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Air cargo binding device

A technology of air freight and binding device, which is applied in the field of binding equipment, which can solve the problems of cargo damage, easy loosening, and detachment, and achieve the effects of reducing labor intensity, saving time and effort, and improving work efficiency

Pending Publication Date: 2022-07-26
浙江盛元航空器材有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the existing air cargo binding fixtures usually cannot fasten the binding straps during the ascent and descent of the aircraft, and the bound goods are easy to break away from the binding fixtures, thereby causing the goods to scatter and the space between the goods. Collision can easily cause damage to the cargo; if the cargo is scattered seriously, it will lead to an unstable center of gravity of the aircraft, which will greatly increase the hidden dangers of flight and often cause major accidents
The existing binding device has the disadvantages of inconvenient operation, time-consuming and labor-intensive, and easy loosening when binding goods

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0035] Please refer to Figure 1 to Figure 5 , this embodiment provides an air cargo binding device, which includes an eccentric shaft 110, a locking buckle 120 and a mounting seat 100 with an installation groove, the eccentric shaft 110 is fixedly installed in the installation groove, and the locking buckle 120 is connected to the eccentric shaft 110 through the eccentric shaft 110. The mounting seat 100 is rotatably connected; when the locking buckle 120 rotates to the first preset position, a first gap 130 is formed between the eccentric shaft 110 and the locking buckle 120 for the strap to pass through; when the locking buckle 120 rotates to the first In two preset positions, a second gap for clamping the strap is formed between the eccentric shaft 110 and the locking buckle 120 .

[0036]In this embodiment, the mounting seat 100 , the eccentric shaft 110 , the locking shaft 121 and the connecting arm 122 are all made of alloy steel. This is because the alloy steel has hi...

Embodiment 2

[0043] Please refer to Figure 1 to Figure 5 , this embodiment proposes based on the technical solution of Embodiment 1: it also includes a switch assembly for connecting the locking buckle 120 and the mounting seat 100 , and the switch assembly includes a limit plate 150 , an elastic member 170 and a locking plate 160 , the two connecting The arms 122 are respectively disposed at both ends of the limit plate 150 , the locking plate 160 is slidably connected with the connecting arm 122 , the elastic member 170 is disposed between the limit plate 150 and the locking plate 160 , and the elastic member 170 is in the compression direction or the extension direction It is consistent with the sliding direction of the locking plate 160 ;

[0044] In this embodiment, the limiting plate 150 and the locking plate 160 are also made of alloy steel, and both have a J shape. The two connecting arms 122 are connected by the horizontal part of the limiting plate 150 . Lock tongues 161 are p...

Embodiment 3

[0046] This embodiment proposes based on the technical solution of Embodiment 1: the mounting seat 100 and the eccentric shaft 110 are integrally formed.

[0047] In this embodiment, the one-piece molding process is mainly used in the manufacturing industry, which means that a certain part is made in one processing, and there is no need to do secondary or more processing, and the whole process can complete the manufacture of a certain part in one process. Integrated molding and non-integrated molding are two different production processes. The manufactured product or part is a whole without any connection. Compared with non-integrated molding, it has better quality, higher strength, superior safety performance, and is more durable. long. The mounting seat 100 and the eccentric shaft 110 can be integrally formed by 3D printing technology, and the structure is stable and firm; the production process is few, and the production cost is low.

[0048] To sum up, the embodiment of t...

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PUM

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Abstract

The invention provides an air cargo binding device, and relates to the technical field of binding devices. The device comprises an eccentric shaft, a locking buckle and a mounting seat with a mounting groove, the eccentric shaft is fixedly mounted in the mounting groove, and the locking buckle is rotationally connected with the mounting seat through the eccentric shaft; when the locking buckle rotates to a first preset position, a first gap for the bandage to pass through is formed between the eccentric shaft and the locking buckle; and when the locking buckle rotates to a second preset position, a second gap for clamping the bandage is formed between the eccentric shaft and the locking buckle. After goods are wound by the binding belt, the binding belt is firmly locked through the binding device, loosening is prevented, and the binding fixity of the goods is enhanced; in addition, the device is simple in structure, reasonable in design and more convenient to operate.

Description

technical field [0001] The present invention relates to the technical field of binding appliances, in particular, to an air cargo binding device. Background technique [0002] Binding and fixing device is a particularly important fixing tool in the transportation of goods. The binding and fixing device belt is also called a cargo trap, which is used to fix the goods during the transportation and movement of the goods. They are tightly locked and will not fall off. It is safe, reliable, light, simple to operate, and has the advantages of protecting objects from damage. [0003] In air freight, the goods must be fixed when they are placed to ensure that the goods will not be loosened during air transportation, thereby ensuring the safety of the transportation process. However, during the ascent and descent of the aircraft, the existing air cargo lashing and fixing devices usually cannot fasten the lashing straps, and the bundled cargo is easily detached from the bundling and ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B65D63/16
CPCB65D63/16
Inventor 王俊
Owner 浙江盛元航空器材有限公司
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