CN217171466U

CN217171466U - Wear-resistant packaging box for missile cabin transportation

Info

Publication number: CN217171466U
Application number: CN202123246357.2U
Authority: CN
Inventors: 黄伟鎔; 吴安德; 吴淑慧
Original assignee: Jiangxi Jinkeli Industry Co ltd
Current assignee: Jiangxi Jinkeli Industry Co ltd
Priority date: 2021-12-22
Filing date: 2021-12-22
Publication date: 2022-08-12
Anticipated expiration: 2031-12-22

Abstract

The utility model discloses an anti-abrasion packing box for missile cabin transportation, which belongs to the technical field of packing boxes and comprises a packing box body, wherein right-angle anti-abrasion plates are arranged at the edge of the packing box body, a plurality of long anti-abrasion plates are arranged on the outer side wall of the packing box body, and anti-abrasion supporting columns are arranged at four corners of the bottom of the packing box body; the bottom is equipped with the support base that has the arc wall in the packing box body, the both sides swing joint who supports the base has the stopper, be equipped with fixing bolt on the stopper, fixing bolt is used for spacing on supporting the base with the stopper, avoids at the in-process of transportation, and the packing box is broken because of wearing and tearing or receive the impact and lead to the packing box broken to reach the missile cabin section to the packing box and protect, stop the stopper through fixing bolt, make the spacing missile cabin section of stopper, avoid at the in-process of transportation, the friction is rocked to the missile cabin section, thereby play the effect to missile cabin section abrasionproof loss.

Description

Wear-resistant packaging box for missile cabin transportation

Technical Field

The utility model relates to a packing box technical field specifically is a guided missile cabin section is abrasionproof decreases packing box for transportation.

Background

The cabin section is an independent structure formed by dividing each structural section opening of the missile body according to the functions and stress characteristics of each section of the missile body and the requirements of processing, assembling, using, maintaining and the like.

In the process of transporting missile cabins, packing boxes are needed to pack the missile cabins, but the existing packing boxes generally have no anti-abrasion effect, so that the anti-abrasion packing box for transporting the missile cabins is needed.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a guided missile cabin section is abrasionproof decreases packing box for transportation has solved the problem of mentioning in the above-mentioned technical background. In order to achieve the above object, the utility model provides a following technical scheme: an anti-abrasion packing box for missile cabin section transportation comprises a packing box body, wherein right-angle anti-abrasion plates are arranged at the edge of the packing box body, a plurality of long anti-abrasion plates are arranged on the outer side wall of the packing box body, and anti-abrasion supporting columns are arranged at four corners of the bottom of the packing box body;

the bottom is equipped with the support base that has the arc wall in the packing box body, the both sides swing joint of supporting the base has the stopper, be equipped with fixing bolt on the stopper, fixing bolt is used for spacing the stopper on supporting the base.

Further, the right-angle anti-abrasion plate and the long anti-abrasion plate are made of elastic rubber.

Further, a plurality of elastic balls are arranged on the outer side walls of the right-angle wear plate and the long wear plate.

Furthermore, four angular points department at packing box body top also is equipped with the abrasionproof support column, all seted up the fixed orifices on the adjacent both sides wall of abrasionproof support column, and two link up mutually between the fixed orifices.

Furthermore, one end, close to the arc-shaped groove, of the limiting block is provided with an arc-shaped chamfer, and an elastic anti-slip ball is arranged on the arc-shaped chamfer.

To sum up, the utility model discloses following beneficial effect has:

this kind of abrasionproof decreases packing box is used in transportation of guided missile cabin section, through the setting of right angle abrasionproof decreases board and long abrasionproof decreases board, protect the packing box, avoid at the in-process of transportation, the packing box is broken because of wearing and tearing or receive the impact and lead to the packing box broken, thereby reach the guided missile cabin section to protect in the packing box, stop the stopper through fixing bolt, make the spacing guided missile cabin section of stopper, avoid at the in-process of transportation, guided missile cabin section rocks the friction, thereby play the effect to guided missile cabin section abrasionproof decreases.

Through the arrangement of the fixing holes in the supporting base, the packaging box is firmly fixed on a transport vehicle through the fixing ropes, so that the shaking of the packaging box is reduced, and the missile cabin section is protected.

Drawings

Fig. 1 is a schematic perspective view of the present invention;

fig. 2 is a side view of the present invention;

FIG. 3 is a schematic view of the internal structure of the present invention;

fig. 4 is an enlarged schematic view of the position a of the present invention.

In the figure: 1. a packaging box body; 2. a right angle wear plate; 3. a long wear plate; 4. an anti-abrasion support column; 401. a fixing hole; 5. a support base; 501. a limiting block; 502. fixing the bolt; 503. an arc-shaped slot; 504. arc chamfering; 505. an elastic anti-slip ball; 6. an elastic ball.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.

Referring to fig. 1-4, an anti-abrasion packing box for missile cabin transportation comprises a packing box body 1, a right-angle anti-abrasion plate 2 is arranged at the edge of the packing box body 1, the right-angle anti-abrasion plate 2 is divided into two anti-abrasion plates which are vertically and fixedly connected, the two anti-abrasion plates are respectively and fixedly connected to two adjacent side walls of the packing box body 1, the edge of the packing box body 1 is protected through the arrangement of the right-angle anti-abrasion plate 2, a plurality of long anti-abrasion plates 3 are uniformly arranged on the outer side wall of the packing box body 1, the side wall of the packing box body 1 is protected through the arrangement of the long anti-abrasion plates 3, anti-abrasion support columns 4 are arranged at four corners of the bottom of the packing box body 1, the anti-abrasion support columns 4 are used for supporting the packing box body 1, anti-skid grains are arranged at the bottom of the anti-abrasion support columns 4, an arc-shaped groove 503 is arranged at the bottom of the packing box body 1, the shape of the arc-shaped groove 503 corresponds to the shape of the missile cabin, the both sides swing joint that supports base 5 has stopper 501, stopper 501 and the top sliding connection who supports base 5 are equipped with fixing bolt 502 on the stopper 501, and fixing bolt 502 is used for spacing stopper 501 on supporting base 5, and the top that supports base 5 is equipped with the screw hole with fixing bolt 502 looks adaptation.

Right angle abrasionproof decreases board 2 and long abrasionproof decreases board 3 and is the elastic rubber material, plays the protection to the packing box through the elastic rubber material, and right angle abrasionproof decreases and arranges on the lateral wall of board 2 and long abrasionproof decreases board 3 and have a plurality of elastic balls 6, and elastic ball 6 also plays the protection to the packing box. Four angular points department at 1 top of packing box body also is equipped with abrasionproof support column 4, has all seted up fixed orifices 401 on the adjacent both sides wall of abrasionproof support column 4, and link up mutually between two fixed orifices 401. An arc-shaped chamfer 504 is arranged at one end, close to the arc-shaped groove 503, of the limiting block 501, an elastic anti-slip ball 505 is arranged on the arc-shaped chamfer 504, the elastic anti-slip ball 505 is arranged, the missile cabin section is more firmly limited, and the missile cabin section is prevented from being damaged by clamping through the elasticity of the elastic anti-slip ball 505.

The utility model discloses a guided missile cabin section transportation is with application method and theory of operation as follows of abrasionproof packing box, when guided missile cabin section needs to be transported, the operator places guided missile cabin section in arc 503, then the operator removes stopper 501 toward the direction of guided missile cabin section, guided missile cabin section is hugged closely to messenger stopper 501's one end, fixing bolt 502 just in time supports the screw hole on the base 5 to it this moment, then twist fixing bolt 502 into threaded hole, make stopper 501 spacing on supporting base 5, stopper 501 spacing lives guided missile cabin section this moment, make guided missile cabin section spacing in packing box body 1, then pass fixed orifices 401 through fixed rope, make packing box body 1 firmly spacing on the transport vechicle, it rocks to reduce the transport package box, thereby reduced rocking of guided missile cabin section on the way, guided missile cabin section has been protected.

The present embodiment is only for explaining the present invention, and it is not limited to the present invention, and those skilled in the art can make modifications to the present embodiment without inventive contribution as required after reading the present specification, but all of them are protected by patent laws within the scope of the claims of the present invention.

Claims

1. An anti-abrasion packing box for missile cabin section transportation comprises a packing box body (1) and is characterized in that right-angle anti-abrasion plates (2) are arranged at the edge of the packing box body (1), a plurality of long anti-abrasion plates (3) are arranged on the outer side wall of the packing box body (1), and anti-abrasion support columns (4) are arranged at four corners of the bottom of the packing box body (1);

the bottom is equipped with support base (5) that have arc wall (503) in packing box body (1), the both sides swing joint that supports base (5) has stopper (501), be equipped with fixing bolt (502) on stopper (501), fixing bolt (502) are used for spacing stopper (501) on supporting base (5).

2. The wear-resistant packing box for missile bay section transportation of claim 1, wherein: the right-angle wear-resistant plate (2) and the long wear-resistant plate (3) are made of elastic rubber.

3. The wear-resistant packing box for missile bay section transportation of claim 1, wherein: and a plurality of elastic balls (6) are arranged on the outer side walls of the right-angle wear-proof plate (2) and the long wear-proof plate (3).

4. The wear-resistant packing box for missile bay section transportation of claim 1, wherein: four angular points department at packing box body (1) top also are equipped with abrasionproof support column (4), fixed orifices (401) have all been seted up on the both sides wall that abrasionproof support column (4) are adjacent, and two link up mutually between fixed orifices (401).

5. The wear-resistant packing box for missile bay section transportation of claim 1, wherein: an arc-shaped chamfer (504) is arranged at one end, close to the arc-shaped groove (503), of the limiting block (501), and an elastic anti-slip ball (505) is arranged on the arc-shaped chamfer (504).