CN212314139U - Area-saving airplane box cutting piece - Google Patents

Area-saving airplane box cutting piece Download PDF

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Publication number
CN212314139U
CN212314139U CN202020215256.5U CN202020215256U CN212314139U CN 212314139 U CN212314139 U CN 212314139U CN 202020215256 U CN202020215256 U CN 202020215256U CN 212314139 U CN212314139 U CN 212314139U
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China
Prior art keywords
plate
box
area
sheet
bottom plate
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CN202020215256.5U
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Chinese (zh)
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桂珍婷
钟秀谷
黄睿修
花志翔
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Hangzhou Bingxin Environmental Protection Packaging Co Ltd
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Hangzhou Bingxin Environmental Protection Packaging Co Ltd
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Priority to CN202020215256.5U priority Critical patent/CN212314139U/en
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Abstract

The utility model discloses an area-saving airplane box cutting piece which is of a symmetrical structure and comprises a bottom plate, wherein two side plates and two end plates which are alternately distributed are arranged on the periphery of the bottom plate, connecting ear plates which can be attached to the end plates are respectively arranged at the two ends of the side plates, a cover plate is arranged at the outer end of one end plate, and a connecting front piece is arranged at the edge of the cover plate; the outer end of the other end plate is provided with a guard plate which can be matched with the end plate to cover the connecting lug plate, and a matched clamping structure is arranged between the guard plate and the bottom plate; the two sides of the end plate provided with the cover plate are respectively provided with a connecting sheet which can be attached to the outer side of the side plate, the connecting sheet is provided with a fixing sheet which can be folded to the inner side of the attached side plate, and a connecting structure is arranged between the fixing sheet and the bottom plate. The utility model discloses a benefit is that the area concentration nature of each part of aircraft box cutting piece is good, compares prior art, can obtain bigger volume's aircraft box through the cardboard of less area, reduces the manufacturing cost of aircraft box.

Description

Area-saving airplane box cutting piece
Technical Field
The utility model belongs to the technical field of the packing carton, specifically an aircraft box cutting blade that area was saved.
Background
An aircraft carton is a paper box used in large numbers, so called for the developed figures like airplanes, mainly for packaging light, thin, flat articles such as clothing and food. The Chinese patent document CN208134843U discloses an environment-friendly aircraft box without sealing tape in 2018, 11.23.A box cover, a box top, a back box plate, a box bottom and a front box plate are sequentially connected, each part is distinguished by a bending line, a tearing and punching line is arranged on the box cover, a male lock is arranged in the middle of the outer side of the box cover, the box top is positioned between a left box top folded plate and a right box top folded plate, the three parts are connected and distinguished by the bending line, the back box plate is positioned between a left back folded plate and a right back folded plate, the three parts are connected and distinguished by the bending line, the box bottom is positioned between the left box bottom folded plate and the right box bottom folded plate, the three parts are connected and distinguished by the bending line, the left box bottom folded plate is connected with the left inner folded plate, the right box bottom folded plate is connected with the right inner folded plate, both the left inner folded plate and the right inner folded plate. The structure is a common airplane box cutting piece structure in the prior art, and has the following defects: the left and right folded plates and the left and right inner folded plates are required to be respectively matched to complete the forming of the box body, and the left and right folded plates and the left and right inner folded plates are arranged to ensure that cut pieces of the airplane box cannot be concentrated in a cuboid paperboard, so that the utilization rate of the paperboard is poor, the area loss is large, and the production cost of the airplane box is increased.
Disclosure of Invention
Based on the problem, the utility model provides an aircraft box of area saving cuts out piece, and the area concentration nature of each part of aircraft box cutting out piece is good, compares prior art, can obtain bigger bulky aircraft box through the cardboard of littleer area, reduces the manufacturing cost of aircraft box.
In order to realize the utility model purpose, the utility model adopts the following technical scheme:
an airplane box cutting piece with saved area is of a symmetrical structure and comprises a bottom plate, wherein two side plates and two end plates which are alternately distributed are arranged on the periphery of the bottom plate, connecting lug plates which can be attached to the end plates are respectively arranged at two ends of each side plate, a cover plate is arranged at the outer end of one end plate, and a connecting flap piece is arranged at the edge of each cover plate; the outer end of the other end plate is provided with a guard plate which can be matched with the end plate to cover the connecting lug plate, and a matched clamping structure is arranged between the guard plate and the bottom plate; the two sides of the end plate provided with the cover plate are respectively provided with a connecting sheet which can be attached to the outer side of the side plate, the connecting sheet is provided with a fixing sheet which can be folded to the inner side of the attached side plate, and a connecting structure is arranged between the fixing sheet and the bottom plate.
Compared with the traditional airplane box, the box body is a single layer in the left and right directions, so that the area of the box body is effectively saved, and the production cost of the airplane box is reduced; the connection flap of the cover plate is inserted into the box, so that the connection reliability and the dustproof performance are ensured; the connecting ear plates are folded inwards to form a double-layer structure, so that the strength of the box body is improved; the end plate provided with the cover plate is fixedly connected with the side plate through the fixing piece and the connecting piece, and the connection is reliable and convenient.
Preferably, the clamping structure comprises a first convex strip positioned on the protective plate and a first clamping groove positioned on the edge of the bottom plate. The joint structure can adopt structures such as sand grip draw-in groove, projection jack, and sand grip and draw-in groove are preferred to this application, aim at convenient manufacturing, reduction in production cost.
Preferably, the outer end of the connecting flap is provided with a transition fillet. The connecting flap is convenient to insert into the box body.
Preferably, the connecting structure comprises a second convex strip positioned on the fixing sheet and a second clamping groove positioned on the edge of the bottom plate. The connection structure also can adopt structures such as sand grip draw-in groove, projection jack, and sand grip and draw-in groove are preferred to this application, aim at convenient manufacturing, reduction in production cost.
Preferably, the cut pieces are of a unitary structure. The whole box body is formed in a one-piece mode, the production process is simple, and the assembly is convenient.
Preferably, the connecting piece is in a right trapezoid shape, and the straight waist of the connecting piece is positioned on the end plate; the connecting sheet is separated from the adjacent connecting lug plate by a cutting line; the edge of the long bottom edge of the connecting sheet is provided with a fixing sheet which is positioned outside the edge of the cover plate and is separated by a cutting line. The connecting sheet is used for connecting the fixing sheet to complete the limit of the end plate and the side plate; the connecting lug plates adjacent to the connecting sheets are used for limiting the supporting cover plate, and the connecting sheets and the areas of the adjacent connecting lug plates are integrated in the corresponding areas of the two outer sides of the same end plate, so that the simplification of the areas of the connecting positions of the end plates and the side plates is realized.
Preferably, the height of the connecting piece is half of the height of the end plate. The strength between the connecting sheet and the adjacent connecting lug plates is close, and the stable supporting effect can be achieved by two structures.
To sum up, the beneficial effects of the utility model are that:
1. the whole box body is formed in a one-piece mode, the production process is simple, and the assembly is convenient;
2. compared with the traditional airplane box, the box body is a single layer in the left and right directions, so that the area of the box body is effectively saved, and the production cost of the airplane box is reduced;
3. the connection flap of the cover plate is inserted into the box, so that the connection reliability and the dustproof performance are ensured;
4. the guard plate is folded inwards to form a double-layer structure, so that the strength of the box body is improved;
5. the end plate provided with the cover plate is fixedly connected with the side plate through the fixing piece and the connecting piece, and the connection is reliable and convenient.
Drawings
Fig. 1 is a schematic structural view of the present invention, in which solid lines represent cutting lines; the dashed lines represent fold lines.
Fig. 2 to 9 are diagrams illustrating the steps of the present invention for folding into a box.
Wherein: the side plate 2 of the bottom plate 1 is connected with the ear plate 21, the end plate 3 is connected with the cover plate 4 and is connected with the first convex strip 51, the first clamping groove 52 of the protective plate 5 of the flap 41, the connecting plate 6 is connected with the second convex strip 71, the second clamping groove 72 of the fixing plate 7.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and the detailed description.
As shown in embodiment 1 of fig. 1, the cutting piece of the airplane box with saved area is a symmetrical structure, and the cutting piece is an integrated structure and comprises a bottom plate 1, two side plates 2 and two end plates 3 which are alternately distributed are arranged on the periphery of the bottom plate 1, two ends of each side plate 2 are respectively provided with a connecting ear plate 21 which can be attached to the end plate 3, the outer end of one end plate 3 is provided with a cover plate 4, and the edge of the cover plate 4 is provided with a connecting flap 41; the outer end of the connecting flap 41 is provided with a transition fillet. The outer end of the other end plate 3 is provided with a guard plate 5 which can be matched with the end plate 3 to cover the connecting lug plate 21, and a matched clamping structure is arranged between the guard plate 5 and the bottom plate 1; the clamping structure comprises a first convex strip 51 positioned on the protective plate 5 and a first clamping groove 52 positioned on the edge of the bottom plate 1. The two sides of the end plate 3 provided with the cover plate 4 are respectively provided with a connecting sheet 6 which can be attached to the outer side of the side plate 2, and the height of the connecting sheet 6 is half of the height of the end plate 3. The connecting sheet 6 is provided with a fixing sheet 7 which can be folded to the inner side of the attaching side plate 2, specifically, the edge of the long bottom edge of the connecting sheet 6 is provided with the fixing sheet 7, and the fixing sheet 7 is positioned outside the edge of the cover plate 4 and is separated by a cutting line. The connecting sheet 6 is in a right trapezoid shape, and the straight waist of the connecting sheet 6 is positioned on the end plate 3; the connecting sheet 6 is separated from the adjacent connecting ear plate 21 by a cutting line; a connecting structure is arranged between the fixing piece 7 and the bottom plate 1. The connecting structure comprises a second convex strip 71 positioned on the fixing sheet 7 and a second clamping groove 72 positioned at the edge of the bottom plate 1.
The folding steps of the application will be described below with reference to fig. 2 to 9 with reference to fig. 1.
A. The two side plates 2 are respectively folded upwards by 90 degrees, as shown in figure 2;
the connecting ear plates 21 at the two ends of the side plate 2 are respectively folded inwards by 90 degrees, as shown in fig. 3;
the end plate 3 where the protection plate 5 is located is folded upwards by 90 degrees, the protection plate 5 is folded around the connecting ear plate 21180 degrees, and the first convex strip 51 is matched with the first clamping groove 52, as shown in fig. 4;
the end panel 3 where the cover plate 4 is located is folded upwards by 90 degrees, as shown in fig. 5;
the connecting sheet 6 is turned over 90 degrees towards the inner direction of the airplane box, as shown in fig. 6;
the fixing piece 7 is turned over 180 degrees towards the interior of the airplane box, and a second convex strip 71 on the fixing piece 7 is matched with a second clamping groove 72 on the bottom plate 1, as shown in fig. 7;
the connecting flap 41 at the edge of the cover plate 4 is turned inwards by 90 degrees, as shown in fig. 8;
the cover plate 4 is folded over 90 degrees, as shown in fig. 9, and the aircraft box is finally formed.
The whole box body is formed in a one-piece mode, the production process is simple, and the assembly is convenient; compared with the traditional airplane box, the box body is a single layer in the left and right directions, so that the area of the box body is effectively saved, and the production cost of the airplane box is reduced; the connection flap 41 of the cover plate 4 is inserted into the box, so that the connection reliability and the dustproof performance are ensured; the guard plate 5 is folded inwards to form a double-layer structure, so that the strength of the box body is improved; the end plate 3 provided with the cover plate 4 is fixedly connected with the side plate 2 through the fixing piece 7 and the connecting piece 6, and the connection is reliable and convenient.

Claims (7)

1. The airplane box cutting piece with the saved area is characterized by being of a symmetrical structure and comprising a bottom plate, wherein two side plates and two end plates are alternately distributed on the periphery of the bottom plate; the outer end of the other end plate is provided with a guard plate which can be matched with the end plate to cover the connecting lug plate, and a matched clamping structure is arranged between the guard plate and the bottom plate; the two sides of the end plate provided with the cover plate are respectively provided with a connecting sheet which can be attached to the outer side of the side plate, the connecting sheet is provided with a fixing sheet which can be folded to the inner side of the attached side plate, and a connecting structure is arranged between the fixing sheet and the bottom plate.
2. The area saving airplane box panel of claim 1, wherein said snap-fit structure comprises a first protruding strip on the guard plate and a first snap-fit groove on the edge of the base plate.
3. An area saving aircraft box panel as claimed in claim 1 wherein the outer end of said attachment flap is provided with a transition radius.
4. The area-saving airplane box cutting piece according to claim 1 or 2, wherein the connecting structure comprises a second convex strip positioned on the fixing piece and a second clamping groove positioned on the edge of the bottom plate.
5. An area saving aircraft box panel as claimed in claim 1 wherein said panel is of unitary construction.
6. The area saving box cut of an aircraft as claimed in claim 1, wherein the connecting piece is in the shape of a right trapezoid, the straight waist of the connecting piece being located on the end plate; the connecting sheet is separated from the adjacent connecting lug plate by a cutting line; the edge of the long bottom edge of the connecting sheet is provided with a fixing sheet which is positioned outside the edge of the cover plate and is separated by a cutting line.
7. An area saving aircraft box panel as claimed in claim 1 or claim 6 wherein the connecting web is half the height of the end panel.
CN202020215256.5U 2020-02-26 2020-02-26 Area-saving airplane box cutting piece Active CN212314139U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020215256.5U CN212314139U (en) 2020-02-26 2020-02-26 Area-saving airplane box cutting piece

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020215256.5U CN212314139U (en) 2020-02-26 2020-02-26 Area-saving airplane box cutting piece

Publications (1)

Publication Number Publication Date
CN212314139U true CN212314139U (en) 2021-01-08

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN202020215256.5U Active CN212314139U (en) 2020-02-26 2020-02-26 Area-saving airplane box cutting piece

Country Status (1)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114572508A (en) * 2021-11-29 2022-06-03 杭州秉信环保包装有限公司 Concealed anti-theft lock structure on paper box

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114572508A (en) * 2021-11-29 2022-06-03 杭州秉信环保包装有限公司 Concealed anti-theft lock structure on paper box

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