CN215045510U

CN215045510U - Air transportation container

Info

Publication number: CN215045510U
Application number: CN202121713203.7U
Authority: CN
Inventors: 王志闫; 李国申
Original assignee: Zhinuo Technology Dalian Co ltd
Current assignee: Zhinuo Technology Dalian Co ltd
Priority date: 2021-07-27
Filing date: 2021-07-27
Publication date: 2021-12-07
Anticipated expiration: 2031-07-27

Abstract

The utility model discloses an air freight container, include: the refrigerator comprises a chassis, a top cover, two side wall plates which are transversely arranged and two side door plates which are longitudinally arranged; the chassis comprises a chassis framework, an upper composite plate, a lower composite plate, a flying fixing side tooth and a flying fixing mooring device, wherein the chassis framework comprises a square chassis frame, fork grooves and a rolling bar beam, the fork grooves are welded on the square chassis frame transversely and longitudinally, the rolling bar beam is welded inside the square chassis frame, the upper composite plate and the lower composite plate are riveted on the upper side and the lower side of the chassis framework, the flying fixing mooring device is arranged above the upper composite plate, and the flying fixing side tooth is riveted on the outer side of the square chassis frame. The utility model solves the problem that large goods can not be carried and moored during air transportation, the large goods can be loaded in the box firstly, and then the box body is arranged on the airplane, thereby greatly improving the loading and mooring efficiency; the utility model discloses rational in infrastructure, dependable performance, loading are moored efficiently, are applicable to the air freight of big, medium and small size goods and bulk cargo and load.

Description

Air transportation container

Technical Field

The utility model relates to a packing box technical field provides an air freight container very much.

Background

When goods are transported by air, special boxes or trays for air transportation are usually used for packaging and then air transportation, the existing air transportation box body and trays have small bearing capacity and cannot load larger and heavier goods, and the loading volume is too small when bulk goods are loaded, so that the internal height space of a cabin is wasted; when large goods are transported by air, the large goods cannot be fixed on the large goods, so the large goods need to be directly loaded on an airplane for fixing, the loading process is long due to the mode, a fixed mooring mode is not available, and a large transport container matched with a transport plane for use is not available at present.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an air freight container can effectual solution above-mentioned problem.

The technical scheme of the utility model is that: an air cargo container comprising: a chassis 100, a top cover 200, two side wall plates 300 arranged transversely, and two side door 400 arranged longitudinally; the chassis 100 comprises a chassis framework 101, an upper composite plate 102, a lower composite plate 103, a flight fixing side tooth 104 and a flight fixing mooring device 105, the chassis framework 101 comprises a square chassis framework 101a, fork grooves 101b and rolling bar beams 101c, the fork grooves 101b are welded on the square chassis framework 101a transversely and longitudinally, the rolling bar beams 101c are welded inside, the upper composite plate 102 and the lower composite plate 103 are riveted on the upper side and the lower side of the chassis framework 101, the flight fixing mooring device 105 is arranged above the upper composite plate 102, and the flight fixing side tooth 104 is riveted on the outer side of the square chassis framework 101 a.

Further, the roof 200 comprises a square roof frame 201, a roof skin 202 and a top mooring ring 203, wherein the roof skin 202 is riveted inside the square roof frame 201, and the top mooring ring 203 is riveted outside the square roof frame 201.

Further, the side wall panel 300 includes a side wall panel framework 301, a side wall panel skin 302, and a ventilator 303, where the side wall panel skin 302 is riveted to the side wall panel framework 301, and the ventilator 303 is disposed on the side wall panel skin 302.

Further, the box door 400 is a folding door, and a bottom mooring ring 401 is riveted below the box door 400.

Further, the upper composite plate 102 and the lower composite plate 103 are formed by bonding a composite plate frame, a middle core material, and upper and lower skins.

Further, the middle core material adopts a BSLSA balsa core material or a honeycomb core material.

Further, the flight fixed side tooth 104 has a tooth space depth of 44mm, a tooth space width of 69.5mm, and a tooth space center distance of 254 mm.

The utility model discloses following profitable effect has:

the utility model solves the problem that large goods can not be carried and moored during air transportation, the large goods can be loaded in the box firstly, and then the box body is arranged on the airplane, thereby greatly improving the loading and mooring efficiency; the utility model discloses rational in infrastructure, dependable performance, loading are moored efficiently, are applicable to the air freight of big, medium and small size goods and bulk cargo and load.

Drawings

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

fig. 2 is a schematic structural view (front side) of the middle chassis of the present invention;

fig. 3 is a schematic structural view (back side) of the middle chassis of the present invention;

FIG. 4 is a schematic structural view of a middle flying fixed side tooth of the present invention;

FIG. 5 is a schematic structural view of the middle chassis frame of the present invention;

fig. 6 is a schematic structural view of an upper and lower composite plate frame according to the present invention;

FIG. 7 is a schematic structural view of the middle and lower composite board frame of the present invention;

in the figure: 100. a chassis; 101. a chassis frame; 101a, a square chassis frame; 101b, fork grooves; 101c, a roller beam; 102. putting a composite board; 103. a lower composite board; 104. flight fixed side teeth; 105. a flight securing mooring device; 200. a top cover; 201. a square header frame; 202. a top cover skin; 203. a top mooring ring; 300. a side wall panel; 301. a sidewall plate skeleton; 302. a sidewall plate skin; 303. a ventilator; 400. a box door; 401. the bottom is tied to the ring.

Detailed Description

The present invention will be described in detail with reference to the accompanying drawings and examples.

As shown in fig. 1 to 7, an air freight container includes: a bottom chassis 100, a top cover 200, two side wall plates 300 arranged laterally, and two side door 400 arranged longitudinally.

The chassis 100 comprises a chassis framework 101, an upper composite plate 102, a lower composite plate 103, a flight fixing side tooth 104 and a flight fixing mooring device 105; the chassis framework 101 comprises a square chassis frame 101a, fork grooves 101b and a roller beam 101c, the fork grooves 101b are welded on the square chassis frame 101a in the transverse direction and the longitudinal direction, and the roller beam 101c is welded inside the square chassis frame 101 a; an upper composite plate 102 and a lower composite plate 103 are riveted on the upper side and the lower side of the chassis framework 101, a flying fixing mooring device 105 is arranged above the upper composite plate 102, and a flying fixing side tooth 104 is riveted on the outer side of the square chassis framework 101 a.

In the embodiment of the present invention, the top cover 200 includes a square top cover frame 201, a top cover skin 202 and a top mooring ring 203, the top cover skin 202 is riveted in the square top cover frame 201, and the top mooring ring 203 is riveted outside the square top cover frame 201, so as to perform the whole box mooring.

In the embodiment of the present invention, the side wall panel 300 includes a side wall panel frame 301, a side wall panel skin 302, and a ventilator 303, the side wall panel skin 302 is riveted to the side wall panel frame 301, and the ventilator 303 is disposed on the side wall panel skin 302; the inside riveting of lateral wall board skeleton 301 has inside mooring ring for the goods is moored.

In the embodiment of the present invention, the box door 400 is a folding door, which facilitates the rapid loading and unloading of goods; a bottom mooring ring 401 is riveted below the box door 400 to perform overall box mooring.

In the embodiment of the present invention, the upper composite plate 102 and the lower composite plate 103 are formed by bonding a composite plate frame, a middle core material, and upper and lower skins.

In the embodiments of the present invention, the middle core material is BSLSA balsa wood core material or honeycomb core material.

In the embodiment of the utility model, the tooth socket degree of depth of flight fixed side tooth 104 is 44mm, and the tooth socket width is 69.5mm, and tooth's socket central distance is 254mm, and flight fixed side tooth 104 is formed by 7 series aluminum products preparation, uses with the cooperation of conveyer locking mechanical system.

The utility model discloses the box dead weight is 1000kg, and the rated load is 8000kg, and the overload is 17000 kg.

The above embodiments are only for illustrating the technical concept and features of the present invention, and the purpose of the embodiments is to enable people skilled in the art to understand the contents of the present invention and to implement the present invention, which cannot limit the protection scope of the present invention. All equivalent changes and modifications made according to the spirit of the present invention should be covered by the protection scope of the present invention.

Claims

1. An air cargo container, comprising: the refrigerator comprises a chassis (100), a top cover (200), two side wall plates (300) which are transversely arranged and two side door (400) which are longitudinally arranged; the chassis (100) comprises a chassis framework (101), an upper composite plate (102), a lower composite plate (103), a flight fixing side tooth (104) and a flight fixing mooring device (105), wherein the chassis framework (101) comprises a square chassis frame (101a), fork grooves (101b) and a rolling bar beam (101c), the fork grooves (101b) are welded transversely and longitudinally in the square chassis frame (101a), the rolling bar beam (101c) is welded internally, the upper side and the lower side of the chassis frame (101) are riveted with the upper composite plate (102) and the lower composite plate (103), the flight fixing mooring device (105) is arranged above the upper composite plate (102), and the flight fixing side tooth (104) is riveted outside the square chassis frame (101 a).

2. An air container according to claim 1, characterized in that the roof (200) comprises a square roof frame (201), a roof skin (202) and a top mooring ring (203), the roof skin (202) being riveted into the square roof frame (201), the top mooring ring (203) being riveted outside the square roof frame (201).

3. An air container according to claim 1, characterised in that the side wall panels (300) comprise a side wall panel carcass (301), a side wall panel skin (302) and a ventilator (303), the side wall panel skin (302) being riveted to the side wall panel carcass (301), the ventilator (303) being provided in the side wall panel skin (302).

4. An air container according to claim 1, characterized in that said door (400) is a folding door, and that a bottom mooring ring (401) is riveted under said door (400).

5. An air container according to claim 1, characterized in that said upper (102) and lower (103) composite panels are formed by bonding of composite panel frames, intermediate cores and upper and lower skins.

6. An air container according to claim 5 wherein said intermediate core is a BSLSA balsa core or a honeycomb core.

7. An air container according to claim 1, wherein said flight securing sideteeth (104) have a gullet depth of 44mm, a gullet width of 69.5mm and a gullet centre distance of 254 mm.