CN215437328U

CN215437328U - Airplane box with fixing device

Info

Publication number: CN215437328U
Application number: CN202023070142.5U
Authority: CN
Inventors: 李祖文; 杨剑飞; 李楠
Original assignee: People's Printing Plant Of Guangzhou Co ltd
Current assignee: People's Printing Plant Of Guangzhou Co ltd
Priority date: 2020-12-18
Filing date: 2020-12-18
Publication date: 2022-01-07
Anticipated expiration: 2030-12-18

Abstract

The utility model relates to an airplane box with a fixing device, wherein one ends of a left body plate and a right body plate, which are far away from a box bottom plate, are connected with an inner side plate in a folding mode, the inner side plate is respectively connected with the left body plate and the right body plate through wide crease marks, the inner side plate can be respectively folded inwards around the wide crease marks, an insertion space is formed between the inner side plate and the left body plate and between the inner side plate and the right body plate, the left side and the right side of the front body plate and the rear body plate are respectively provided with a flap piece capable of being inserted into the insertion space, when the front body plate, the rear body plate, the right body plate and the left body plate are vertically folded relative to the box bottom plate, the flap piece can be inserted into the insertion space to form a box-shaped structure, the airplane box-shaped airplane box also comprises a cover plate component arranged on one side of the box bottom plate based on the principle of the rear body plate and a fixing device arranged in the box and used for fixing a loading object, and the airplane box can form the insertion space through the folding structure, so that a jack can be easily inserted into the airplane box, the multilayer structure increases the stability and the pressure resistance of the airplane box.

Description

Airplane box with fixing device

Technical Field

The utility model relates to the technical field of folding boxes, in particular to an airplane box with a fixing device.

Background

The airplane box is named as an airplane due to the fact that the unfolded appearance of the airplane box is similar to that of an airplane, belongs to a branch of a paper box, and is the first choice for express packaging and delivery.

With the increasing development of the internet, the threshold is low, the individual households and small merchants of the online stores also rise with water, and how to avoid the abrasion of goods in the delivery process is a problem which needs to be considered. In addition, information such as a shop name address can be printed, so that the recognition degree of a customer on a brand can be improved, and the viscosity of the customer is increased. But to some breakable products, the performance of the abrasionproof of independent aircraft box decreases anticollision still has to be improved, current aircraft box on the market generally is made by the corrugated paper, generally there are three-layer and five-layer branch, the inconvenient inserting of socket in front when folding of structure of current aircraft box is gone into, and stability is slightly poor, compressive capacity is poor, some inside aircraft boxes that are provided with fixing device and are used for placing breakable product (like the beverage bottle) at present, fixing device generally is split type installation inside aircraft box, its unstable structure, lead to the buffering protective properties poor.

SUMMERY OF THE UTILITY MODEL

The utility model aims to solve the technical defects that a front socket is inconvenient to insert when the structure of the aircraft box in the prior art is folded, the stability is poor, the pressure resistance is poor, and the structure of a fixing device is unstable, so that the buffer protection performance is poor.

In order to solve the technical problems, the technical scheme adopted by the utility model is as follows:

the airplane box with the fixing device comprises a box bottom plate, a front body plate, a rear body plate, a right body plate and a left body plate, wherein the front body plate, the rear body plate, the right body plate and the left body plate are respectively connected to four side edges of the box bottom plate in a foldable manner, one ends of the left body plate and the right body plate, which are far away from the box bottom plate, are connected with the inner side plate in a foldable manner, the inner side plate is respectively connected with the left body plate and the right body plate through wide-grain creases, the inner side plate can be respectively folded inwards around the wide-grain creases, an insertion space is formed between the inner side plate and the left body plate and between the inner side plate and the right body plate, the left side and the right side of the front body plate and the rear body plate are respectively provided with a flap piece capable of being inserted into the insertion space, when the front body plate, the rear body plate, the right body plate and the left body plate are vertically folded relative to the box bottom plate, the flap piece can be inserted into the insertion space to form a box-shaped structure, and a cover plate assembly arranged on one side of the box bottom plate of the rear body plate, and a fixing device provided in the box for fixing the load.

Further, the fixing device comprises an inner lining plate and height side plates which are connected to four side plates of the inner lining plate in a foldable mode, the height side plates can be vertically folded relative to the inner lining plate to form supporting legs for supporting the inner lining plate, and through holes for fixing loads are formed in the inner lining plate.

Further, the loading article is a cup, and the through hole can be correspondingly arranged according to the structure of the cup.

Furthermore, the cover plate assembly comprises an upper cover plate connected with the rear body plate in a folding and pressing mode, two sides of the upper cover plate are connected with side plates in a folding and pressing mode, the side plates can be vertically folded and inserted into the airplane box relative to the upper cover plate to form covering, one side, far away from the rear body plate, of the upper cover plate is connected with a fixing plate in a folding and pressing mode, two sides of the fixing plate are connected with inserting tongues in a folding and pressing mode, the inserting tongues can be vertically folded relative to the fixing plate, and when the upper cover plate is in a covering and pressing mode, the inserting tongues can be inserted into the inserting space to fix the upper cover plate.

Further, the insertion tongue is provided in an elliptical shape to facilitate insertion into the insertion space.

Furthermore, bayonets are arranged on two sides of the box bottom plate, clamping blocks corresponding to the bayonets are arranged on the outer side of the inner side plate, and when the left body plate and the right body plate are vertically folded relative to the box bottom plate, the clamping blocks on the inner side plate can be clamped into the bayonets to form fixation of the inner side plate, so that the insertion space is formed.

Further, the aircraft box is made of corrugated paper.

Compared with the prior art, the utility model has the following beneficial effects:

the utility model is provided with a box bottom plate, a front body plate, a rear body plate, a right body plate, a left body plate, an inner side plate, a flap, a cover plate assembly and a fixing device, wherein the box body is formed by vertically folding the front body plate, the rear body plate, the right body plate and the left body plate relative to the box bottom plate, the inner side plate, the right body plate and the left body plate form an insertion space, the flap can be inserted into the insertion space to fix the box body structure, the cover plate assembly and the fixing device are arranged to form a complete box body, the fixing device has a fixing and buffering effect on an internal loading object, the insertion space is formed by the folding structure to enable a socket to be easily inserted, and the stability and the pressure resistance of the airplane box are improved by the multilayer structure.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

FIG. 1 is a schematic structural view of the present invention;

fig. 2 is a schematic structural view of the fixing device of the present invention.

In the figure: 1. the box comprises a box bottom plate, 2 front body plates, 3 rear body plates, 4 front flaps, 5 right body plates, 6 inner side plates, 7 left body plates, 8 bayonets, 9 clamping blocks, 10 upper cover plates, 11 side plates, 12 fixing plates and 13 inserting tongues.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

As shown in fig. 1-2, an aircraft box with a fixing device comprises a box bottom plate 1, and a front body plate 2, a rear body plate 3, a right body plate 5 and a left body plate 7 respectively connected to four sides of the box bottom plate 1 in a foldable manner, wherein one ends of the left body plate 7 and the right body plate 5 away from the box bottom plate 1 are connected to an inner side plate 6 in a foldable manner, the inner side plate 6 is respectively connected to the left body plate 7 and the right body plate 5 through wide crease lines 17, the inner side plate 6 can be respectively folded inwards around the wide crease lines 17, an insertion space is formed between the inner side plate 6 and the left body plate 7 and the right body plate 5, flaps 4 capable of being inserted into the insertion space are respectively arranged on the left side and the right side of the front body plate 2 and the rear body plate 3, and the front body plate 2, the rear body plate 3, the right body plate 5 and the left body plate 7 are vertically folded relative to the box bottom plate 1, the flap 4 is insertable into the insertion space to form a box-like structure, and comprises a cover plate assembly arranged on the side of the rear body plate 3 remote from the box bottom plate 1, and a fixing device arranged in the box for fixing a load.

The utility model is provided with a box bottom plate 1, a front body plate 2, a rear body plate 3, a right body plate 5, a left body plate 7, an inner side plate 6, a flap 4, a cover plate assembly and a fixing device, wherein the front body plate 2, the rear body plate 3, the right body plate 5 and the left body plate 7 are vertically folded relative to the box bottom plate 1 to form a box body, the inner side plate 6, the right body plate 5 and the left body plate 7 form an insertion space through the arrangement of the inner side plate 6, the flap 4 can be inserted into the insertion space to fix the box body structure, and a complete box body is formed through the arrangement of the cover plate assembly and the fixing device, the fixing device has the function of fixing and buffering on internal loads, the insertion space is formed through the folding structure to enable a socket to be easily inserted, and the multilayer structure increases the stability and the pressure resistance of the airplane box.

Specifically, as shown in the figure, the fixing device comprises an inner lining plate 14 and a height side plate 15 which is connected to four side plates of the inner lining plate 14 in a folding mode, the height side plate 15 can be folded vertically relative to the inner lining plate 14 to form a supporting foot for supporting the inner lining plate 14, and a through hole 16 for fixing a loading object is formed in the inner lining plate 14.

In particular, as shown, the load is a cup, and the through hole 16 may be correspondingly configured according to the structure of the cup.

Specifically, as shown in the figure, the cover plate assembly comprises an upper cover plate 10 connected with a rear body plate 3 in a foldable and compressible manner, side plates 11 are connected to two sides of the upper cover plate 10 in a foldable and compressible manner, the side plates 11 can be vertically folded relative to the upper cover plate 10 and inserted into the interior of the aircraft box to form a cover, a fixing plate 12 is connected to one side of the upper cover plate 10 far away from the rear body plate 3 in a foldable and compressible manner, inserting tongues 13 are connected to two sides of the fixing plate 12 in a foldable and compressible manner, the inserting tongues 13 can be vertically folded relative to the fixing plate 12, and when the upper cover plate 10 is in a covered state, the inserting tongues 13 can be inserted into the inserting space to form a fixing effect on the upper cover plate 10.

Specifically, as shown in the drawing, the insertion tongue 13 is provided in an oval shape to facilitate insertion into the insertion space.

Specifically, as shown in the figure, bayonets 8 are arranged on two sides of the box bottom plate 1, clamping blocks 9 corresponding to the bayonets 8 are arranged on the outer side of the inner side plate 6, and when the left body plate 7 and the right body plate 5 are vertically folded relative to the box bottom plate 1, the clamping blocks 9 on the inner side plate 6 can be clamped into the bayonets 8 to fix the inner side plate 6, so that the insertion space is formed.

Specifically, as shown in the figures, the aircraft box is made of corrugated paper.

Specifically, the folding principle of the utility model is as follows:

step 1, folding and pressing the die-cut airplane box along pressing lines, conveniently folding, folding and erecting a front body plate and a rear body plate, and then folding left and right flaps of the front and rear body plates for 90 degrees;

step 2, folding and erecting the left and right body plates, folding the body plates in the left and right body plates inwards, covering the left and right flaps of the front and rear body plates, and buckling the left and right flaps into the locking opening of the bottom plate;

step 3, folding and pressing all side plates of the lining plate along the crease lines, folding the side plates downwards for 90 degrees, and then putting the side plates into the box body, wherein the bottoms of the side plates are tightly contacted with the bottom of the box;

step 4, folding the left and right side plates of the cover plate, and covering the box body with the cover plate;

and 5, folding the left and right inserting tongues of the box cover front body plate in half, opening into a gap formed at two ends of the box body, and then molding.

Furthermore, the left side and the right side of the airplane box are normally supported by three layers of paper boards respectively, but the inner lining and the left flap and the right flap of the box cover form a fourth layer of paper board support in the same plane, and compared with other airplane boxes and common paper boxes, the airplane box has higher strength, allows the stacking number to be far larger than that of the common paper boxes, and has better stability;

furthermore, the liner and the box body are perfectly combined in size, product stability is facilitated, the liner is provided with the hollow similar to a cat face, a good appearance display effect is achieved, meanwhile, the baffle on the liner fixes products, and a buffering protection effect is achieved.

The novel inner lining structure is added while inheriting the advantages of a common aircraft box, such as corrugated boards, simplicity in manufacturing, mass production, stable structure, green packaging, environment friendliness, good stability, good pressure resistance, relatively low cost, high cost performance and the like, the side plates of the newly added inner lining structure and the left and right front plates of the box cover form a fourth layer of paper board support on the same plane, the stacking number is allowed to be far greater than that of the common aircraft box and the common paper box, the structural stability is better, and the pressure resistance is stronger; simultaneously, the baffle position of newly-increased inside lining plays fixed, the protection effect of buffering to the product, improves overall stability, avoids the friction damaged, and the condition such as collision damage, simultaneously, inside lining structural design possess better outward appearance effect.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the utility model, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.

Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims

1. The airplane box with the fixing device is characterized by comprising a box bottom plate (1), and a front body plate (2), a rear body plate (3), a right body plate (5) and a left body plate (7) which are respectively connected to four sides of the box bottom plate (1) in a foldable manner, wherein one ends of the left body plate (7) and the right body plate (5) far away from the box bottom plate (1) are connected with an inner side plate (6) in a foldable manner, the inner side plate (6) is respectively connected with the left body plate (7) and the right body plate (5) through wide-grain creases (17), the inner side plate (6) can be respectively folded inwards around the wide-grain creases (17), insertion spaces are formed between the inner side plate (6) and the left body plate (7) and the right body plate (5), and flap pieces (4) capable of being inserted into the insertion spaces are arranged on the left side and the right side of the front body plate (2) and the rear body plate (3), when the front body plate (2), the rear body plate (3), the right body plate (5) and the left body plate (7) are vertically folded relative to the box bottom plate (1), the flap (4) can be inserted into the insertion space to form a box-shaped structure, the box-shaped structure further comprises a cover plate assembly arranged on one side, away from the box bottom plate (1), of the rear body plate (3) and a fixing device arranged in the box and used for fixing a loaded article.

2. The aircraft box with fastening device according to claim 1, characterized in that the fastening device comprises an inner lining panel (14) and a height side panel (15) foldably connected to four side panels of the inner lining panel (14), the height side panel (15) being foldable vertically relative to the inner lining panel (14) to form a support foot for supporting the inner lining panel (14), the inner lining panel (14) being provided with through holes (16) for fastening loads.

3. The aircraft box with fastening device according to claim 2, characterized in that the load is a cup, the through-holes (16) are correspondingly arranged according to the cup structure, and the inner lining (14) is placed in the aircraft box for use.

4. The aircraft box with the fixing device according to claim 1, characterized in that the cover plate assembly comprises an upper cover plate (10) connected with a rear body plate (3) in a foldable manner, two sides of the upper cover plate (10) are connected with side plates (11) in a foldable manner, the side plates (11) can be vertically folded relative to the upper cover plate (10) and inserted into the aircraft box to form a cover, one side of the upper cover plate (10) far away from the rear body plate (3) is connected with a fixing plate (12) in a foldable manner, two sides of the fixing plate (12) are connected with plug tongues (13) in a foldable manner, the plug tongues (13) can be vertically folded relative to the fixing plate (12), and when the upper cover plate (10) is in a covered state, the plug tongues (13) can be inserted into the insertion space to form a fixing of the upper cover plate (10).

5. An aircraft box with fastening device according to claim 4, characterized in that the insertion tongue (13) is provided with an oval shape which facilitates insertion into the insertion space.

6. The aircraft box with the fixing device according to claim 1, wherein bayonets (8) are arranged on two sides of the box bottom plate (1), clamping blocks (9) corresponding to the bayonets (8) are arranged on the outer side of the inner side plate (6), and when the left body plate (7) and the right body plate (5) are vertically folded relative to the box bottom plate (1), the clamping blocks (9) on the inner side plate (6) can be clamped into the bayonets (8) to fix the inner side plate (6), so that the insertion space is formed.

7. The aircraft cassette of claim 1, wherein the aircraft cassette is corrugated paper.