CN214268298U

CN214268298U - Buckle formula aircraft box

Info

Publication number: CN214268298U
Application number: CN202022631196.8U
Authority: CN
Inventors: 蔡锦水
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-11-15
Filing date: 2020-11-15
Publication date: 2021-09-24
Anticipated expiration: 2030-11-15

Abstract

The invention discloses a buckle type aircraft box, comprising: go up buckle, lamina tecti, left side apron, right side apron, bottom plate, preceding curb plate, posterior lateral plate, left side board, right side board and end buckle board, going up buckle, lamina tecti, left side apron, right side apron, posterior lateral plate, bottom plate, preceding curb plate, left side board, right side board and end buckle board and pass through the crease and connect as an organic wholely, buckle device in the aircraft box through setting up need not to use the sticky tape can satisfy the encapsulation requirement, and one-step closure reduces intensity of labour, has improved security and feature of environmental protection.

Description

Buckle formula aircraft box

Technical Field

The utility model relates to a packing, accomodate technical field, specifically, relate to a packing carton that can be used to express delivery box, clothing shoes box, receiver etc.

Background

The existing packaging and containing boxes, such as express boxes and airplane boxes, mostly adopt a large amount of adhesive tape envelopes or adhesive bag envelopes for repeated packaging, and the boxes have the following defects: 1, the box stuck with the adhesive tape is not beneficial to recycling, and the discarded box has poor environmental protection property; 2 > the operation of sealing the box by using the adhesive tape is complicated, namely, the time for sealing the box is wasted, and the adhesive tape needs to be untied again when the box is opened, even by using tools such as scissors, the box opening operation is very inconvenient for 3 > the common airplane box is formed by a manual folding mode, the working efficiency is extremely low, and the materials are wasted

The current online shopping is on the rise, and the use of all kinds of packing containing boxes is also more and more frequent, owing to there is above-mentioned shortcoming, consequently, need one kind at present need not to use sticky tape, the feature of environmental protection is good, to user easy operation's packing containing box.

Disclosure of Invention

The utility model discloses based on above-mentioned prior art problem, the innovation provides an interior buckle formula aircraft box, through the folding buckle device of innovative design integral type, it is extravagant to have reduced the material, and whole box, division box process easy operation need not instrument a card and closes promptly, opens promptly one and draws, need not to use sticky tape or plastic bag big envelope, and the feature of environmental protection is good, the practicality is strong, has improved the recycle and utilization ratio and the work efficiency of packing carton by a wide margin.

The utility model provides a technical scheme as follows that above-mentioned technical problem took:

a buckle-type aircraft box characterized by comprising: the bottom connection forming device comprises an upper buckle plate, a top cover plate, a left cover plate, a right cover plate, a bottom plate, a front side plate, a rear side plate, a left side plate, a right side plate and a bottom buckle plate, wherein the upper buckle plate, the top cover plate, the left cover plate, the right cover plate, the rear side plate, the bottom plate, the front side plate, the left side plate, the right side plate and the bottom buckle plate are connected into a whole through creases, a positioning groove is arranged at the joint of the bottom plate and the front side plate of an airplane box, triangular connection areas are arranged at two ends of the left side plate and the right side plate of the airplane box, the triangular connection areas at two ends of the left side plate and the right side plate of the airplane box are respectively connected with the inner side plates at two ends of the front side plate and the inner side plates at two ends of the rear side plate through viscose glue or binding to realize the bottom connection forming of the packing box,

preferably, the aircraft box still includes buckle device, buckle device includes the last buckle mechanism that links to each other with the lamina tecti, the end buckle mechanism that links to each other with the preceding curb plate, it is provided with catching groove and buckle tongue to go up buckle mechanism, end buckle mechanism is provided with triangle buckle board, catching groove and flange, triangle buckle board divides into two sections through the indentation line and inwards buckles back and form a triangle-shaped back-off, and when the last buckle of box top cap inserted the end buckle inboard, inserts the buckle tongue in the catching groove that is located the end buckle simultaneously, and the catching groove in the middle of the last buckle locks each other with the triangle-shaped back-off that triangle buckle board formed.

Preferably, the outer surface of the aircraft box is printed or coated with a decorative pattern.

Preferably, the outer surface of the aircraft box is provided with a hole line type tearing anti-theft line for facilitating unpacking.

The assembly and locking process of the packing box of the invention is as follows:

the method comprises the steps of firstly, connecting triangular connecting areas at two ends of a left side plate and triangular connecting areas at two ends of a right side plate of an airplane box with bottom side portions of inner side plates at two ends of a front side plate and inner side plates at two ends of a rear side plate respectively through viscose glue or binding to finish packaging box bottom side portions, then dividing a triangular buckle plate on a bottom buckle plate into two sections to be bent inwards through crease lines to form a triangular inverted buckle, bending the bottom buckle plate inwards by 180 degrees through crease lines, clamping a flange at the top end of the bottom buckle plate into a positioning groove to achieve airplane box bottom assembly molding, finally, folding a left side cover and a right side cover mutually, inserting the left side cover and the right side cover into inner sides of left and right side plates of the box, inserting left buckle tongues and right buckle tongues positioned on an upper buckle plate into left and right buckle grooves of the bottom buckle plate, tightly downwards covering by force, and then, enabling the top cover plate to be incapable of opening, and finishing box locking.

Compared with the prior art, the invention has the beneficial effects that:

1 > the triangular folding connecting area is designed for pasting or binding connection, thereby saving the waste of materials compared with the common airplane case and improving the packaging efficiency.

2, the inner buckle device is designed for sealing without adhesive tape and adhesive bag sealing sleeve, thereby improving the safety and environmental protection of the packing box.

Drawings

FIG. 1 is a schematic illustration of an expanded configuration of an aircraft case

FIG. 2 is a schematic view of the bottom of the airplane box after the front, rear, left and right side plates are connected

FIG. 3 is a perspective view of the bottom of the airplane box after being formed

FIG. 4 is the effect diagram after the box sealing of the airplane

Fig. 5 is a perspective view of a triangular latch plate of the aircraft box latch mechanism.

Detailed Description

The invention is further described with reference to the following figures and specific embodiments:

referring to fig. 1-5, a snap-on aircraft case, comprising: the packaging box comprises an upper buckle plate 5, a top cover plate 4, a left cover plate 8, a right cover plate 9, a bottom plate 2, a front side plate 1, a rear side plate 3, a left side plate 6, a right side plate 7 and a bottom buckle plate 10, wherein the upper buckle plate, the top cover plate, the left cover plate, the right cover plate, the rear side plate, the bottom plate, the front side plate, the left side plate, the right side plate and the bottom buckle plate are connected into a whole through creases, a positioning groove 21 is arranged at the joint of the bottom plate 2 and the front side plate of the aircraft box, triangular connecting

areas

61, 62, 71 and 72 are arranged at two ends of the left side plate 6 and the right side plate 7 of the aircraft box, the

triangular connecting areas

61 and 62 at two ends of the left side plate 6 of the aircraft box and the triangular connecting

areas

71 and 72 at two ends of the right side plate 7 of the aircraft box are respectively connected and formed with the inner side plates at two ends of the front side plate 1 and the inner side plates at two ends of the rear side plate 3 through viscose glue or binding,

the aircraft box further comprises a buckling device, the buckling device comprises an upper buckling plate mechanism connected with the top cover plate 4 and a bottom buckling plate mechanism connected with the front side plate 1, the upper buckling plate mechanism is provided with buckling grooves 51 and buckling

tongues

52 and 53, the bottom buckling plate mechanism is provided with a triangular buckling plate 101,

buckling grooves

102 and 103 and a flange 104, the triangular buckling plate 101 is divided into two sections through a pressing crease line and is bent inwards to form a triangular reverse buckle, when an upper buckling plate 5 of the top cover of the box is inserted into the inner side of the bottom buckling plate 10, the

buckling tongues

52 and 53 are inserted into the

buckling grooves

102 and 103 on the bottom buckling plate, and the buckling grooves 51 in the middle of the upper buckling plate and the triangular reverse buckle formed by the triangular buckling plate 101 are locked with each other.

The invention has the advantages that:

1 the aircraft box of the invention is an integrated structure, can meet the packaging requirement without using adhesive tape, reduces the noise, and improves the environmental protection

The buckle device of 2 box has simple design and one-step locking, reduces labor intensity

The buckling device of the 3 > box adopts an inner buckling design, thereby improving the safety

Appropriate changes and modifications to the embodiments described above will become apparent to those skilled in the art from the disclosure and teachings of the foregoing description. Therefore, the present invention is not limited to the specific embodiments disclosed and described above, and some modifications and variations of the present invention should fall within the scope of the claims of the present invention. Furthermore, although specific terms are employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation.

Claims

1. A buckle-type aircraft box characterized by comprising: go up buckle, lamina tecti, left side apron, right side apron, bottom plate, preceding curb plate, posterior lateral plate, left side board, right side board and end buckle, go up buckle, lamina tecti, left side apron, right side apron, posterior lateral plate, bottom plate, preceding curb plate, left side board, right side board and end buckle and pass through the crease and connect as an organic wholely, aircraft box bottom plate is provided with the constant head tank with preceding curb plate junction, aircraft box left side board and right side board both ends are provided with the triangle-shaped joining region, the triangle-shaped joining region at aircraft box left side board both ends and the triangle-shaped joining region at right side board both ends pass through the viscose or bind the bottom connection shaping that realizes the packing carton with the both ends interior plate of preceding curb plate and the both ends interior plate of posterior lateral plate respectively.

2. An aircraft box according to claim 1, wherein: the aircraft box further comprises a buckling device, the buckling device comprises an upper buckling plate mechanism and a bottom buckling plate mechanism, the upper buckling plate mechanism is connected with the top cover plate, the bottom buckling plate mechanism is connected with the front side plate, the upper buckling plate mechanism is provided with a buckling groove and a buckling tongue, the bottom buckling plate mechanism is provided with a triangular buckling plate, the buckling groove and a flange, the triangular buckling plate is divided into two sections through a creasing line and is inwards bent to form a triangular inverted buckle, when the upper buckling plate of the top cover of the box is inserted into the inner side of the bottom buckling plate, the buckling tongue is simultaneously inserted into the buckling groove on the bottom buckling plate, and the buckling groove in the middle of the upper buckling plate and the triangular inverted buckle formed by the triangular buckling plate are mutually locked.

3. An aircraft box according to claim 1, wherein: the outer surface of the aircraft box is provided with a hole line type tearing anti-theft line to facilitate unpacking.