CN218617658U - Exempt from to assemble integral type express delivery aircraft box - Google Patents

Exempt from to assemble integral type express delivery aircraft box Download PDF

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Publication number
CN218617658U
CN218617658U CN202222737018.2U CN202222737018U CN218617658U CN 218617658 U CN218617658 U CN 218617658U CN 202222737018 U CN202222737018 U CN 202222737018U CN 218617658 U CN218617658 U CN 218617658U
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China
Prior art keywords
plate
folded
folded plate
creases
box
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CN202222737018.2U
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Chinese (zh)
Inventor
倪东成
程相顺
杨新风
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Qingdao Shikang Xingwei Printing And Packaging Co ltd
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Qingdao Shikang Xingwei Printing And Packaging Co ltd
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Priority to CN202222737018.2U priority Critical patent/CN218617658U/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02WCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
    • Y02W30/00Technologies for solid waste management
    • Y02W30/50Reuse, recycling or recovery technologies
    • Y02W30/80Packaging reuse or recycling, e.g. of multilayer packaging

Abstract

The utility model discloses an assembly-free integrated express airplane box in the technical field of paper boxes, which comprises a bottom plate, a front plate, a back plate, a top plate, a left side plate and a right side plate, wherein the left side and the right side of the bottom plate are respectively connected with the left side plate and the right side plate through creases, a left folded plate is not connected with the left side plate, a right folded plate is not connected with the right side plate, the creases respectively separate the left folded plate, the right folded plate, the left folded plate and the right folded plate into a right-angled trapezoidal plate and a fan-shaped plate, and one bevel edge of the fan-shaped plate of the left folded plate and the right folded plate is connected with the front plate; one bevel edge of the sector plate of the left two folding plates and the right two folding plates is connected with the back plate. The beneficial effects are as follows: the shape of the ear is changed according to the folding forming rule, the reverse indentation strip is added on the ear to realize reverse folding, the airplane box is integrated, the cover is opened, and the boxes on two sides are formed by pulling one side to realize rapid packaging.

Description

Exempt from to assemble integral type express delivery aircraft box
Technical Field
The utility model belongs to the technical field of the carton, in particular to exempt from to assemble integral type express delivery aircraft box.
Background
At present, boxes for E-commerce express delivery are basically pasted with mouth boxes through adhesive tapes, finished products are low, but the appearance is low, the boxes are not attractive, more and more E-commerce companies adopt airplane boxes as packaging boxes, but the general box types of the airplane boxes on the market at present are manually folded and formed on site when the airplane boxes need to be packaged, time and labor are wasted, the E-commerce delivery efficiency is greatly influenced, and the folding-free integrated type airplane box which is designed and researched aiming at the current E-commerce confusion is designed and developed.
SUMMERY OF THE UTILITY MODEL
In order to solve the above problem, the utility model discloses the decision research and development exempt from to assemble integral type express delivery aircraft box.
An assembly-free integrated express airplane box comprises a bottom plate, a front plate, a rear plate, a top plate, a left side plate and a right side plate, wherein the front end and the rear end of the bottom plate are respectively connected with the front plate and the rear plate through creases; the front side and the rear side of the top plate are respectively connected with a rear plate and a front pinch plate, and the left side and the right side of the top plate are respectively connected with a left side inserting plate and a right side inserting plate;
the left folded plate is not connected with the left side plate, the right folded plate is not connected with the right side plate, the left two folded plates are not connected with the left side plate, the right two folded plates are not connected with the right side plate, creases are respectively arranged on the left folded plate, the right folded plate, the left two folded plate and the right two folded plate, the creases respectively divide the left folded plate, the right folded plate, the left two folded plate and the right two folded plate into a right-angled trapezoidal plate and a sector plate, and one bevel edge of the sector plate of the left folded plate and the right folded plate is connected with the front plate; one bevel edge of the sector plate of the left second folded plate and the right second folded plate is connected with the back plate.
Furthermore, the front buckle plate also comprises a front extension plate, and one side of the front extension plate is connected with one side of the front buckle plate through a crease.
The utility model discloses the beneficial effect who gains as follows: become the box and more pleasing to the eye than ordinary aircraft box, it is more firm, alleviated the condition because of the unusual damage that the commodity circulation violence loading and unloading leads to, change aircraft box and insert box ear length, change the ear shape according to the fold-forming rule, increase reverse indentation strip on the ear, realize reverse folding, aircraft box realizes the integration, lifts the lid, draws the shaping of both sides box, realizes quick packing, and the shaping back stereoeffect is good, and the deflection is high, and it is convenient to convert into.
Drawings
Fig. 1 is a schematic structural diagram of an assembly-free integrated express aircraft box in embodiment 1;
fig. 2 is a perspective view of an assembly-free integrated express aircraft box according to embodiment 1;
fig. 3 is a schematic structural view of an assembly-free integrated express delivery aircraft box according to embodiment 2;
the reference numbers in the figures are:
1 bottom plate, 2 front bezel, 3 back plates, 4 roof, 5 left side board, 6 right side board, 7 left side buckle, 8 right side buckle, 9 left side picture peg, 10 right side picture peg, 11 left folded plate, 12 right folded plate, 13 left two folded plates, 14 right two folded plates, 15 preceding buckle, 16 preceding extension boards.
Detailed Description
Example 1
As shown in fig. 1-2, an assembly-free integrated express airplane box comprises a bottom plate 1, a front plate 2, a rear plate 3, a top plate 4, a left side plate 5 and a right side plate 6, wherein the front end and the rear end of the bottom plate 1 are respectively connected with the front plate 2 and the rear plate 3 through creases, the left side and the right side of the bottom plate 1 are respectively connected with the left side plate 5 and the right side plate 6 through the creases, the outer end of the left side plate 5 is connected with a left buckle plate 7 through the creases, the outer end of the right side plate 6 is connected with a right buckle plate 8 through the creases, the left end and the right end of the front plate 2 are respectively connected with a left folded plate 11 and a right folded plate 12 through the creases, and the left end and the right end of the rear plate 3 are respectively connected with a left folded plate 13 and a right folded plate 14; the front side and the rear side of the top plate 4 are respectively connected with a rear plate 3 and a front buckle plate 15, and the left side and the right side of the top plate 4 are respectively connected with a left side inserting plate 9 and a right side inserting plate 10;
the left first folded plate 11 is not connected with the left side plate 5, the right first folded plate 12 is not connected with the right side plate 6, the left second folded plate 13 is not connected with the left side plate 5, the right second folded plate 14 is not connected with the right side plate 6, creases are respectively arranged on the left first folded plate 11, the right folded plate 13, the left second folded plate 12 and the right second folded plate 14, the creases respectively divide the left first folded plate 11, the right folded plate 13, the left second folded plate 12 and the right second folded plate 14 into a right-angled trapezoidal plate and a sector plate, and one bevel edge of the sector plate of the left first folded plate 11 and the right folded plate 12 is connected with the front plate 2; the folding marks respectively divide the left and right folded plates 13 and 14 into a right-angled trapezoidal plate and a fan-shaped plate, and one bevel edge of the fan-shaped plate of the left and right folded plates 13 and 14 is connected with the back plate 3. The specific dimensions are shown in fig. 1 in millimeters.
Example 2
As shown in fig. 3, the front extension plate 16 is further included, one side of the front extension plate 16 is connected with one side of the front gusset plate 15 through a crease, and the rest is the same as that of the embodiment 1.

Claims (2)

1. An assembly-free integrated express airplane box comprises a bottom plate, a front plate, a rear plate, a top plate, a left side plate and a right side plate, wherein the front end and the rear end of the bottom plate are respectively connected with the front plate and the rear plate through creases; the front side and the rear side of the top plate are respectively connected with a rear plate and a front pinch plate, and the left side and the right side of the top plate are respectively connected with a left side inserting plate and a right side inserting plate; the method is characterized in that: the left folded plate is not connected with the left side plate, the right folded plate is not connected with the right side plate, the left two folded plates are not connected with the left side plate, the right two folded plates are not connected with the right side plate, creases are respectively arranged on the left folded plate, the right folded plate, the left two folded plate and the right two folded plate, the creases respectively divide the left folded plate, the right folded plate, the left two folded plate and the right two folded plate into a right-angled trapezoidal plate and a sector plate, and one bevel edge of the sector plate of the left folded plate and the right folded plate is connected with the front plate; one bevel edge of the sector plate of the left two folding plates and the right two folding plates is connected with the back plate.
2. The assembly-free integrated express delivery aircraft box of claim 1, wherein: still include preceding extension board, one side of preceding extension board passes through the crease with one side of preceding buckle and is connected.
CN202222737018.2U 2022-10-18 2022-10-18 Exempt from to assemble integral type express delivery aircraft box Active CN218617658U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202222737018.2U CN218617658U (en) 2022-10-18 2022-10-18 Exempt from to assemble integral type express delivery aircraft box

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202222737018.2U CN218617658U (en) 2022-10-18 2022-10-18 Exempt from to assemble integral type express delivery aircraft box

Publications (1)

Publication Number Publication Date
CN218617658U true CN218617658U (en) 2023-03-14

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN202222737018.2U Active CN218617658U (en) 2022-10-18 2022-10-18 Exempt from to assemble integral type express delivery aircraft box

Country Status (1)

Country Link
CN (1) CN218617658U (en)

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