Aviation case

Abstract

The utility model discloses an aviation case which comprises a case body, a case cover is hinged to the top of the case body through a hinge, a bottom plate is arranged at the bottom of the case body, the case body comprises two sets of first side plates arranged oppositely and two sets of second side plates arranged oppositely, and the two sets of first side plates and the two sets of second side plates are connected in a clamped mode through clamping assemblies. The buckles on the two sides of the two sets of first side plates are inserted into the clamping grooves in the two sides of the adjacent second side plates respectively, after the buckles are inserted into the clamping grooves, the two sets of first side plates are moved upwards, the two sets of first side plates can drive the buckles on the two sides to move in the clamping grooves, the buckles move from the large openings in the clamping grooves to the small openings in the clamping grooves, and therefore the buckles can be clamped in the clamping grooves. And the two groups of first side plates and the two groups of second side plates are buckled and fixed through the buckles and the clamping grooves, so that the assembly is relatively convenient and rapid, the problem that a plurality of groups of screws need to be screwed is avoided, and the assembly efficiency of the aviation case is greatly improved.

Description

Technical Field

[0001] The utility model belongs to the technical field of aviation boxes, and in particular relates to an aviation box. Background Art

[0002] Traditional simple wooden box packaging and transportation cannot provide effective protection for electronic products during long-distance transportation. In order to ensure that electronic products are not damaged during transportation, aviation boxes are used for packaging to prevent damage to electronic products due to bumps.

[0003] In the existing production and assembly process of aviation boxes, screws are generally used to fix them. During assembly, two sets of box panels are aligned and the screws on the surfaces of the box panels are tightened one by one, which results in a long operation time and low efficiency when assembling the aviation box. In particular, the larger the volume of the aviation box is, the more screws need to be tightened, which makes it difficult to assemble the aviation box, resulting in a long time spent on assembling the aviation box, which greatly reduces the assembly efficiency of the aviation box. Utility Model Content

[0004] The purpose of the utility model is to provide an aviation box to solve the problems raised in the above background technology.

[0005] To achieve the above purpose, the utility model provides the following technical solution: an aviation box, comprising:

[0006] A box body, wherein the top of the box body is hinged with a box cover via a hinge, the bottom of the box body is provided with a bottom plate and the bottom of the bottom plate is provided with a plurality of casters, the box body comprises two groups of first side plates arranged opposite to each other and two groups of second side plates arranged opposite to each other, the two groups of first side plates and the two groups of second side plates are clamped together via a clamping assembly, and the buckle of the clamping assembly is clamped together with the clamping groove on the surface of the adjacent second side plate, so that the first side plate and the second side plate are clamped and fixed.

[0007] Preferably, the snap-fit ​​assembly includes a plurality of bottom buckles, the buckles are provided in a plurality of groups and are evenly distributed on both sides of the first side panel, the plurality of bottom buckles are evenly distributed at the bottom of the first side panel, and the card slots are provided in a plurality of groups and are evenly distributed on both sides of the second side panel.

[0008] Preferably, the buckle and the bottom buckle are both arranged in a T-shape, and the slot is arranged in a shape of being larger at the bottom and smaller at the top.

[0009] Preferably, a plurality of inserts are provided at the bottom of the second side panel, button holes are evenly distributed on the surface of the bottom panel and at the bottom of the first side panel, slots are evenly distributed on the surface of the bottom panel and at the bottom of the second side panel, the bottom buttons cooperate with the button holes for insertion, the inserts are inserted into the slots, and screws are passed through the through holes on the surface of the inserts and then screwed together with the threaded grooves provided in the bottom panel.

[0010] Preferably, two sides of the tops of adjacent first side panels and second side panels are connected by a connecting plate.

[0011] Preferably, one end of the hinge is connected to one of the first side panels, and the other end is connected to the box cover. A handle is provided in the middle of the surface of the second side panel. Two groups of inner liners are provided in the box body. The handles on the surfaces of the two groups of second side panels facilitate the box body to be lifted and moved by two hands.

[0012] Compared with the prior art, the utility model has the following beneficial effects: during assembly, the buckles on both sides of the two groups of first side panels are respectively inserted into the slots on both sides of the adjacent second side panels; after the buckles are inserted into the slots, the two groups of first side panels are moved upward, and the two groups of first side panels drive the buckles on both sides to move in the slots, so that the buckles move from the larger opening in the slots to the smaller opening in the slots, thereby achieving buckle fixation between the buckles and the slots; and after the two groups of first side panels and the two groups of second side panels are assembled, the four groups of connecting plates are riveted to the four corner connections of the first side panels and the second side panels by rivets, thereby strengthening the connection between the two groups of first side panels and the two groups of second side panels. Stability, and then correctly insert the bottom buckles of the two groups of first side panels into the buckle holes on the surface of the bottom panel respectively. When the bottom buckles are inserted into the buckle holes, the insert pieces at the bottom of the second side panel are inserted into the slots, and screws are passed through the through holes on the surface of the insert pieces and screwed to the threaded grooves in the bottom panel, so that the bottom panel is fixed to the first side panel and the bottom of the second side panel, and connected with the box cover and the first side panel through the two sets of leaves, so as to realize the hinge connection between the box cover and the box body, and the two groups of first side panels and the two groups of second side panels are fixed by buckles and slots, which makes the assembly more convenient and quick, avoids the problem of screwing multiple sets of screws, and greatly improves the assembly efficiency of the aviation box. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic diagram of the structure of the utility model;

[0014] Figure 2 It is an exploded view of the utility model;

[0015] Figure 3 This is a schematic diagram of the structure of the second side plate of the utility model;

[0016] Figure 4 It is a structural schematic diagram of the bottom plate of the utility model.

[0017] In the figure: 1. box body; 2. hinge; 3. box cover; 4. bottom plate; 5. casters; 6. first side panel; 7. second side panel; 8. buckle; 9. slot; 10. bottom buckle; 11. insert; 12. buckle hole; 13. slot; 14. connecting plate; 15. handle; 16. liner; 17. threaded groove. DETAILED DESCRIPTION

[0018] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0019] The utility model provides Figure 1-4 A flight case shown includes:

[0020] A box body 1, wherein a box cover 3 is hingedly connected to the top of the box body 1 by a hinge 2, a bottom plate 4 is provided at the bottom of the box body 1 and a plurality of casters 5 are provided at the bottom of the bottom plate 4, the box body 1 comprises two groups of first side panels 6 arranged opposite to each other and two groups of second side panels 7 arranged opposite to each other, the two groups of first side panels 6 and the two groups of second side panels 7 are clamped together by a clamping assembly, and the buckle 8 of the clamping assembly is clamped together with the clamping groove 9 on the surface of the adjacent second side panel 7, so that the first side panel 6 and the second side panel 7 are clamped and fixed.

[0021] The snap-on assembly includes a plurality of bottom buckles 10 , the buckles 8 are provided in a plurality of groups and are evenly distributed on both sides of the first side plate 6 , the plurality of bottom buckles 10 are evenly distributed at the bottom of the first side plate 6 , and the card slots 9 are provided in a plurality of groups and are evenly distributed on both sides of the second side plate 7 .

[0022] The buckle 8 and the bottom buckle 10 are both arranged in a T shape, and the slot 9 is arranged in a shape of being larger at the bottom and smaller at the top.

[0023] A plurality of inserts 11 are provided at the bottom of the second side panel 7, buckle holes 12 are evenly distributed on the surface of the bottom panel 4 and at the bottom of the first side panel 6, slots 13 are evenly distributed on the surface of the bottom panel 4 and at the bottom of the second side panel 7, the bottom buckles 10 are matched with the buckle holes 12 for plugging, and after the inserts 11 are inserted into the slots 13, the screws penetrate through the through holes on the surface of the inserts 11 and are screwed to the threaded grooves 17 provided in the bottom panel 4.

[0024] The tops of the adjacent first side panels 6 and second side panels 7 are connected by connecting plates 14 on both sides, and four groups of connecting plates 14 are riveted to the four corner connections of the first side panels 6 and the second side panels 7 by rivets, thereby enhancing the stability of the connection between the two groups of first side panels 6 and the two groups of second side panels 7.

[0025] One end of the hinge 2 is connected to one of the first side panels 6, and the other end is connected to the box cover 3. A handle 15 is provided in the middle of the surface of the second side panel 7. Two groups of inner liners 16 are provided in the box body 1. The box cover 3 connected by the hinge 2 can be flipped open so that things to be stored can be placed in the inner liners 16.

[0026] When assembling the aviation box, the buckles 8 on both sides of the two groups of first side panels 6 are respectively inserted into the slots 9 on both sides of the adjacent second side panels 7. After the buckles 8 are inserted into the slots 9, the two groups of first side panels 6 are moved upward, and the two groups of first side panels 6 will drive the buckles 8 on both sides to move in the slots 9, so that the buckles 8 move from the larger opening in the slots 9 to the smaller opening in the slots 9, so that the buckles 8 are fixed to the slots 9. After the two groups of first side panels 6 and the two groups of second side panels 7 are assembled, the four groups of connecting plates 14 are riveted to the four corner connections of the first side panels 6 and the second side panels 7 by rivets, so as to enhance the stability of the connection between the two groups of first side panels 6 and the two groups of second side panels 7, and then the two groups are respectively The bottom buckle 10 at the bottom of the first side panel 6 is correctly inserted into the buckle hole 12 on the surface of the bottom panel 4. When the bottom buckle 10 is inserted into the buckle hole 12, the insert piece 11 at the bottom of the second side panel 7 is inserted into the slot 13, and the screw passes through the through hole on the surface of the insert piece 11 and is screwed to the threaded groove 17 provided in the bottom panel 4, so that the bottom panel 4 is fixed to the bottom of the first side panel 6 and the second side panel 7, and is connected to the box cover 3 and the first side panel 6 through two sets of leaves 2, so as to realize the hinge connection between the box cover 3 and the box body 1, and the two sets of first side panels 6 and the two sets of second side panels 7 are fixed by the buckle 8 between the buckle 8 and the slot 9, so that the assembly is more convenient and quick, avoiding the problem of needing to screw multiple sets of screws, and greatly improving the assembly efficiency of the aviation box.

[0027] Finally, it should be noted that the above is only a preferred embodiment of the present invention and is not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments or make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. An aviation box, characterized in that: include: A box body (1), wherein the top of the box body (1) is hingedly connected to a box cover (3) via a hinge (2), the bottom of the box body (1) is provided with a bottom plate (4), and the bottom of the bottom plate (4) is provided with a plurality of casters (5), the box body (1) comprises two groups of first side plates (6) arranged opposite to each other and two groups of second side plates (7) arranged opposite to each other, the two groups of first side plates (6) and the two groups of second side plates (7) are clamped together via a clamping assembly, and the buckle (8) of the clamping assembly is clamped together with a clamping groove (9) on the surface of an adjacent second side plate (7), so that the first side plate (6) and the second side plate (7) are clamped and fixed.

2. An aviation box according to claim 1, characterized in that: The snap-fit ​​assembly comprises a plurality of bottom buckles (10), the buckles (8) are provided in a plurality of groups and are evenly distributed on both sides of the first side plate (6), the plurality of bottom buckles (10) are evenly distributed on the bottom of the first side plate (6), and the clamping slots (9) are provided in a plurality of groups and are evenly distributed on both sides of the second side plate (7).

3. An aviation box according to claim 2, characterized in that: The buckle (8) and the bottom buckle (10) are both arranged in a T-shape, and the slot (9) is arranged in a shape that is larger at the bottom and smaller at the top.

4. The aviation box according to claim 2, characterized in that: A plurality of inserting pieces (11) are provided at the bottom of the second side plate (7); buckle holes (12) are evenly distributed on the surface of the bottom plate (4) and located at the bottom of the first side plate (6); slots (13) are evenly distributed on the surface of the bottom plate (4) and located at the bottom of the second side plate (7); the bottom buckles (10) are matched and plugged into the buckle holes (12); after the inserting pieces (11) are inserted into the slots (13), screws are passed through the through holes on the surface of the inserting pieces (11) and then screwed into the threaded grooves (17) provided in the bottom plate (4).

5. The aviation box according to claim 1, characterized in that: The top sides of the adjacent first side panels (6) and second side panels (7) are connected via a connecting plate (14).

6. The aviation box according to claim 1, characterized in that: One end of the hinge (2) is connected to one of the first side panels (6), and the other end is connected to the box cover (3). A handle (15) is provided in the middle of the surface of the second side panel (7). Two groups of inner containers (16) are provided in the box body (1).

Images