a specific orientation, or be constructed and operated in a specific orientation.
[0025] Moreover, in addition to being used to represent the orientation or positional relationship, some of the above terms may also be used to represent other meanings. For example, the term "upper" may also be used to represent a certain attachment relationship or connection relationship in some cases. For those of ordinary skill in the art, the specific meanings of these terms in the present utility model can be understood according to specific circumstances.
[0026] In addition, the terms "mounted", "arranged", "provided with", "connected", "linked" should be understood in a broad sense. For example, it may be a fixed connection, a detachable connection, or an integral structure; it may be a mechanical connection or an electrical connection; it may be directly connected, or indirectly connected through an intermediate medium, or there may be internal communication between two devices, elements or components. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.
[0027] In addition, terms such as "first", "second", etc. are mainly used to distinguish different devices, elements or components (the specific types and structures may be the same or different), and are not intended to indicate or imply the relative importance and quantity of the indicated devices, elements or components. Unless otherwise specified, the meaning of "a plurality" is two or more.
[0028] It should also be understood that the terms used in the specification of the present utility model are only for the purpose of describing specific embodiments and are not intended to limit the present utility model. As used in the specification of the present utility model and the appended claims, unless the context clearly indicates otherwise, the singular forms "a", "an" and "the" are intended to include the plural forms.
[0029] It should be further understood that the term " / and" used in the specification of the present utility model and the appended claims refers to any combination and all possible combinations of one or more of the related listed items, and includes these combinations.
[0030] Such as Figures 1 to 6As shown in the figure, a flight case that is convenient for assembly and disassembly includes a base 1, a front panel 2, side panels 3, a rear panel 4, a cover plate 5, vertical corner fittings 6 and corner protectors 7; a plug-in groove 101 is provided around the base 1; the front panel 2, the rear panel 4 and the side panels 3 are correspondingly plugged into the plug-in groove 101; the front panel 2 and the rear panel 4 are respectively connected to the side panels 3 through the vertical corner fittings 6; the cover plate 5 is rotatably connected to the rear panel 4; and each corner of the flight case is connected and fixed through the corner protector 7.
[0031] As an example, a flight case that is convenient for assembly and disassembly provided by an embodiment of the present application is a new modular flight case structure designed for convenient transportation and storage. The flight case includes seven modular composite materials, namely a base 1, a front panel 2, side panels 3, a rear panel 4, a cover plate 5, vertical corner fittings 6 and corner protectors 7. Each module is a standardized module and can be used independently or in combination; among them, the front panel 2, the side panels 3, the rear panel 4 and the cover plate 5 are formed plates, and the cover plate 5 is pre-rotatably connected to the rear panel 4 through a hinge to form an integral body, so that the cover plate 5 can be flipped and closed or opened; the vertical corner fittings 6 and the corner protectors 7 are formed aluminum materials; the base 1 is an assembled component formed by a bottom plate 11 and bottom corner fittings 12. A plug-in groove 101 is provided around the base 1 for vertically plugging the front panel 2, the rear panel 4 and the side panels 3, so that the front panel 2, the rear panel 4 and the side panels 3 are correspondingly distributed and connected around the base 1 to form a box structure. At the same time, the vertical corner fittings 6 are provided with slots that can be plugged into the front panel 2, the rear panel 4 and the side panels 3. The front panel 2 and the rear panel 4 are respectively connected to the side panels 3 through the vertical corner fittings 6 to form an integral body, so that the box structure is fixed. In addition, each corner of the box structure is connected and fixed through the corner protector 7 to further strengthen the stability of the flight case.
[0032] The usage method of the flight case in this embodiment is as follows: During the assembly process, taking the assembled base 1 as the bottom layer foundation of the flight case, first plug the front panel 2, the rear panel 4 and the side panels 3 correspondingly into the plug-in grooves 101 around the base 1 to form a box structure, then connect and fix the front panel 2, the rear panel 4 and the side panels 3 through the vertical corner fittings 6, and finally further strengthen the connection at each corner of the flight case through the corner protector 7, and the complete flight case can be assembled. The cover plate 5 pre-rotatably connected to the rear panel 4 through a hinge can be used to close or open the flight case. During transportation or storage, first disassemble and separate the seven modules of the base 1, the front panel 2, the side panels 3, the rear panel 4, the cover plate 5, the vertical corner fittings 6 and the corner protector 7 that form the flight case, and then they can be stacked and transported.
[0033] Different from the existing technology flight cases, the flight case provided in this embodiment realizes flexible assembly and disassembly by introducing a modular design; it is convenient for efficient stacking and space utilization, reduces storage space requirements, facilitates inventory management, and improves management efficiency; it can adapt to different transportation spaces, reduces transportation costs; it is also convenient for maintenance and module replacement; greatly improves the flexibility and economy of the flight case, meets the packaging and transportation needs of various modern products, adapts to market changes, and provides an efficient and economic solution.
[0034] In one embodiment, referring to Figures 1 to 5 , the base 1 includes a bottom plate 11 and bottom corner fittings 12. The bottom corner fittings 12 are connected around the four sides of the bottom plate 11, and plug-in slots 101 are provided on the bottom corner fittings 12.
[0035] As an example, the bottom plate 11 is a processed plate, and the bottom corner fittings 12 are processed aluminum materials; the bottom corner fittings 12 are provided with slots for plugging the bottom plate 11 and plug-in slots 101 for plugging the front plate 2, side plates 3, and rear plate 4. When assembling the flight case, first plug the bottom corner fittings 12 around the four sides of the bottom plate 11, and make the plug-in slots 101 of the bottom corner fittings 12 face upward; then respectively plug the front plate 2, rear plate 4, and side plates 3 into the plug-in slots 101 around the base 1 corresponding to their positions, and a box structure can be formed.
[0036] In one embodiment, referring to Figures 1 to 4 , the corner fittings 7 are respectively connected and fixed to the bottom plate 11, front plate 2, side plates 3, and rear plate 4 by screws.
[0037] As an example, the corner fittings 7 are respectively connected and fixed to the bottom plate 11, front plate 2, side plates 3, and rear plate 4 by screws. This connection method is simple and fast, and is easy to disassemble and repair.
[0038] In one embodiment, referring to Figures 1 to 5 , the flight case further includes casters 8, and the casters 8 are arranged at the bottom of the base 1.
[0039] As an example, in order to improve the mobility of the flight case, the present invention also provides casters 8 at the bottom of the bottom plate 11 module, which is convenient for the handling and movement of the flight case.
[0040] In one embodiment, the bottom corner fittings 12 are angle aluminum profiles. The vertical corner fittings 6 are angle aluminum profiles.
[0041] As an example, both the bottom corner fittings 12 and the vertical corner fittings 6 are preferably angle aluminum profiles. This material has high strength and corrosion resistance, and can meet the strict requirements of air transportation.
[0042] In one embodiment, referring to Figures 1 to 3 、and Figure 6, the flight case further includes a flat-edge edging member 9, which is disposed on the front panel 2 and the side panels 3, and the cover plate 5 is closed inside the flat-edge edging member 9.
[0043] As an example, the flight case further includes a flat-edge edging member 9, which is disposed on the front panel 2 and the side panels 3, and the cover plate 5 is closed inside the flat-edge edging member 9 to protect the edge of the opening of the flight case and hide the cover plate 5 inside the flat-edge edging member 9 to improve the aesthetics.
[0044] In one embodiment, the flat-edge edging member 9 is a flat-edge winged edging aluminum material.
[0045] As an example, the flat-edge edging member 9 is preferably a flat-edge winged edging aluminum material, which has good strength and durability.
[0046] In one embodiment, refer to Figure 2 and Figure 3 , a lock body 51 is provided on the cover plate 5.
[0047] As an example, to enhance the security of the flight case, a lock body 51 is provided on the cover plate 5 to lock the cover plate 5 and prevent the flight case from being accidentally opened.
[0048] In one embodiment, refer to Figures 1 to 4 , a handle 31 is provided on the side panel 3.
[0049] As an example, for convenient handling, a handle 31 is also provided on the side panel 3 to facilitate manual lifting and moving of the flight case.
[0050] For the embodiments of the present invention, it should also be noted that, without conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other to obtain new embodiments.
[0051] The above is only a preferred embodiment of the present invention, and it does not impose any form of limitation on the present invention. The protection scope of the present invention should be subject to the protection scope of the claims. Although the present invention has been disclosed above with preferred embodiments, it is not intended to limit the present invention. Any person skilled in the art can make some changes or modifications to the above-disclosed technical content to obtain equivalent embodiments with equivalent changes, but as long as it does not depart from the technical content of the present invention, any simple modification, equivalent change and modification made to the above embodiments based on the technical essence of the present invention still fall within the scope of the technical solution of the present invention.
Claims
1. An aviation box that is easy to assemble and disassemble, characterized in that: The aviation box comprises a base (1), a front panel (2), a side panel (3), a rear panel (4), a cover panel (5), a vertical angle piece (6) and an angle piece (7); the base (1) is provided with insertion slots (101) around the periphery; the front panel (2), the rear panel (4) and the side panel (3) are correspondingly inserted into the insertion slots (101); the front panel (2) and the rear panel (4) are respectively connected to the side panel (3) via the vertical angle piece (6); the cover panel (5) is rotatably connected to the rear panel (4); and the corners of the aviation box are connected and fixed via the angle piece (7).
2. The aviation box according to claim 1, characterized in that: The base (1) comprises a bottom plate (11) and a bottom corner piece (12); the bottom corner piece (12) is connected around the bottom plate (11); and a plug-in slot (101) is provided on the bottom corner piece (12).
3. The aviation box according to claim 2, characterized in that: The corner pieces (7) are respectively connected and fixed to the bottom plate (11), the front plate (2), the side plates (3) and the rear plate (4) by means of screws.
4. The aviation box according to claim 2, characterized in that: The aviation box also includes casters (8), and the casters (8) are arranged at the bottom of the base (1).
5. The aviation box according to claim 2, characterized in that: The bottom corner piece (12) is an aluminum angle profile.
6. The aviation box according to claim 1, characterized in that: The vertical corner piece (6) is an aluminum angle profile.
7. The aviation box according to claim 1, characterized in that: The aviation box further comprises a flat edge binding member (9), wherein the flat edge binding member (9) is arranged on the front plate (2) and the side plate (3), and the cover plate (5) covers the inner side of the flat edge binding member (9).
8. The aviation box according to claim 7, characterized in that: The flat edge edging piece (9) is a flat edge winged edging aluminum material.
9. The aviation box according to claim 1, characterized in that: A lock body (51) is arranged on the cover plate (5).
10. The aviation box according to claim 1, characterized in that: A handle (31) is provided on the side plate (3).