CN213200751U

CN213200751U - Combined aviation case

Info

Publication number: CN213200751U
Application number: CN202021576371.1U
Authority: CN
Inventors: 郭玉峰
Original assignee: Shenzhen Taiminghui Industry Co ltd
Current assignee: Shenzhen Taiminghui Industry Co ltd
Priority date: 2020-07-31
Filing date: 2020-07-31
Publication date: 2021-05-14
Anticipated expiration: 2030-07-31

Abstract

The utility model relates to a combination flight case. The combined aviation case comprises an upper cover, a middle case body and a lower case body, wherein the upper cover is a first cavity with a downward opening, and first handles are arranged on the left side plate and the right side plate of the upper cover; the lower box body is a second cavity with an upward opening, and the bottom of the lower box body is provided with a caster; the middle box body comprises a left box cover and a right box cover, the left box cover and the right box cover are of a U-shaped structure, the left box cover and the right box cover are connected into a hollow shell with an upper opening and a lower opening through the buckling of a first locking component, the hollow shell is connected into a square structure with a first cavity and a second cavity through the buckling of a second locking component, corner balls are arranged at four corners of the square structure, and a second handle is arranged on each side plate of the left box cover and the right box cover. The application provides a combination aviation case passes through opening respectively of a plurality of parts of aviation case for user's perpendicular operation height greatly reduced guarantees that the product accomplishes the loading and unloading in very steady safe environment, easy operation, labour saving and time saving, and is safe convenient.

Description

Combined aviation case

Technical Field

The utility model relates to an aviation case technical field especially relates to a combination aviation case.

Background

Generally, the aviation case consists of an upper cover and a lower cover, and is mainly used for packaging heavy special equipment and the like, and has the functions of storing positions and transporting protection of products. However, when the conventional aviation case is used and packed, the upper cover of the case needs to be lifted to take out the product, which is time-consuming, labor-consuming and poor in safety.

SUMMERY OF THE UTILITY MODEL

The to-be-solved technical problem of the utility model is to provide a combination aviation case that loading and unloading are convenient, factor of safety is high.

For realizing the purpose of the utility model, the utility model adopts the following technical scheme:

a combined aviation box comprises an upper cover, a middle box body and a lower box body, wherein the upper cover is a first cavity with a downward opening; the lower box body is a second cavity with an upward opening; the middle box body comprises a left box cover and a right box cover, the left box cover and the right box cover are of U-shaped structures, the left box cover and the right box cover are buckled and connected into a hollow shell with an upper opening and a lower opening through a first locking component, the hollow shell is buckled and connected into a square structure with the first cavity and the second cavity through a second locking component, and four corners of the square structure are provided with corner balls; the bottom of box body is equipped with the truckle down, be equipped with first handle on the left and right sides board of upper cover, left side case lid with be equipped with the second handle on each curb plate of right side case lid.

Compare in traditional two-layer formula aviation case of lifting cap, the combination aviation case that this embodiment provided is based on reducing the loading and unloading potential safety hazard that has the take the altitude product and alleviate operating personnel fatigue strength's novel structure, mainly divide into three layer construction about, open about still in the intermediate level, open respectively through a plurality of parts of aviation case, user's perpendicular operating height greatly reduced for the loading and unloading can be accomplished in very steady safe environment to the product, and easy operation, labour saving and time saving, it is safe convenient.

In one embodiment, the first locking component and the second locking component each include a plurality of connecting locks, and the connecting locks are butterfly locks.

In one embodiment, the hollow shell, the first cavity and the second cavity are provided with straight corner protectors at corners.

Drawings

FIG. 1 is a front-to-back view of a combination flight box in one embodiment;

figure 2 is a side view of the assembled flight box of figure 1.

Detailed Description

In order to facilitate understanding of the present invention, the present invention will be described more fully hereinafter with reference to the accompanying drawings. Preferred embodiments of the present invention are shown in the drawings. The invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise. In the description of the present invention, "a plurality" means at least one, e.g., one, two, etc., unless specifically limited otherwise.

It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only and do not represent the only embodiments.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the methods or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

Referring to fig. 1 and 2, the present embodiment provides a combined aviation case, which includes an upper cover 100, a middle case 200, and a lower case 300, wherein the upper cover 100 is a first cavity with a downward opening; the lower case 300 is a second cavity with an upward opening; the middle box body 200 comprises a left box cover 210 and a right box cover 220, the left box cover 210 and the right box cover 220 are U-shaped structures, the left box cover 210 and the right box cover 220 are connected into a hollow shell with an upper opening and a lower opening through a first locking component 212 in a buckling mode, the hollow shell is connected into a square structure through a second locking component 214 in a buckling mode between the hollow shell and the first cavity and between the hollow shell and the second cavity, specifically, the first locking component 212 and the second locking component 214 both comprise a plurality of connecting lock catches, and the connecting lock catches are butterfly locks.

In the embodiment, the corner balls 500 are arranged at four corners of the square structure, and the corner balls 500 can provide the anti-collision performance of the flight box and protect the flight box; the bottom of the lower case 300 is provided with casters 400, the left and right side plates of the upper cover 100 are provided with first handles 110, and the side plates of the left case cover 210 and the right case cover 220 are provided with second handles 216, so that the suitcase can be conveniently moved.

Furthermore, the corners of the hollow shell and the first and second cavities may further be provided with a straight corner bead 600, and the arrangement of the straight corner bead 600 may effectively prevent the abrasion between the middle box 200 and the upper cover 100 and between the middle box 300 and the lower box 300.

When a user wants to take out a product stored in the combined aviation case provided by the embodiment, the second locking assembly 214 between the middle case 200 and the upper cover 100 can be firstly opened, and the upper cover 100 can be taken down through the first handle 110 on the upper cover 100; then, the first latch assembly 212 between the left box cover 210 and the right box cover 220 and the second latch assembly 214 between the middle box body 200 and the lower box body 100 are sequentially opened, and the left box cover 210 and the right box cover 220 are respectively taken down through the second pull handles 216 on the left box cover 210 and the right box cover 220; the user can then store the product on the lower case 300 to remove it. The operation steps of the user for storing the product through the combined flight box provided by the embodiment are the same as the principle of the operation steps of the product taking out, and the details are not repeated in the embodiment.

The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.

The above-mentioned embodiments only represent some embodiments of the present invention, and the description thereof is specific and detailed, but not to be construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the appended claims.

Claims

1. The combined aviation case is characterized by comprising an upper cover, a middle case body and a lower case body, wherein the upper cover is a first cavity with a downward opening; the lower box body is a second cavity with an upward opening; the middle box body comprises a left box cover and a right box cover, the left box cover and the right box cover are of U-shaped structures, the left box cover and the right box cover are buckled and connected into a hollow shell with an upper opening and a lower opening through a first locking component, the hollow shell is buckled and connected into a square structure with the first cavity and the second cavity through a second locking component, and four corners of the square structure are provided with corner balls; the bottom of box body is equipped with the truckle down, be equipped with first handle on the left and right sides board of upper cover, left side case lid with be equipped with the second handle on each curb plate of right side case lid.

2. The sectional aviation case of claim 1, wherein said first latch assembly and said second latch assembly each comprise a plurality of connecting latches, said connecting latches being butterfly locks.

3. The combination flight case of claim 1, wherein the hollow shell and the corners of the first and second cavities are provided with straight corner protectors.