CN215152305U

CN215152305U - Folding auxiliary tool of aircraft box

Info

Publication number: CN215152305U
Application number: CN202121594379.5U
Authority: CN
Inventors: 高阳; 范玉婷
Original assignee: Dongguan Haisha Filter Co ltd
Current assignee: Dongguan Haisha Filter Co ltd
Priority date: 2021-07-13
Filing date: 2021-07-13
Publication date: 2021-12-14
Anticipated expiration: 2031-07-13

Abstract

The utility model relates to an aircraft box shaping technical field, concretely relates to folding supplementary tool of aircraft box, include the base plate, install a plurality of baffles on the base plate, it is a plurality of the region that the baffle encloses is the same with aircraft box bottom plate size, baffle slidable mounting is in so that it is a plurality of on the base plate the aircraft box bottom plate of the not unidimensional of regional adaptation that the baffle encloses to the realization only needs an supplementary tool just can assist folding unidimensional aircraft box, avoids changing the material waste and the high cost that supplementary tool caused.

Description

Folding auxiliary tool of aircraft box

Technical Field

The utility model relates to an aircraft box shaping technical field, concretely relates to supplementary tool is folded to aircraft box.

Background

The aircraft box is one of the packing forms of avoiding mechanical parts to damage in the transportation, belongs to a carton, and because the appearance that its expansion is exactly like the aircraft and gets its name, the preparation raw materials are corrugated paper, often is used for express delivery packing and transport. Because of the relatively low cost and the high cost performance of the aircraft box, more and more enterprises select the aircraft box to deliver commodities as a packing box, and the aircraft box needs to be folded by a positioning jig when the commodities are packed manually at present.

The folding supplementary tool of current aircraft box includes the base plate and sets up a plurality of cuboid structure baffles on the base plate, and a plurality of baffles enclose into the region the same with the bottom plate size of aircraft box. When folding aircraft box, only need aim at the region that a plurality of baffles surrounded with the bottom plate and place, then both hands are put and are pushed down the bottom plate of aircraft box in the left and right sides board of aircraft box and bottom plate junction, in-process pushing down the bottom plate, the medial surface that each curb plate of aircraft box is pasting the baffle is landing downwards, when pushing down bottom plate to the base plate on, each curb plate of aircraft box is perpendicular with the bottom plate, convenient shaping when follow-up manual folding aircraft box (as shown in fig. 1, the base plate is designated to reference numeral 1, the baffle is designated to reference numeral 2, reference numeral 22 designates the medial surface, reference numeral 23 designates the up end).

However, the baffle of the folding auxiliary tool of aircraft box and base plate fixed mounting at present can only assist folding aircraft box of a size, if want to fold aircraft box of not unidimensional and need change auxiliary tool, complex operation and with high costs.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to prior art not enough, provide a can assist folding not unidimensional aircraft box's folding supplementary tool of aircraft box.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides an aircraft box folds supplementary tool, includes the base plate, installs a plurality of baffles on the base plate, and is a plurality of the region that the baffle encloses is the same with aircraft box bottom plate size, baffle slidable mounting is in so that it is a plurality of on the base plate the not unidimensional aircraft box bottom plate of regional adaptation that the baffle encloses.

In the above technical scheme, the base plate is provided with a chute, and the baffle is connected with the base plate through the chute in a sliding manner.

In the technical scheme, an inclined plane is processed on the inner side surface of each baffle, and the inclined plane extends to the upper end surface of the baffle from the inner side surface of the baffle.

In the technical scheme, the upper end face of the baffle is a convex cambered surface.

In the above technical scheme, the inclined plane is a linear inclined plane, and an included angle between the inclined plane and the substrate is 40-50 degrees.

Preferably, the included angle between the inclined plane and the substrate is 45 °.

In the above technical scheme, four bases for supporting the substrate are installed below the substrate.

The utility model has the advantages that:

the utility model discloses an auxiliary tool is folded to aircraft box because baffle slidable mounting can be according to the position of aircraft box bottom plate size adjustment baffle on the base plate to make the not unidimensional aircraft box bottom plate of regional adaptation that a plurality of baffles enclose, thereby realize only needing an auxiliary tool just can assist folding not unidimensional aircraft box, avoid changing the material waste and the high cost that auxiliary tool caused.

Drawings

The drawings are only for purposes of illustrating the preferred embodiments and are not to be construed as limiting the invention, and the same reference numbers are used throughout the drawings to identify the same parts.

Fig. 1 is a schematic structural view of an auxiliary folding jig for an airplane box in the prior art.

Fig. 2 is a schematic structural view of an auxiliary folding jig of an airplane box according to an embodiment.

FIG. 3 is a side view of the baffle in the example.

Reference numerals: the base plate 1, the baffle 2, the inclined plane 21, the medial surface 22, the up end 23, the spout 3, the base 4.

Detailed Description

Exemplary embodiments of the present invention will be described in more detail below with reference to the accompanying drawings. While exemplary embodiments of the invention are shown in the drawings, it should be understood that the invention can be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.

The folding supplementary tool of aircraft box of this embodiment, as shown in fig. 2, including base plate 1, install a plurality of baffles 2 on base plate 1, the region that a plurality of baffles 2 surround is the same with the size of the chassis of aircraft box. The bottom plate of the aircraft box that will need to fold aligns the region that a plurality of baffles 2 surrounded, then pushes down the bottom plate near the junction of the bottom plate of aircraft box and curb plate, when the bottom plate pushed down to base plate 1 on, the medial surface 22 of baffle 2 is hugged closely to each side of bottom plate to guarantee that the bottom plate of aircraft box is perpendicular with the curb plate, make things convenient for follow-up fold forming.

Further, in order to avoid baffle 2 to influence gliding speed or the fish tail curb plate of the curb plate of aircraft box when pushing down the bottom plate, the medial surface 22 of every baffle 2 in this embodiment has all processed an inclined plane 21, inclined plane 21 extends to the up end 23 of baffle 2 from the medial surface 22 of baffle 2, make inclined plane 21 and medial surface 22's contained angle be the obtuse angle, when pushing down the bottom plate, each curb plate of aircraft box can be quick pass through medial surface 22 and glide to from inclined plane 21, inclined plane 21 can not block the aircraft box curb plate with the intersection of medial surface 22, thereby improve the speed that aircraft box curb plate glided, and can not fish tail the curb plate. The inclined plane 21 can be selected to be a linear inclined plane 21, the included angle between the inclined plane 21 and the substrate 1 is 40-50 degrees, the preferred included angle is 45 degrees, the angle can be selected to ensure that the aircraft box cannot be scratched, and the side plate of the aircraft box can have a moderate gliding speed.

In order to further avoid the risk of scratching the side plates, the upper end surface 23 of the baffle 2 is provided as a convex arc surface, as shown in fig. 3.

The folding supplementary tool of aircraft box of this embodiment, as the structure shown in fig. 2, base plate 1 is equipped with spout 3, and baffle 2 passes through spout 3 sliding connection with base plate 1, and the gliding mode of baffle 2 can be: the manual movable baffle 2 slides on the chute 3 to a position matched with the bottom plate of the airplane box; the baffle 2 is pushed to slide on the chute 3 by a pushing device, which can be selected as a cylinder assembly.

Further, the pushing device can be disposed at a side portion of the auxiliary fixture, or at a bottom portion of the auxiliary fixture. When thrust unit sets up in the bottom of supplementary tool, if thrust unit position sets up inappropriately, cause supplementary tool unbalance easily, consequently, install four bases 4 that are used for supporting base plate 1 in the below of base plate 1 to make supplementary tool steadily place.

It should be finally noted that the above embodiments are only intended to illustrate the technical solutions of the present invention, and not to limit the scope of the present invention, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the technical solutions of the present invention can be modified or replaced with equivalents without departing from the spirit and scope of the technical solutions of the present invention.

Claims

1. The utility model provides an auxiliary tool is folded to aircraft box, includes the base plate, installs a plurality of baffles on the base plate, and is a plurality of the region that the baffle encloses is the same with aircraft box bottom plate size, its characterized in that: the baffles are slidably mounted on the base plate so that the area defined by the baffles can be adapted to airplane box bottom plates with different sizes.

2. The auxiliary tool is folded to aircraft box of claim 1, characterized in that: the base plate is provided with a sliding groove, and the baffle is connected with the base plate in a sliding mode through the sliding groove.

3. The auxiliary tool of claim 1 or 2, wherein: the inner side surface of each baffle is provided with an inclined surface, and the inclined surface extends to the upper end surface of the baffle from the inner side surface of the baffle.

4. The auxiliary tool is folded to aircraft box of claim 3, characterized in that: the upper end surface of the baffle is a convex cambered surface.

5. The auxiliary tool is folded to aircraft box of claim 3, characterized in that: the inclined plane is a linear inclined plane, and the inclined plane and the substrate form an included angle of 40-50 degrees.

6. The auxiliary tool is folded to aircraft box of claim 5, characterized in that: the inclined plane and the substrate form an included angle of 45 degrees.

7. The auxiliary tool is folded to aircraft box of claim 1, characterized in that: four bases for supporting the substrate are installed below the substrate.