Aircraft cartridge

Abstract

The utility model discloses an airplane box, which relates to the technical field of paper boxes and comprises a bottom plate and two cover closing structures. According to the technical scheme, the two cover closing structures are symmetrically arranged on the bottom plate, and when the two cover closing structures are manually rotated, the two cover closing structures are opened or closed in the middle area of the bottom plate, so that products packaged by the airplane box can be visually and comprehensively displayed when the airplane box is opened, the display effect of the products is improved, and the practicability of the airplane box is improved. And through the cushioning structure arranged on the cover closing structure and the first edge folding part wrapped by the cover closing structure, the periphery of the product packaged by the airplane box is surrounded, so that the product is protected in a damping mode in the conveying process, the protection effect and quality of the product are improved, and the packaging quality and efficiency of the product are improved.

Description

Technical Field

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

[0002] The airplane box is named because its shape when unfolded resembles an airplane. It is a branch of cardboard and is the first choice for express packaging and delivery. It is made of corrugated paper.

[0003] In the related art, when using airplane boxes to package products, in order to reduce the impact of collisions, falls, etc. on the products, fillers such as foam air bags are generally filled in the airplane boxes. Although this can provide shock-absorbing protection for the products, it reduces the packaging efficiency and increases the packaging cost during the product packaging process. In addition, the filling reduces the aesthetics of the packaged products. Utility Model Content

[0004] The main purpose of the utility model is to provide an airplane box, aiming to improve product packaging efficiency, reduce packaging costs, and improve the aesthetics of product packaging.

[0005] To achieve the above-mentioned purpose, the airplane box proposed by the utility model comprises:

[0006] A bottom plate, wherein two first folded edge portions are arranged opposite to each other;

[0007] Two covering structures, the two covering structures are symmetrically arranged on two opposite sides of the bottom plate, and the bottom plate, the two first folded edge portions and the two covering structures are combined to form a placement space;

[0008] Wherein, a shock absorbing structure is provided in the closing structure, and the closing structure rotates toward the bottom plate and wraps the two first folded edge portions.

[0009] In one embodiment, two opposite side edges of the bottom plate are each provided with a folding groove, and the first folding portion is connected to the folding groove.

[0010] In one embodiment, the shock-absorbing structure includes a first buffer portion and a second buffer portion, the first buffer portion and the second buffer portion are adjacently arranged in the shock-absorbing structure, and are respectively connected to different sides of the closing structure, the first buffer portion and the second buffer portion are in contact with each other, and a shock-absorbing space is set between the second buffer portion and a side of the closing structure.

[0011] In one embodiment, the first buffer portion is provided with a through hole penetrating the first buffer portion, and the second buffer portion is provided with a clamping portion, the clamping portion penetrates the through hole and is clamped and connected with the first buffer portion.

[0012] In one embodiment, the closing structure includes a second folded edge portion and a third folded edge portion, the second folded edge portion is connected to the side of the bottom plate, the third folded edge portion is connected to the side of the second folded edge portion facing away from the bottom plate, the two opposite sides of the third folded edge portion are respectively connected to a fourth folded edge portion and a fifth folded edge portion, and the fourth folded edge portion and the fifth folded edge portion are respectively located on both sides of the second folded edge portion.

[0013] In one embodiment, the side of the fourth folding portion facing away from the third folding portion is connected to the sixth folding portion, the side of the fifth folding portion facing away from the third folding portion is connected to the seventh folding portion, one side of the sixth folding portion is connected to the first buffer portion, and one side of the seventh folding portion is connected to the second buffer portion.

[0014] In one embodiment, the third folded edge portion is bent toward the direction of the second folded edge portion, the fourth folded edge portion and the fifth folded edge portion are both bent toward the direction of the third folded edge portion, the sixth folded edge portion is bent toward the direction of the fourth folded edge portion and contacts the fourth folded edge portion, and the seventh folded edge portion is bent toward the direction of the fifth folded edge portion and contacts the fifth folded edge portion.

[0015] In one embodiment, the fourth folded edge portion, the fifth folded edge portion, the third folded edge portion and the second folded edge portion together form a receiving space, and the first buffer portion and the second buffer portion are both bent toward the receiving space.

[0016] In one embodiment, two opposite sides of the second folded edge portion are respectively connected with an eighth folded edge portion.

[0017] In one embodiment, the eighth folded edge portion is bent toward the second folded edge portion, the eighth folded edge portion is inserted between the sixth folded edge portion and the fourth folded edge portion, and the eighth folded edge portion is inserted between the seventh folded edge portion and the fifth folded edge portion.

[0018] The technical solution of the utility model is to symmetrically arrange two closing structures on the bottom plate. When the two closing structures are manually rotated, the two closing structures are opened or closed in the middle area of ​​the bottom plate, so that the products packaged in the airplane box can be displayed intuitively and comprehensively when the airplane box is opened, thereby improving the display effect of the products. In addition, through the shock-absorbing structure arranged on the closing structure and the first folded edge portion wrapped by the closing structure, the products packaged in the airplane box are surrounded on all sides, so that the products are protected by shock absorption during transportation, thereby improving the protection effect and quality of the products, and improving the packaging quality and efficiency of the products. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on the structures shown in these drawings without paying creative work.

[0020] Figure 1 This is a structural schematic diagram of an embodiment of an aircraft box provided by the utility model;

[0021] Figure 2 This is a schematic diagram of the unfolded structure of an embodiment of the aircraft box provided by the utility model;

[0022] Figure 3 This is a structural schematic diagram of another embodiment of the aircraft box provided by the utility model.

[0023] Description of Figure Numbers:

[0024] 100, airplane box; 10, bottom plate; 20, first folding portion; 30, shock-absorbing structure; 31, snap-fit ​​portion; 32, first buffer portion; 33, sixth folding portion; 34, through hole; 35, seventh folding portion; 36, second buffer portion; 40, lid structure; 41, eighth folding portion; 42, fourth folding portion; 43, third folding portion; 44, second folding portion; 45, fifth folding portion; 50, shock-absorbing space.

[0025] The realization of the purpose, functional features and advantages of the utility model will be further explained in conjunction with embodiments and with reference to the accompanying drawings. DETAILED DESCRIPTION

[0026] 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 of 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.

[0027] It should be noted that if the embodiments of the present invention involve directional indications (such as up, down, left, right, front, back...), the directional indications are only used to explain the relative position relationship, movement status, etc. between the components in a certain specific posture. If the specific posture changes, the directional indications will also change accordingly.

[0028] In addition, if there are descriptions involving "first", "second", etc. in the embodiments of the utility model, the descriptions of "first", "second", etc. are only used for descriptive purposes and cannot be understood as indicating or implying their relative importance or implicitly indicating the number of technical features indicated. Therefore, the features limited to "first" and "second" may explicitly or implicitly include at least one of the features. In addition, if "and / or" or "and / or" appears in the full text, its meaning includes three parallel solutions. Taking "A and / or B" as an example, it includes solution A, solution B, or solutions that satisfy both A and B. In addition, the technical solutions between the various embodiments can be combined with each other, but it must be based on the ability of ordinary technicians in this field to implement. When the combination of technical solutions is contradictory or cannot be implemented, it should be deemed that such combination of technical solutions does not exist and is not within the scope of protection required by the utility model.

[0029] The utility model provides an aircraft box.

[0030] See also Figure 1 In one embodiment of the utility model, the aircraft box comprises:

[0031] A bottom plate 10, wherein two first folding portions 20 are arranged opposite to each other;

[0032] Two covering structures 40, the two covering structures 40 are symmetrically arranged on two opposite sides of the bottom plate 10, and the bottom plate 10, the two first folded edge portions 20 and the two covering structures 40 together form a placement space;

[0033] The cover structure 40 is provided with a shock absorbing structure 30 . The cover structure 40 rotates toward the bottom plate 10 and wraps the two first folded edge portions 20 .

[0034] It can be understood that the two closing structures 40 are symmetrically arranged on both sides of the bottom plate 10, the closing structure 40 rotates around the side of the bottom plate 10, the two first folding portions 20 are bent, and the first folding portions 20 are arranged vertically to the bottom plate 10, and when the closing structure 40 rotates, the closing structure 40 wraps the first folding portion 20.

[0035] It can be understood that when the two closing structures 40 are manually rotated, the two closing structures 40 are opened or closed in the middle area of ​​the bottom plate 10 .

[0036] The technical solution of the utility model is to symmetrically arrange two closing structures 40 on the bottom plate 10. When the two closing structures 40 are manually rotated, the two closing structures 40 are opened or closed in the middle area of ​​the bottom plate 10, so that the products packaged in the airplane box can be displayed intuitively and comprehensively when the airplane box is opened, thereby improving the display effect of the products. In addition, through the shock-absorbing structure 30 arranged on the closing structure 40 and the first folding edge portion 20 wrapped by the closing structure 40, the products packaged in the airplane box are surrounded on all sides, so that the products are protected by shock absorption during transportation, thereby improving the protection effect and quality of the products, and improving the packaging quality and efficiency of the products.

[0037] In one embodiment, two opposite side edges of the bottom plate 10 are provided with folding grooves, and the first folding portion 20 is connected to the folding grooves.

[0038] It can be understood that the first folding portion 20 is arranged in the folding groove. When the first folding portion 20 is bent toward the bottom plate 10, the first folding portion 20 is bent along the groove wall of the folding groove, so that the projection of the first folding portion 20 after bending is located on the plane of the bottom plate 10.

[0039] It is understandable that when the closing structure 40 rotates toward the bottom plate 10 , the closing structure 40 wraps the first folded edge portion 20 , and the closing structure 40 abuts against the bottom plate 10 to ensure the integrity of the edge of the aircraft box 10 after closing.

[0040] In one embodiment, the shock-absorbing structure 30 includes a first buffer portion 32 and a second buffer portion 36, the first buffer portion 32 and the second buffer portion 36 are adjacently arranged in the shock-absorbing structure 30, and are respectively connected to different sides of the closing structure 40, the first buffer portion 32 and the second buffer portion 36 are in contact with each other, and a shock-absorbing space 50 is set between the second buffer portion 36 and a side surface of the closing structure 40.

[0041] like Figure 1 and Figure 3 As shown, the first buffer portion 32 and the second buffer portion 36 are mounted in the cover structure 40 . When the cover structure 40 is closed on the bottom plate 10 , the first buffer portion 32 and the second buffer portion 36 separate the placement space.

[0042] It can be understood that when a product is packaged in the airplane box, the first buffer portion 32 and the second buffer portion 36 on both sides clamp the product to achieve shock-absorbing protection for the left and right sides of the product.

[0043] It should be noted that the first buffer part 32 and the second buffer part 36 are both made of cardboard. The two first buffer parts 32 and the second buffer parts 36 are stacked and connected. When the product contacts the first buffer part 32 or the second buffer part 36, the shock-absorbing space 50 prevents the product from directly hitting the wall of the aircraft box, thereby improving the impact protection quality of the product.

[0044] In one embodiment, the first buffer portion 32 is provided with a through hole 34 penetrating the first buffer portion 32 , and the second buffer portion 36 is provided with a clamping portion 31 , the clamping portion 31 penetrating the through hole 34 and being clamped and connected with the first buffer portion 32 .

[0045] In order to connect the first buffer portion 32 with the second buffer portion 36, the clamping portion 31 is provided on the second buffer portion 36, so that the clamping portion 31 passes through the through hole 34, so that the first buffer portion 32 and the second buffer portion 36 are firmly connected in two layers, thereby preventing the first buffer portion 32 and the second buffer portion 36 from separating and affecting the protection of the product when the product abuts against the first buffer portion 32 and the second buffer portion 36.

[0046] In one embodiment, the closing structure 40 includes a second folded edge portion 44 and a third folded edge portion 43, the second folded edge portion 44 is connected to the side of the bottom plate 10, the third folded edge portion 43 is connected to the side of the second folded edge portion 44 away from the bottom plate 10, and the two opposite sides of the third folded edge portion 43 are respectively connected to the fourth folded edge portion 42 and the fifth folded edge portion 45, and the fourth folded edge portion 42 and the fifth folded edge portion 45 are respectively located on both sides of the second folded edge portion 44.

[0047] like Figure 1 and Figure 2 As shown, when the closing structure 40 is closed on the bottom plate 10, the second folding portion 44 is located on the side of the bottom plate 10, the third folding portion 43 is located on the top side of the bottom plate 10, and the fourth folding portion 42 and the fifth folding portion 45 are respectively located on both sides of the bottom plate 10, so as to facilitate the wrapping of the product placed on the bottom plate 10.

[0048] It can be understood that the two closing structures 40 are rotated so that the two closing structures 40 can be closed on one side of the top surface of the bottom plate 10, thereby completing the rapid packaging of the product.

[0049] It can be understood that when the two closing structures 40 are rotated, the two closing structures 40 are opened and closed at the center of the product, which improves the effect and quality of displaying the product and facilitates the placement and removal of the product.

[0050] In one embodiment, the side of the fourth folded edge portion 42 facing away from the third folded edge portion 43 is connected to the sixth folded edge portion 33, the side of the fifth folded edge portion 45 facing away from the third folded edge portion 43 is connected to the seventh folded edge portion 35, one side of the sixth folded edge portion 33 is connected to the first buffer portion 32, and one side of the seventh folded edge portion 35 is connected to the second buffer portion 36.

[0051] like Figure 1 and Figure 2 As shown, when the sixth folding portion 33 and the seventh folding portion 35 are bent along with the fourth folding portion 42 and the fifth folding portion 45, the first buffer portion 32 and the second buffer portion 35 can be vertically arranged in the accommodation space, and there is a gap between them and the second folding portion 44, so as to achieve shock-absorbing protection for the product.

[0052] In one embodiment, the third folded edge portion 43 is bent toward the second folded edge portion 44, the fourth folded edge portion 42 and the fifth folded edge portion 45 are both bent toward the third folded edge portion 43, the sixth folded edge portion 33 is bent toward the fourth folded edge portion 42 and contacts the fourth folded edge portion 42, and the seventh folded edge portion 35 is bent toward the fifth folded edge portion 45 and contacts the fifth folded edge portion 45.

[0053] It can be understood that the third folded edge portion 43 is bent toward the direction of the second folded edge portion 44, the fourth folded edge portion 42 and the fifth folded edge portion 45 are both bent toward the direction of the third folded edge portion 43, the sixth folded edge portion 33 is bent toward the direction of the fourth folded edge portion 42 and contacts the fourth folded edge portion 42, and the seventh folded edge portion 35 is bent toward the direction of the fifth folded edge portion 45 and contacts the fifth folded edge portion 45, so that when the aircraft box is in an opened state, the bent second folded edge portion 44, the sixth folded edge portion 33, the seventh folded edge portion 35 and the third folded edge portion 43 are combined to form a accommodating space, so that after the closing structure 40 is rotated, it can be buckled on the first folded edge portion 20 to cooperate with the bottom plate 10 to form an aircraft box.

[0054] In one embodiment, the fourth folded edge portion 42 , the fifth folded edge portion 45 , the third folded edge portion 43 and the second folded edge portion 44 together form a receiving space, and the first buffer portion 32 and the second buffer portion 36 are both bent toward the receiving space.

[0055] It can be understood that the first buffer portion 32 and the second buffer portion 36 are bent in the accommodation space to separate the accommodation space so as to separate the product from the wall of the aircraft box and improve the shock-absorbing effect on the product.

[0056] In one embodiment, two opposite sides of the second folded edge portion 44 are respectively connected to the eighth folded edge portion 41 .

[0057] In order to enhance the shock-absorbing effect on the front and rear sides of the product, the first folded edge portion 20 is provided on both the front and rear sides of the product, and the sixth folded edge portion 33, the fourth folded edge portion 42, the eighth folded edge portion 41, the fifth folded edge portion 45 and the seventh folded edge portion 35 that wrap the first folded edge portion 20 after the covering structure 40 is closed, thereby enhancing the protection effect on the front and rear sides of the product.

[0058] In one embodiment, the eighth folded edge portion 41 is bent toward the second folded edge portion 44 , the eighth folded edge portion 41 is inserted between the sixth folded edge portion 33 and the fourth folded edge portion 42 , and the eighth folded edge portion 41 is inserted between the seventh folded edge portion 35 and the fifth folded edge portion 45 .

[0059] It can be understood that by inserting the eighth folded edge portion 41 between the sixth folded edge portion 33 and the fourth folded edge portion 42, and inserting the eighth folded edge portion 41 between the seventh folded edge portion 35 and the fifth folded edge portion 45, the eighth folded edge portion 41 is fixed, and when the closing structure 40 is closed, the shock-absorbing effect on the front and rear sides of the product is enhanced, thereby improving the protection effect and quality of the product.

[0060] The above description is only an exemplary embodiment of the present invention, and does not limit the patent scope of the present invention. All equivalent structural changes made by using the contents of the present invention specification and drawings under the technical concept of the present invention, or directly / indirectly applied in other related technical fields are included in the patent protection scope of the present invention.

Claims

1. An aircraft box, characterized in that: include: A bottom plate, wherein two first folded edge portions are arranged opposite to each other; Two covering structures, the two covering structures are symmetrically arranged on two opposite sides of the bottom plate, and the bottom plate, the two first folded edge portions and the two covering structures are combined to form a placement space; Wherein, a shock absorbing structure is provided in the closing structure, and the closing structure rotates toward the bottom plate and wraps the two first folded edge portions.

2. The aircraft box according to claim 1, characterized in that: Two opposite side edges of the bottom plate are each provided with a folding groove, and the first folding portion is connected in the folding groove.

3. The aircraft box according to claim 2, characterized in that: The shock-absorbing structure includes a first buffer portion and a second buffer portion. The first buffer portion and the second buffer portion are adjacently arranged in the shock-absorbing structure and are respectively connected to different sides of the covering structure. The first buffer portion and the second buffer portion are in contact with each other, and a shock-absorbing space is arranged between the second buffer portion and a side of the covering structure.

4. The aircraft box according to claim 3, characterized in that: The first buffer portion is provided with a through hole penetrating the first buffer portion, and the second buffer portion is provided with a clamping portion, which penetrates the through hole and is clamped and connected with the first buffer portion.

5. The aircraft box according to claim 3, characterized in that: The closing structure includes a second folding edge portion and a third folding edge portion, the second folding edge portion is connected to the side of the bottom plate, the third folding edge portion is connected to the side of the second folding edge portion facing away from the bottom plate, the two opposite sides of the third folding edge portion are respectively connected to the fourth folding edge portion and the fifth folding edge portion, and the fourth folding edge portion and the fifth folding edge portion are respectively located on both sides of the second folding edge portion.

6. The aircraft box according to claim 5, characterized in that: The side of the fourth folding portion facing away from the third folding portion is connected to the sixth folding portion, the side of the fifth folding portion facing away from the third folding portion is connected to the seventh folding portion, one side of the sixth folding portion is connected to the first buffer portion, and one side of the seventh folding portion is connected to the second buffer portion.

7. The aircraft box according to claim 6, characterized in that: The third folded edge portion is bent toward the direction of the second folded edge portion, the fourth folded edge portion and the fifth folded edge portion are both bent toward the direction of the third folded edge portion, the sixth folded edge portion is bent toward the direction of the fourth folded edge portion and contacts the fourth folded edge portion, and the seventh folded edge portion is bent toward the direction of the fifth folded edge portion and contacts the fifth folded edge portion.

8. The aircraft box according to claim 7, characterized in that: The fourth folded edge portion, the fifth folded edge portion, the third folded edge portion and the second folded edge portion together form a receiving space, and the first buffer portion and the second buffer portion are both bent toward the receiving space.

9. The aircraft box according to claim 6, characterized in that: Two opposite sides of the second folded edge portion are respectively connected with the eighth folded edge portion.

10. The aircraft box according to claim 9, characterized in that: The eighth folded edge portion is bent toward the direction of the second folded edge portion, the eighth folded edge portion is inserted between the sixth folded edge portion and the fourth folded edge portion, and the eighth folded edge portion is inserted between the seventh folded edge portion and the fifth folded edge portion.

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