Anti-leakage zipper type material-saving airplane box

By changing the groove path and indentation line, and combining them with a cross-fixing structure and double-sided adhesive tear strips, the problems of leakage and material waste in the aircraft box were solved, achieving the effects of material saving and leakage prevention.

CN223687053UActive Publication Date: 2025-12-19SHANGHAI YUANTU IND & TRADE CO LTD
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Patent Information

Application Number
CN202520319968.4
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-02-26
Publication Date
2025-12-19
Estimated Expiration
2035-02-26

AI Technical Summary

Technical Problem

Existing aircraft boxes suffer from leakage and material waste during the packaging process, making it difficult to reduce costs while maintaining performance.

Method used

A leak-proof zipper-type material-saving airplane box was designed. By changing the groove path and combining the embossing line, the leak-proof function of the bottom of the box is increased. A cross-fixing structure is adopted on the left and right side panels. Double-sided tape and tear strips are used to achieve the sealing of the box, eliminating unnecessary materials to save costs.

Benefits of technology

It achieves reduced material usage, improved sealing and anti-tampering effects without compromising performance, and is easy to operate.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model belongs to the technical field of packaging boxes, and provides an anti-leakage zipper type material-saving airplane box which comprises a box body and a flip type box cover. The box body comprises a bottom plate, and front, rear, left and right side plates connected with four sides of the bottom plate, wherein the top of the rear side plate is connected with the box cover; the box cover comprises a cover plate, an auxiliary cover plate, a left clamping plate and a right clamping plate, the auxiliary cover plate is a switch of the airplane box, and double-faced adhesive tape and a tearing strip are pre-pasted on the auxiliary cover plate. The anti-seepage zipper type material-saving airplane box is characterized in that 1, a slotting path of a traditional process is changed, meanwhile, an indentation line is matched, and the box bottom has a certain anti-seepage function after being spliced, folded and formed; 2, the left and right side structures of the traditional airplane box are changed, the materials on the left and right sides are saved, the left and right clamping plates and the left and right side plates form cross fixation when the box cover is covered, and a better box sealing effect is brought; and by matching with the double-faced adhesive tape and the tearing strip for use, the anti-leakage and anti-mistaken-dismounting advantages are realized.
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Description

TECHNICAL FIELD

[0001] The utility model belongs to the packaging box technical field, concretely relates to a zippered material-saving aircraft box with anti-leakage. BACKGROUND

[0002] With the development of society and the change of people's consumption habits, the market demand for packaging boxes is more and more diversified, and with the fierce market competition, people hope to reduce the use cost of packaging materials under the premise of not reducing the performance of packaging materials. In view of the market demand, we designed this bottom anti-leakage zippered material-saving aircraft box, which has the following characteristics: 1. Change the slotting path of the traditional process and cooperate with the indentation line, and the box bottom has a certain anti-leakage function after folding forming; 2. Change the structure of the left and right sides of the traditional aircraft box, save the materials of the left and right sides, and form cross fixation when the left and right clamping plates and the left and right side plates are covered with the box cover, which brings better sealing effect; Use with double-sided tape and tear strip, which has the advantages of anti-leakage, material saving and anti-misassembly. SUMMARY

[0003] The utility model improves on the basis of the traditional aircraft box and proposes a zippered material-saving aircraft box with anti-leakage, which has a certain anti-leakage function at the bottom, saves materials and prevents misassembly, and is easy to operate.

[0004] The purpose of the utility model can be realized by the following technical scheme: a zippered material-saving aircraft box with anti-leakage, including box body and box cover, flip cover style, the box body contains bottom plate 1 and four edges connected with front side plate 2, rear side plate 3, left side plate 4 and right side plate 5, the box cover contains cover plate 11, auxiliary cover plate 12, left clamping plate 13 and right clamping plate 14, wherein the auxiliary cover plate 12 is the switch of sealing and opening, and the double-sided tape 1201 and tear strip 1202 are pre-stuck;The box body and the box cover are connected together by the rear side plate 3, when the box cover is covered, the left and right side plates 4, 5 of the box body are respectively crossed fixed with the left and right clamping plates 13, 14 of the box cover, the auxiliary cover plate 12 is covered on the front side plate 2, if sealing is needed, the double-sided tape 1201 surface release paper is peeled off to stick the auxiliary cover plate 12 and the front side plate 2 together, once sealed, a sealed space is formed, and the box can only be opened by tearing the tear strip 1202;The double-sided tape 1201 and the tear strip 1202 are disposable.

[0005] Further, the front side plate 2 is connected with the front inner flap 6, and the upper left corner of the front side plate 2 is cut off, and the upper right corner is cut off; the left side plate 4 is connected with the left front flap 7 at the front edge and connected with the left rear flap 8 at the rear edge; the right side plate 5 is connected with the right front flap 9 at the front edge and connected with the right rear flap 10 at the rear edge; the front side plate 2 between the left front flap 7 and the right front flap 9 is cut off by a die-cutting slot; the front inner flap 6 has two "V" shaped small notches, and the left edge of the left front flap 7 and the right edge of the right front flap 9 are respectively provided with a notch with a score line, and when the box is folded, the two small notches of the front inner flap 6 are respectively clamped into the notches of the left front flap 7 and the right front flap 9 to fix the box body.

[0006] Further, the rear side plate 3 is connected with the bottom plate 1 and the cover plate 11, and the left and right edges are respectively the left rear flap 8 and the right rear flap 10 which are cut off by die-cutting slots, and a left insertion plate 301 and a right insertion plate 302 are respectively left on the left and right sides of the rear side plate during die-cutting, the left insertion hole 801 is provided at the connection between the left rear flap 8 and the left side plate 4, and the right insertion hole 1001 is provided at the connection between the right rear flap 10 and the right side plate 5, and when the left rear flap 8 and the right rear flap 10 are bent inward by 90 degrees, the left insertion plate 301 and the right insertion plate 302 are respectively inserted into the left insertion hole 801 and the right insertion hole 1001, so as to fix the left and right side plates 4 and 5 and the rear side plate 3.

[0007] Further, the cutting and slotting between the left front flap 7, the right front flap 9 and the front side plate 2 and between the left rear flap 8, the right rear flap 10 and the rear side plate 3 are changed from straight cutting in the traditional process to a combination of partial cutting and partial score line, the slotting is extended by 3 cm outward at 90 degrees at a position 3 cm away from the bottom plate 3 and cut by 3 cm to form an "L" shape, the length of 3 cm away from the bottom plate 3 is changed from slotting cutting to score line, and a 45 degree score line is additionally provided at a right angle from the bottom plate and connected with the extended slotting, the left slotting is bent leftward by 90 degrees, and the right slotting is bent rightward by 90 degrees, so as to realize the anti-leakage function of the bottom plate after the box is folded and formed.

[0008] Further, the left side plate 4 and the right side plate 5 have a large V-shaped opening, the upper left corner of the left clamping plate 13 and the upper right corner of the right clamping plate 14 are cut off a part, when the box cover is covered, the left and right clamping plates are fixed by the large V-shaped opening and the left and right side plates to form a cross state, and the left and right sides of the aircraft box are better protected; the traditional aircraft box further extends a left side plate inner flap with a small size difference on the left side of the left side plate 4, and there are double pressure lines with a spacing of 8-10 mm between the left side plate and the left side plate inner flap; one or two insertion ears with a length of about 5 mm are further extended on the leftmost side of the left side plate inner flap, and there is one or two insertion holes on the side of the bottom plate corresponding to the connection between the left side plate and the bottom plate; similarly, the right side of the right side plate 5 of the traditional aircraft box further extends a right side plate inner flap with a small size difference, and there are double pressure lines with a spacing of 8-10 mm between the right side plate and the right side plate inner flap; one or two insertion ears with a length of about 5 mm are further extended on the rightmost side of the right side plate inner flap, and there is one or two insertion holes on the side of the bottom plate corresponding to the connection between the right side plate and the bottom plate; compared with the traditional aircraft box, the left and right side plates of the aircraft box are saved, the width of the left and right double pressure lines and the left and right insertion ears with a length of about 5 mm are saved, and the insertion hole corresponding to the insertion ear on the box bottom is cancelled, the corrugated paperboard on the box bottom is kept complete, and the anti-leakage function of the box bottom is strengthened.

[0009] Further, the left clamping plate 13 is connected with the left ear plate 15, the right clamping plate 14 is connected with the right ear plate 16, and the left ear plate 15 and the right ear plate 16 are the auxiliary cover plate 12 which is cut off by a slot, and when the box cover is covered, the left ear plate 15 is embedded into the left notch of the front side plate 2, and the right ear plate 16 is embedded into the right notch of the front side plate 2.

[0010] Further, the auxiliary cover plate 12 has a pre-pasted double-sided adhesive tape 1201 and a tear-off tape 1202, the double-sided adhesive tape 1201 is used for sealing the box, and the tear-off tape 1202 is used for opening the box; the release paper of the double-sided adhesive tape 1201 is torn off, and the auxiliary cover plate 12 is pasted on the surface of the front side plate 2; the pasting position is above the surface of the front side plate 2, and the left ear plate 15 and the right ear plate 16 embedded into the left and right notches are pasted together. BRIEF DESCRIPTION OF DRAWINGS

[0011] Figure 1 It is the unfolding schematic view of the utility model;

[0012] Figure 2 It is the marking schematic view of the utility model;

[0013] Figure 3 It is the application change view of the utility model, which is changed from disposable use to multiple use;

[0014] Figure 4 It is the folding box schematic view of the utility model;

[0015] Figure 5 The forming diagram of the utility model;

[0016] The solid line is a knife line, and the dotted line is an indentation line: 1, a bottom plate; 2, a front side plate; 3, a rear side plate; 301, a left plug-in plate; 302, a right plug-in plate; 4, a left side plate; 5, a right side plate; 6, a front inner folding plate; 7, a left front folding plate; 8, a left rear folding plate; 801, a left jack; 9, a right front folding plate; 10, a right rear folding plate; 1001, a right jack; 11, a cover plate; 12, a sub cover plate; 1201, double-sided adhesive tape; 1202, a tear strip; 13, a left clamping plate; 14, a right clamping plate; 15, a left ear plate; 16, a right ear plate; 17, a sub cover plate with changes; 18, a sub cover plate inner folding plate. DETAILED DESCRIPTION

[0017] The technical solutions in the embodiments of the utility model will be further described below with reference to the accompanying drawings and specific embodiments. It should be noted that, in the description of the present application, for the orientation words such as "up", "down", "left", "right", "front", "rear", "inner", "outer" and the like, only the orientation shown in the drawings is used for the convenience of expressing the present application and simplifying the description. The described embodiments are only part of the embodiments of the utility model. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without making creative efforts fall within the scope of protection of the utility model.

[0018] The following are specific operation steps:

[0019] Embodiment one

[0020] Reference Figure 1 Figure 2 Figure 4 Figure 5

[0021] First step: fold the left side plate 4 and the right side plate 5 from the left and right sides respectively, so that the left and right side plates stand vertically at a 90-degree state with the bottom plate 1;

[0022] Second step: immediately fold the left front folding plate 7 and the right front folding plate 9 inward by 90 degrees;

[0023] Third step: then fold the front side plate 2, so that it is tightly attached to the left front folding plate 7 and the right front folding plate 9;

[0024] Fourth step: fold the front inner folding plate 6 inward and downward, and at the same time, fold the notched indentation lines of the left front folding plate 7 and the right front folding plate 9, so as to insert the two small notches of the front inner folding plate 6 into the notches of the left and right front folding plates respectively;

[0025] Fifth step: fold the left rear folding plate 8 and the right rear folding plate 10 inward by 90 degrees, so as to expose the left jack 801 and the right jack 1001;

[0026] Sixth step: then fold the back plate 3, while the left and right plug-in plate 301 and 302 on both sides of the back plate 3 are inserted into the corresponding left and right plug-in holes 801 and 1001;

[0027] Seventh step: fold the left and right clamping plates 13 and 14, cover the cover plate 11, while the left clamping plate 13 is inserted into the left side plate 4 and is wound out from the V-shaped opening of the left side plate 4, so that the left clamping plate 13 and the left side plate 4 form a cross state, and the left and right clamping plates 13 and 14 are operated simultaneously;

[0028] Eighth step: embed the left ear plate 15 into the left notch of the front side plate 2, embed the right ear plate 16 into the right notch of the front side plate 2, peel off the release paper of the double-sided adhesive tape 1201 of the secondary cover plate 12, and paste the front side plate 2 to complete the sealing of the box, and also paste the left ear plate 15 and the right ear plate 16.

[0029] Example two

[0030] The utility model slightly changes, cancels the double-sided adhesive tape and the tear strip, the secondary cover plate 17 increases the secondary cover plate inner folding plate 18 with the bolt, and the plug-in hole is increased between the cover plate 11 and the secondary cover plate 17, so that the one-time use zipper type material-saving aircraft box can be changed into the new material-saving aircraft box that can be repeatedly used, and reference Figure 2 Figure 3 , the folding steps are as follows:

[0031] The first to seventh steps are the same as those in example one;

[0032] Eighth step: fold the left and right ear plates 15 and 16, fold the secondary cover plate inner folding plate 18, wrap the left and right ear plates 15 and 16, insert the bolt of the secondary cover plate inner folding plate 18 into the plug-in hole between the cover plate 11 and the secondary cover plate 17, and complete the folding of the box cover.

[0033] The above is only the preferred embodiment of the utility model, but the protection scope of the utility model is not limited to this. Any skilled person in the art can make changes or modifications to the above disclosed technology content to obtain equivalent embodiments with equivalent changes applied to other fields, but any simple modification, equivalent change and modification made to the above embodiments according to the technical essence of the utility model still belongs to the protection scope of the technical scheme of the utility model. The skilled person in the technical field to which the utility model belongs can make various modifications or supplements to the described specific embodiments or adopt similar ways to replace, but will not deviate from the spirit of the utility model or exceed the scope defined by the attached claims.

Claims

1. A leakproof, zipper type material-saving aircraft box, comprising a box body and a box cover, the box body comprising a bottom plate (1) and front side plate (2), rear side plate (3), left side plate (4) and right side plate (5) connected to the four edges of the bottom plate (1), and the box cover comprising a cover plate (11), a sub-cover plate (12), a left clamping plate (13) and a right clamping plate (14), characterized in that, The flip cover is connected with the box body through the rear side plate (3), when the cover is closed, the left clamping plate (13) and the left side plate (4) and the right clamping plate (14) and the right side plate (5) form cross fixation, the sub-cover plate (12) is the switch of the box, and the double-sided adhesive tape (1201) and the tear strip (1202) are pre-stuck, the slotting process is changed, the traditional jack of the bottom plate of the aircraft box is cancelled, the integrity of the bottom plate is retained, and the box is folded and formed, and the box bottom has the anti-leakage function.

2. A leak-proof zipper-saved airplane box according to claim 1, characterized in that: The front edge of the left side plate (4) is connected with the left front folding plate (7), and the rear edge is connected with the left rear folding plate (8). The front edge of the right side plate (5) is connected with the right front folding plate (9), and the rear edge is connected with the right rear folding plate (10). The left upper corner of the front side plate (2) is cut off to form a left missing corner, and the right upper corner is cut off to form a right missing corner. The front inner folding plate (6) has two "V"-shaped small clamping holes. The left edge of the left front folding plate (7) and the right edge of the right front folding plate (9) are respectively provided with a slot with a pressing line. The left side plate (4) and the left rear folding plate (8) are connected at the left jack (801). The right side plate (5) and the right rear folding plate (10) are connected at the right jack (1001).

3. A leak-proof, zipper-enabled, material-saving aircraft box according to claim 2, characterized in that: The slotting cutting between the left front folding plate (7), the right front folding plate (9) and the front side plate (2) is changed from the traditional straight line cutting to partial cutting combined with partial pressing line. The slotting cutting is cut for 3 cm in an "L" shape at a position 3 cm away from the bottom plate. The length of 3 cm away from the bottom plate is changed from slotting cutting to pressing line. Another 45-degree pressing line is added at the right angle of the bottom plate (1) and connected with the extended slot. The left slot bends leftwards by 90 degrees, and the right slot bends rightwards by 90 degrees. The slotting process between the left rear folding plate (8), the right rear folding plate (10) and the rear side plate (3) is the same as that between the left front folding plate (7), the right front folding plate (9) and the front side plate (2). By changing the traditional slotting mode, the integrity of the bottom plate is retained, and the bottom plate has the anti-leakage function after the box is folded and formed.

4. A leak-proof zipper-saved airplane box according to claim 1, characterized in that: The left edge of the cover plate (11) is connected with the left clamping plate (13), and the right edge is connected with the right clamping plate (14). The left clamping plate (13) is connected with the left ear plate (15), and the right clamping plate (14) is connected with the right ear plate (16). A part of the left upper corner of the left clamping plate (13) and the right upper corner of the right clamping plate (14) are cut off. When the cover is closed, the left clamping plate (13) and the right clamping plate (14) are fixed in the cross state through the large "V"-shaped openings of the left side plate (4) and the right side plate (5) respectively. The left ear plate (15) and the right ear plate (16) are respectively embedded in the left missing corner and the right missing corner of the front side plate (2) before sealing the box.

5. A leak-proof zipper airplane box of claim 1, wherein: The length of the auxiliary cover plate (12) is consistent with the front side plate (2), the auxiliary cover plate (12) covers the left and right notches of the front side plate (2), when the box needs to be sealed, the release paper on the surface of the double-sided adhesive (1201) is peeled off, the auxiliary cover plate (12) is pasted and fixed above the surface of the front side plate (2), and the left ear plate (15) and the right ear plate (16) embedded in the left and right notches of the front side plate (2) are also pasted and fixed to complete the sealing of the box.