CN215623312U - Double-box-cover aircraft box - Google Patents

Abstract

The utility model relates to the technical field of packaging boxes, and particularly discloses a double-box-cover aircraft box which comprises a bottom plate, wherein the left side and the right side of the bottom plate are connected with folding side plates, and the folding side plates can be folded along the middle part; the upper side and the lower side of the bottom plate are connected with an upper side plate and a lower side plate, the outer sides of the upper side plate and the lower side plate are both connected with an upper box cover, one upper box cover is provided with a connecting buckle, and the other upper box cover is provided with a connecting port clamped with the connecting port; the edges of the left side and the right side of the upper box covers are also provided with safety buckles, and the folding side plates arranged on the left side and the right side of the bottom plate can improve the structural strength of the whole box body and have high-strength pressure resistance; the upper box cover with a double-layer structure is molded and has more obvious three-dimensional effect after patterns are printed; the connecting structures such as the safety buckle and the connecting buckle are added to ensure that the box body has high-strength pressure resistance; and is more material efficient than existing aircraft box models at comparable sizes.

Description

Double-box-cover aircraft box

Technical Field

The utility model relates to the technical field of packaging boxes, in particular to a double-box-cover aircraft box.

Background

With the development of the logistics industry and the internet business, the packaging structure and the packaging products have long-term and large-scale application in various fields of production and life, and the packaging box structure is required to be used for more and more products. With respect to the package structure, the end use of the package structure is often the individual user of the terminal. Therefore, users often put higher and higher requirements on the performance, the use convenience and the like of the packing box; the widely used aircraft box at present is named as an aircraft because of the expansion appearance, belongs to a branch of a paper box, is a first choice for express packaging and delivery, and is made of corrugated paper; the airplane box in the prior art has lower structural strength, low aesthetic degree and high production and use cost in use.

SUMMERY OF THE UTILITY MODEL

Aiming at the defects in the prior art, the utility model aims to provide a double-box-cover aircraft box which is convenient to use, high in aesthetic degree and capable of improving the structural strength of the aircraft box.

The technical scheme adopted by the utility model is as follows: a double-box-cover airplane box comprises a bottom plate, wherein folding side plates are connected to the left side and the right side of the bottom plate, and can be folded along the middle part to form an inner side plate and an outer side plate which are arranged from inside to outside; the upper side and the lower side of the bottom plate are connected with an upper side plate and a lower side plate, the outer sides of the upper side plate and the lower side plate are both connected with an upper box cover, one upper box cover is provided with a connecting buckle, and the other upper box cover is provided with a connecting port clamped with the connecting port; two the both sides edge still is equipped with the safety catch about the upper box lid, each the safety catch can corresponding card go into locate folding curb plate middle part safety mouth of folding department in.

In the technical scheme; the folding side plates positioned at the left side and the right side of the bottom plate can be folded along the middle part thereof to form double-layer side plates, the structural strength of the whole box body can be improved under the double-layer supporting action of the inner side plates and the outer side plates, and the box body has high-strength compression resistance; the upper side plate and the lower side plate which are positioned at the upper side and the lower side of the bottom plate can be folded to form a side plate structure, and an upper box cover connected with the upper side plate and the lower side plate is used for closing the box body; the upper box cover can form a double-layer box cover structure, and the upper box cover adopting the double-layer structure has more obvious three-dimensional effect after being molded and printed with patterns, and is more novel. The connecting ports and the connecting buckles on the two upper box covers can be mutually clamped, so that the stability of the closed box body is improved; in addition, the safety buckles positioned at the two sides of the upper box cover can be clamped into the safety openings of the folding side plates, so that the structural strength of the closed box body is further improved; after the structure is adopted, materials are saved more than that of the existing airplane box type under the same-proportion size, and the connection structures such as the safety buckle and the connecting buckle are added to ensure that the box body has high-strength pressure resistance; the production simplicity, high efficiency and other excellent functions of the airplane box are enhanced.

Further, one side that bottom plate and folding curb plate link to each other is equipped with the folding bayonet socket of interval arrangement, folding curb plate keeps away from bottom plate one side and is equipped with the folding fixed part of interval arrangement, folding fixed part can block into in the corresponding folding bayonet socket.

Furthermore, the outer edge of the upper box cover provided with the safety opening is provided with an expanding part which is arranged in an arc shape.

Furthermore, the left side and the right side of the upper side plate and the lower side plate are connected with folded edges, and the width of each folded edge is matched with the width of the upper measuring plate and the width of the lower side plate.

Furthermore, folding ears are arranged on the left side and the right side of the upper box cover.

Further, the folding side plates are provided with folding marks along the middle parts thereof.

The utility model has the beneficial effects that: the folding side plates arranged on the left side and the right side of the bottom plate of the double-box-cover aircraft box provided by the utility model can be folded along the middle part of the bottom plate to form double-layer side plates, so that the structural strength of the whole box body can be improved under the double-layer supporting effect, and the double-box-cover aircraft box has high-strength compression resistance; the upper box cover connected with the upper side plate and the lower side plate can form a double-layer box cover structure, and the double-layer upper box cover has a more obvious three-dimensional effect and is more novel after being molded and printed with patterns; the connecting structures such as the safety buckle and the connecting buckle are added to ensure that the box body has high-strength pressure resistance; the production simplicity, high efficiency and other excellent functions of the airplane box are enhanced, and materials are saved under the same-proportion size compared with the existing airplane box type: the high-efficiency production and sustainability are realized by combining the existing machinery and production process in the market; has higher practical value and popularization value.

Drawings

In order to more clearly illustrate the detailed description of the utility model or the technical solutions in the prior art, the drawings that are needed in the detailed description of the utility model or the prior art will be briefly described below. Throughout the drawings, like elements or portions are generally identified by like reference numerals. In the drawings, elements or portions are not necessarily drawn to scale.

Fig. 1 is a block diagram 1 of a dual-deck aircraft box according to an embodiment of the present invention.

Fig. 2 is a block diagram 2 of a dual-deck aircraft box according to an embodiment of the present invention.

Fig. 3 is a block diagram 3 of a dual-deck aircraft box according to an embodiment of the present invention.

Reference numerals: the folding box comprises a bottom plate 100, a folding side plate 200, a safety opening 210, a folding bayonet 220, a folding fixing part 230, a folding trace 240, an upper side plate 300, a lower side plate 400, an upper box cover 500, a connecting buckle 510, a connecting opening 520, a safety buckle 530, an unfolding part 540, a folding edge 600 and a folding ear 700.

Detailed Description

Embodiments of the present invention will be described in detail below with reference to the accompanying drawings. The following examples are only for illustrating the technical solutions of the present invention more clearly, and therefore are only examples, and the protection scope of the present invention is not limited thereby.

It is to be noted that, unless otherwise specified, technical or scientific terms used herein shall have the ordinary meaning as understood by those skilled in the art to which the utility model pertains.

As shown in fig. 1 to 3, embodiments of the present invention provide a double-deck aircraft box that can significantly increase structural strength; the folding type folding bed comprises a bottom plate 100, wherein folding side plates 200 are connected to the left side and the right side of the bottom plate 100, and the folding side plates 200 can be folded along the middle part to form an inner side plate and an outer side plate which are arranged from inside to outside; the upper side plate 300 and the lower side plate 400 are connected to the upper side and the lower side of the bottom plate 100, the outer sides of the upper side plate 300 and the lower side plate 400 are both connected with an upper box cover 500, one upper box cover 500 is provided with a connecting buckle 510, and the other upper box cover 500 is provided with a connecting port 520 clamped with the connecting port 520; the left and right edges of the upper box cover 500 are further provided with safety buckles 530, and each safety buckle 530 can be correspondingly clamped into the safety opening 210 at the middle folding position of the folding side plate 200.

In the present embodiment; the folding side plates 200 positioned at the left side and the right side of the bottom plate 100 can be folded along the middle part thereof to form double-layer side plates, the structural strength of the whole box body can be improved under the double-layer supporting action of the inner side plates and the outer side plates, and the box body has high-strength and pressure-resistant performance; the upper and lower side plates 300 and 400 positioned at the upper and lower sides of the bottom plate 100 can be folded to form a side plate structure, and the upper box cover 500 connected with the upper and lower side plates 300 and 400 is used to open or close the box body; because the upper box cover 500 can form a double-layer box cover structure, the box body has obvious three-dimensional effect after being formed and printed with patterns, and is more novel. The connecting ports 520 and the connecting buckles 510 on the two upper box covers 500 can be mutually clamped, so that the stability of the closed box body is improved; in addition, the safety catches 530 located at the two sides of the upper box cover 500 can be clamped into the safety openings 210 of the folding side plates 200, so that the structural strength of the closed box body is further improved; after the structure is adopted, materials are saved more than that of the existing airplane box type under the same-proportion size, and the connection structures such as the safety buckle 530, the connection buckle 510 and the like are added to ensure that the box body has high-strength pressure resistance; the production simplicity, high efficiency and other excellent functions of the airplane box are enhanced. In this embodiment, the connecting buckle 510 is arranged in a heart shape, which improves the aesthetic property and the interest of the box body; the corresponding shape can also be adopted according to the requirement in the production application.

As mentioned above, the folding side plate 200 can be folded along the middle portion thereof to form a double-layer side plate structure of the inner side plate and the outer side plate, in order to improve the stability of the folding side plate 200 after folding, the embodiment is provided with the folding bayonets 220 arranged at intervals on the side where the bottom plate 100 is connected with the folding side plate 200, the folding side plate 200 is provided with the folding fixing portions 230 arranged at intervals on the side away from the bottom plate 100, and the folding fixing portions 230 can be snapped into the corresponding one of the folding bayonets 220. Thus, when the folding side plate 200 is folded along the middle portion, the folding fixing portion 230 on the outer side plate at the outer side can be clamped into the folding bayonet 220, so as to prevent the folding side plate 200 from unfolding after folding; in order to facilitate folding, the present embodiment further provides folding marks 240 along the middle of the folding side panel 200, and these marks can ensure that the outer side panel and the inner side panel are more closely fitted.

As shown in fig. 1 to 3, after the body of the airplane box is closed, the two upper box covers 500 are attached to each other in a manner of attaching up and down, so as to ensure that the safety catch 530 is locked in the corresponding safety opening 210; the upper case cover 500 provided with the safety catch 530 is located below the upper case cover 500 provided with the safety opening 210, so that the safety catch 530 upwardly passes through the safety opening 210 to facilitate the user to open the case body, and in this embodiment, the outer edge of the upper case cover 500 provided with the safety opening 210 is provided with an expanding portion 540 in an arc shape. Thus, when the airplane case is opened, the upper case cover 500 may be unfolded by the unfolding part 540; the convenience of box body equipment is improved.

As shown in fig. 1 to 3, after the aircraft box is assembled, the folding side plate 200, the upper side plate 300 and the lower side plate 400 form the outer side surface of the aircraft box, and in order to improve the stability of the upper side plate 300 and the lower side plate 400, in the present embodiment, the left and right sides of the upper side plate 300 and the lower side plate 400 are connected with the folding edges 600, and the width of the folding edges 600 is adapted to the width of the upper side plate and the lower side plate 400. Thus, the folded edge 600 can be clamped between the outer side plate and the inner side plate, and the pressure resistance of the airplane box is improved. In addition, the present embodiment further includes folding ears 700 at the left and right sides of the upper case cover 500. Thus, after the airplane box is sealed by the upper box cover 500, the folding ears 700 can be attached to the inner side surface of the inner side plate, and the structural strength of the airplane box is improved.

Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the utility model has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention, and they should be construed as being included in the following claims and description.

Claims (6)

1. A dual-deck aircraft box comprising a base plate (100), characterized in that;

the left side and the right side of the bottom plate (100) are connected with folding side plates (200), and the folding side plates (200) can be folded along the middle part to form an inner side plate and an outer side plate which are arranged from inside to outside;

the upper side plate (300) and the lower side plate (400) are connected to the upper side and the lower side of the bottom plate (100), the outer sides of the upper side plate (300) and the lower side plate (400) are respectively connected with an upper box cover (500), one upper box cover (500) is provided with a connecting buckle (510), and the other upper box cover (500) is provided with a connecting port (520) clamped with the connecting port (520); two safety buckles (530) are further arranged on the edges of the left side and the right side of the upper box cover (500), and each safety buckle (530) can be correspondingly clamped into a safety opening (210) formed in the middle folding position of the folding side plate (200).

2. The dual-deck aircraft box of claim 1, wherein; one side that bottom plate (100) and folding curb plate (200) link to each other is equipped with folding bayonet socket (220) of interval arrangement, folding curb plate (200) are kept away from bottom plate (100) one side and are equipped with folding fixed part (230) of interval arrangement, folding fixed part (230) can be gone into in corresponding folding bayonet socket (220) in can blocking.

3. The dual-deck aircraft box of claim 1, wherein; the outer side edge of the upper box cover (500) provided with the safety opening (210) is provided with an expanding part (540) which is arranged in an arc shape.

4. The dual-deck aircraft box of claim 1, wherein; the left and right sides of the upper side plate (300) and the lower side plate (400) are connected with folded edges (600), and the width of each folded edge (600) is matched with the width of the upper measuring plate and the width of the lower side plate (400).

5. The dual-deck aircraft box of claim 1, wherein; folding ears (700) are arranged on the left side and the right side of the upper box cover (500).

6. The dual-deck aircraft box of claim 1, wherein; the folding side plate (200) is provided with a folding mark (240) along the middle part.

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