Aviation case

Abstract

The utility model relates to the technical field of packaging boxes, in particular to a flight case which comprises a top plate and a case body, in the flight case, the case body is a container with a first opening in one face, a plurality of first positioning blocks and a plurality of first buckles are arranged at the first opening, and the shape of the top plate is matched with that of the first opening; a plurality of first through grooves and a plurality of first buckling grooves are formed in the top plate, the first through grooves correspond to the first positioning blocks one to one, the first buckling grooves are matched with the first buckles, the position of the top plate is determined through the matching effect of the first positioning blocks and the first through grooves, and the top plate is fixedly assembled with the box body through the matching effect of the first buckles and the first buckling grooves; the problems that a traditional aviation case is fixed through screws, so that when case plates are assembled into the finished aviation case, the screws need to be tightened one by one, operation time is long, and efficiency is low are solved.

Description

Technical Field

[0001] The present application relates to the technical field of packaging boxes, and in particular to an aviation box. Background Art

[0002] Air box is a new type of packaging product that replaces transportation because traditional simple wooden box packaging cannot solve the problems of high-tech products not being effectively protected during long-distance transportation and having poor maneuverability.

[0003] Currently, aviation boxes are generally fixed by screws. Therefore, when assembling the box panels into a finished aviation box, each screw needs to be tightened one by one, which takes a long time and is inefficient. Utility Model Content

[0004] The present application provides an aviation box, which aims to solve the problem that traditional aviation boxes are fixed by screws, which requires each screw to be tightened one by one when assembling the box panels into a finished aviation box, resulting in long operation time and low efficiency.

[0005] In order to solve the above technical problems, the present application proposes an aviation box, which includes: a top plate and a box body;

[0006] The box body is a container with a first opening on one side, and a plurality of first positioning blocks and a plurality of first buckles are provided at the first opening. The shape of the top plate matches the shape of the first opening, and a plurality of first through grooves and a plurality of first buckle grooves are provided on the top plate. The first through grooves correspond one-to-one with the first positioning blocks, and the first buckle grooves match the first buckles. The position of the top plate is determined by the cooperation of the first positioning block and the first through groove, and the top plate is fixedly assembled with the box body by the cooperation of the first buckles and the first buckle grooves.

[0007] Furthermore, a notch is provided at the first buckle slot, and the notch is communicated with the edge of the top plate. The provision of the notch facilitates pushing the first buckle out of the first buckle slot.

[0008] Furthermore, the box body includes two first side panels and two second side panels, the two first side panels are arranged in parallel and spaced apart, the two second side panels are arranged in parallel and spaced apart, and the first side panels are perpendicular to the second side panels.

[0009] Furthermore, a plurality of second positioning blocks and a plurality of second buckles are provided on both sides of the first side plate, and the second positioning blocks and the second buckles are alternately arranged in the vertical direction.

[0010] Furthermore, a plurality of second through slots and a plurality of second buckle slots are provided on both sides of the second side plate, the second through slots correspond one-to-one to the second positioning blocks, and the second buckle slots correspond one-to-one to the second buckles.

[0011] Furthermore, the box body also includes a bottom plate, a first positioning groove is provided at the edge of the bottom plate, and the first side plate and the second side plate are respectively provided with a first ridge and a second ridge on the side close to the bottom plate, and the first ridge and the second ridge are both inserted into the first positioning groove.

[0012] Furthermore, a second positioning groove is provided on the side of the top plate close to the box body, and a third ridge and a fourth ridge are provided on the side of the first side plate and the second side plate close to the top plate respectively, and the third ridge and the fourth ridge are both inserted into the second positioning groove.

[0013] Furthermore, the first positioning block is located on the fourth convex strip of the second side plate.

[0014] Furthermore, the first buckle is located on the third protruding strip of the first side panel.

[0015] The beneficial effects of the present application are: in the aviation box provided in the present application, the box body is a container having a first opening on one side, and a plurality of first positioning blocks and a plurality of first clips are provided at the first opening. The shape of the top plate matches the shape of the first opening, and a plurality of first through grooves and a plurality of first clip grooves are provided on the top plate. The first through grooves correspond one-to-one to the first positioning blocks, and the first clip grooves match the first clips. The position of the top plate is determined by the cooperation of the first positioning blocks and the first through grooves, and the top plate is fixedly assembled with the box body by the cooperation of the first clips and the first clip grooves, so that when the box panel components are assembled into a finished aviation box, the assembly is simple and the operation is convenient. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the following briefly introduces the drawings required for describing the embodiments. Obviously, the drawings described below are only some embodiments of the present application. For those skilled in the art, other drawings can be obtained based on these drawings without inventive efforts. Among them:

[0017] Figure 1 This is a schematic diagram of the three-dimensional structure of an aviation box according to one embodiment of the present invention;

[0018] Figure 2 This is a schematic diagram of the three-dimensional structure of the first side panel in the aviation box according to one embodiment of the present utility model;

[0019] Figure 3This is a schematic diagram of the three-dimensional structure of the second side panel in the aviation box according to one embodiment of the present utility model;

[0020] Figure 4 This is a schematic diagram of the three-dimensional structure of the top plate in the aviation box according to one embodiment of the present utility model;

[0021] Figure 5 It is a schematic diagram of the three-dimensional structure of the bottom plate in the aviation box according to one embodiment of the present utility model.

[0022] Explanation of the accompanying drawings: 100, box body; 110, first side panel; 111, second positioning block; 112, second buckle; 113, first ridge; 114, third ridge; 120, second side panel; 121, second through groove; 122, second buckle groove; 123, second ridge; 124, fourth ridge; 130, first positioning block; 140, first buckle; 200, top panel; 210, first through groove; 220, first buckle groove; 230, notch; 300, bottom panel; 310, first positioning groove. DETAILED DESCRIPTION

[0023] In order to make the purpose, technical solutions and advantages of this application more clear, the following further describes this application in detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain this application and are not intended to limit this application.

[0024] Those skilled in the art will understand that, unless expressly stated otherwise, the singular forms "a", "an", "above", and "the" used herein may also include plural forms. It should be further understood that the term "comprising" used in the specification of this application refers to the presence of features, integers, steps, operations, elements, modules, and / or components, but does not exclude the presence or addition of one or more other features, integers, steps, operations, elements, modules, components, and / or groups thereof. It should be understood that when we refer to an element as being "connected" or "coupled" to another element, it may be directly connected or coupled to the other element, or there may be intermediate elements. In addition, "connected" or "coupled" as used herein may include wireless connections or wireless couplings. The term "and / or" used herein includes all or any module and all combinations of one or more associated listed items.

[0025] It will be understood by those skilled in the art that, unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by those skilled in the art to which this application belongs. It should also be understood that terms such as those defined in common dictionaries should be understood to have meanings consistent with their meanings in the context of the prior art and will not be interpreted in an idealized or overly formal sense unless specifically defined as herein.

[0026] like Figure 1 As shown, the present application provides an aviation box, which includes a top plate 200 and a box body 100. The box body 100 is a container with a first opening on one side. The first opening is provided with a plurality of first positioning blocks 130 and a plurality of first clips 140. The shape of the top plate 200 matches the shape of the first opening. The top plate 200 is provided with a plurality of first through grooves 210 and a plurality of first clip grooves 220. The first through grooves 210 correspond one-to-one to the first positioning blocks 130, and the first clip grooves 220 match the first clips 140. The position of the top plate 200 is determined by the cooperation of the first positioning block 130 and the first through groove 210. The top plate 200 is fixedly assembled with the box body 100 by the cooperation of the first clips 140 and the first clip grooves 220.

[0027] In one embodiment, the housing 100 is in the shape of a rectangular parallelepiped, with a first opening that is rectangular. The top plate 200 is a rectangular plate. The shape of the top plate 200 matches the shape of the first opening. The first positioning block 130 is a block-shaped structure disposed at the first opening of the housing 100. Its primary function is to cooperate with a first through-slot 210 on the top plate 200 to precisely determine the position of the top plate 200. The first latch 140 is also located at the first opening of the housing 100. The first latch 140 and the first latch slot 220 on the top plate 200 mate with each other. When the first latch 140 engages the first latch slot 220, the top plate 200 and the housing 100 are securely fixed together. The first through-slot 210 is a groove-like structure provided on the top plate 200. The number and position of the first through-slot 210 correspond one-to-one with the first positioning block 130, allowing the positioning block to smoothly fit into the groove and perform its positioning function. The first buckle groove 220 is a groove of a specific shape provided on the top plate 200 to accommodate the first buckle 140 . A plurality of first through grooves 210 and a plurality of first buckle grooves 220 are surrounded around the edge of the top plate 200 .

[0028] In summary, through the cooperation of the first positioning block 130 and the first through-slot 210, the position of the top plate 200 can be accurately determined, avoiding the displacement or misalignment of the top plate 200 during the installation process, and ensuring the regularity of the overall appearance of the aviation box. Secondly, the matching fixing method of the first clip 140 and the first clip slot 220 makes the connection between the top plate 200 and the box body 100 very firm. During transportation, even if it encounters bumps, vibrations, etc., the top plate 200 will not easily loosen or fall off, thereby effectively protecting the safety of the items in the box. Furthermore, this structural design is relatively simple and easy to operate, which can improve assembly efficiency during the assembly process.

[0029] like Figure 4 As shown, a notch 230 is provided at the first buckle groove 220 , and the notch 230 is connected to the edge of the top plate 200 . The notch 230 is provided to facilitate pushing the first buckle 140 out of the first buckle groove 220 .

[0030] In a specific embodiment, a notch 230 is added to each first buckle groove 220. The notch 230 is located on the side of the top plate 200 away from the box body 100. The notch 230 is connected to the edge of the top plate 200. The side of the notch 230 is arranged so that the first buckle 140 in the first buckle groove 220 is exposed, so as to facilitate the withdrawal of the first buckle 140 from the first buckle groove 220 and then the removal of the top plate 200 from the box body 100.

[0031] like Figure 1 As shown, the box body 100 includes two first side panels 110 and two second side panels 120 . The two first side panels 110 are arranged in parallel and spaced apart, and the two second side panels 120 are arranged in parallel and spaced apart. The first side panels 110 and the second side panels 120 are perpendicular to each other.

[0032] In one specific embodiment, the first side panel 110 and the second side panel 120 are important components that form the sides of the box body 100. Both the first side panel 110 and the second side panel 120 are rectangular panels. The two first side panels 110 are parallel to each other and spaced a certain distance apart. The first side panels 110 primarily support and define the length of the box body 100. Similarly, the two second side panels 120 are also spaced apart and parallel to each other. The second side panels 120 are perpendicular to the first side panels 110 and primarily define the width of the box body 100. This arrangement creates a relatively regular rectangular parallelepiped shape for the box body 100.

[0033] In summary, the parallel, spaced-apart first and second side panels 110, 120 cooperate to form a stable support frame. During transportation, even when subjected to strong jolts, vibrations, and other external forces, the box body 100 maintains its shape and structure, effectively protecting the contents from damage. Furthermore, this structural design facilitates subsequent assembly and maintenance, providing strong support for the widespread use of air boxes.

[0034] like Figure 2 As shown, a plurality of second positioning blocks 111 and a plurality of second buckles 112 are provided on both sides of the first side plate 110 , and the second positioning blocks 111 and the second buckles 112 are alternately arranged in the vertical direction.

[0035] In a specific embodiment, the first side panel 110, as an important component of the box body 100, is provided with a plurality of second positioning blocks 111 and a plurality of second buckles 112 on both sides. The second positioning blocks 111 are rectangular block structures, and their main function is to cooperate with corresponding structures on the second side panel 120 to assist in fixing the first side panel 110 and the second side panel 120. The second buckles 112 are used to engage with corresponding structures on the second side panel 120. The plurality of second positioning blocks 111 and the plurality of second buckles 112 on each side of the first side panel 110 are alternately arranged in the vertical direction. This arrangement makes the connection between the first side panel 110 and the second side panel 120 more stable and uniform.

[0036] In summary, in actual use, stress concentration often causes deformation, wear and other problems in the components of the aviation box connection parts. The design of alternating arrangement of the second positioning blocks 111 and the second clips 112 avoids stress concentration, so that each second positioning block 111 and the second clip 112 can evenly withstand external force, reducing the chance of damage to the components, so that the aviation box can still maintain good performance during long-term use.

[0037] like Figure 3 As shown, a plurality of second through slots 121 and a plurality of second buckle slots 122 are provided on both sides of the second side plate 120 . The second through slots 121 correspond one-to-one to the second positioning blocks 111 , and the second buckle slots 122 correspond one-to-one to the second buckles 112 .

[0038] In a specific embodiment, the second side panel 120, as another important component of the box body 100, is provided with a plurality of second through-slots 121 and a plurality of second buckle slots 122 on both sides. The shape of the second through-slots 121 matches the shape of the second positioning blocks 111, and the number and position of the second through-slots 121 correspond one-to-one with the second positioning blocks 111. When the first side panel 110 and the second side panel 120 are assembled, the second positioning blocks 111 can be accurately inserted into the second through-slots 121, thereby determining the relative position of the first side panel 110 and the second side panel 120. The shape of the second buckle slots 122 matches the shape of the second buckle 112 on the first side panel 110. The purpose of the second buckle slots 122 is to allow the second buckle 112 to be smoothly snapped into them, thereby achieving a snap connection between the first side panel 110 and the second side panel 120.

[0039] In summary, the one-to-one correspondence between the second through groove 121 and the second positioning block 111, and the second buckle groove 122 and the second buckle 112 makes the connection between the first side panel 110 and the second side panel 120 more accurate, avoiding the problem of overall structural instability of the aviation box due to misaligned connection.

[0040] like Figure 5As shown, the box body 100 also includes a bottom plate 300, and a first positioning groove 310 is provided at the edge of the bottom plate 300. The first side plate 110 and the second side plate 120 are respectively provided with a first ridge 113 and a second ridge 123 on the side close to the bottom plate 300, and the first ridge 113 and the second ridge 123 are both inserted into the first positioning groove 310.

[0041] In a specific embodiment, the bottom plate 300 is a component that forms the bottom of the air box and provides bottom support for the items inside the box. The first positioning groove 310 is a groove-like structure arranged around the edge of the bottom plate 300. The first ridge 113 and the second ridge 123 are respectively provided on the side of the first side panel 110 and the second side panel 120 close to the bottom plate 300. The first ridge 113 and the second ridge 123 are both rectangular strip structures. The first ridge 113 protrudes from the lower surface of the first side panel 110, and the second ridge 123 protrudes from the lower surface of the second side panel 120. When assembling the air box, the first ridge 113 and the second ridge 123 on the side of the first side panel 110 and the second side panel 120 close to the bottom plate 300 are respectively inserted into the first positioning groove 310 at the edge of the bottom plate 300. In this way, the box body 100 and the bottom plate 300 are connected.

[0042] like Figure 4 As shown, a second positioning groove is provided on the side of the top plate 200 close to the box body 100, and a third ridge 114 and a fourth ridge 124 are respectively provided on the side of the first side plate 110 and the second side plate 120 close to the top plate 200, and the third ridge 114 and the fourth ridge 124 are both inserted into the second positioning groove.

[0043] In one embodiment, the top panel 200 serves as the top component of the air box. A second positioning groove is provided on the side of the top panel 200 that is adjacent to the box body 100. The second positioning groove surrounds the edge of the top panel 200. A third ridge 114 and a fourth ridge 124 are provided on the side of the first and second side panels 110, 120 that are adjacent to the top panel 200, respectively. The third ridge 114 and the fourth ridge 124 are both rectangular parallelepiped structures. The third ridge 114 protrudes from the upper surface of the first side panel 110, and the fourth ridge 124 protrudes from the upper surface of the second side panel 120. When assembling the air box, the third ridge 114 and the fourth ridge 124 on the side of the first and second side panels 110, 120 that are adjacent to the top panel 200 are respectively inserted into the second positioning groove on the side of the top panel 200 that is adjacent to the box body 100, thereby improving the seal between the box body 100 and the top panel 200.

[0044] like Figure 3 As shown, the first positioning block 130 is located on the fourth protruding strip 124 of the second side plate 120 .

[0045] In one specific embodiment, the first positioning block 130 is located on the fourth ridge 124 of the second side panel 120. When assembling the air box, while the fourth ridge 124 on the side of the second side panel 120 close to the top panel 200 is inserted into the second positioning groove on the side of the top panel 200 close to the box body 100, the first positioning block 130 on the fourth ridge 124 of the second side panel 120 also mates with the first through groove 210 on the top panel 200, thereby more accurately determining the position of the top panel 200. This arrangement allows the top panel 200 to more accurately match the second side panel 120 during installation, ensuring the sealing and stability of the overall structure of the air box.

[0046] like Figure 2 As shown, the first buckle 140 is located on the third protruding strip of the first side panel 110 .

[0047] In one specific embodiment, the first buckle 140 is located on the third ridge of the first side panel 110. When assembling the air box, while inserting the third ridge on the side of the first side panel 110 near the top panel 200 into the second positioning groove at the edge of the top panel 200, the first buckle 140 on the third ridge of the first side panel 110 also engages with the first buckle groove 220 on the top panel 200, thereby completing the fixed connection between the top panel 200 and the box body 100. This arrangement allows the top panel 200 to be more accurately matched with the first side panel 110 during installation, further ensuring the sealing and stability of the overall structure of the air box.

[0048] The above are only preferred embodiments of the present application and do not limit the patent scope of the present application. Any equivalent structure or equivalent process transformation made using the contents of the present application specification and drawings, or directly or indirectly applied in other related technical fields, are also included in the patent protection scope of the present application.

Claims

1. An aviation box, characterized in that: Including: top plate and box body; The box body is a container with a first opening on one side, and a plurality of first positioning blocks and a plurality of first buckles are provided at the first opening. The shape of the top plate matches the shape of the first opening, and a plurality of first through grooves and a plurality of first buckle grooves are provided on the top plate. The first through grooves correspond one-to-one with the first positioning blocks, and the first buckle grooves match the first buckles. The position of the top plate is determined by the cooperation of the first positioning block and the first through groove, and the top plate is fixedly assembled with the box body by the cooperation of the first buckles and the first buckle grooves.

2. The aviation box according to claim 1, characterized in that: A notch is provided at the first buckle slot, and the notch is connected to the edge of the top plate. The provision of the notch facilitates pushing the first buckle out of the first buckle slot.

3. The aviation box according to claim 1, characterized in that: The box body includes two first side panels and two second side panels, the two first side panels are arranged in parallel and spaced apart, the two second side panels are arranged in parallel and spaced apart, and the first side panels are perpendicular to the second side panels.

4. The aviation box according to claim 3, characterized in that: A plurality of second positioning blocks and a plurality of second buckles are provided on both sides of the first side plate, and the second positioning blocks and the second buckles are alternately arranged in the vertical direction.

5. The aviation box according to claim 4, characterized in that: A plurality of second through slots and a plurality of second buckle slots are provided on both sides of the second side plate. The second through slots correspond to the second positioning blocks in a one-to-one manner, and the second buckle slots correspond to the second buckles in a one-to-one manner.

6. The aviation box according to claim 3, characterized in that: The box body also includes a bottom plate, a first positioning groove is provided at the edge of the bottom plate, and the first side plate and the second side plate are respectively provided with a first ridge and a second ridge on one side close to the bottom plate, and the first ridge and the second ridge are both inserted into the first positioning groove.

7. The aviation box according to claim 3, characterized in that: A second positioning groove is provided on the side of the top plate close to the box body, and a third ridge and a fourth ridge are respectively provided on the side of the first side plate and the second side plate close to the top plate. The third ridge and the fourth ridge are both inserted into the second positioning groove.

8. The aviation box according to claim 7, characterized in that: The first positioning block is located on the fourth convex strip of the second side plate.

9. The aviation box according to claim 7, characterized in that: The first buckle is located on the third protruding strip of the first side panel.

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