A missile spreader capable of quick adjustment and automatic locking

An automatic locking and spreader technology, applied in the directions of transportation and packaging, load hanging components, etc., can solve the problems of time-consuming and labor-intensive, poor adjustment ability and high safety, and achieve the effect of ensuring lifting

Active Publication Date: 2016-08-24
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] There are many ways to lift missiles. Previous missile spreaders are either simple to operate but poor in safety, or high in safety but complicated in operation.
Moreover, the adjustment ability of the previous missile spreader was poor. When the missile was hoisted in different states, the state adjustment of the spreader was time-consuming and labor-intensive.

Method used

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  • A missile spreader capable of quick adjustment and automatic locking
  • A missile spreader capable of quick adjustment and automatic locking
  • A missile spreader capable of quick adjustment and automatic locking

Examples

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Embodiment Construction

[0016] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments. The following examples are only used to illustrate the present invention, and are not intended to limit the protection scope of the present invention.

[0017] refer to figure 1 , a missile spreader that can quickly adjust the state and automatically lock according to the present invention, the missile spreader includes a spreader main beam 2, a positioning device 3, a lifting ring 4, a front lifting block 1 and a rear safety device 5, and a positioning device 3 It is arranged under the lifting ring 4, and the positioning device 3 fixes the lifting ring 4 on the specific position of the spreader main beam 2. A plurality of positioning holes 6 are arranged on one side of the spreader main beam 2, and the plurality of positioning holes 6 correspond to different types of missiles. At the position of the center of gravity, the front lifting block 1 ...

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Abstract

The invention discloses a missile lifting appliance with a quick state regulation function and an automatic locking function. The missile lifting appliance comprises a lifting appliance girder, a positioning device, a lifting ring, a front lifting block and a rear safety device, wherein the positioning device is arranged below the lifting ring, and is used for fixing the lifting ring at a specific position of the lifting appliance girder; a plurality of positioning holes are formed in one side of the lifting appliance girder and respectively correspond to the centre-of-gravity positions of missiles of different types; the front lifting block and the rear safety device are respectively arranged at two ends of the lifting appliance girder. The missile lifting appliance is easy to operate and high in lifting safety, and has the advantage that quick regulation is realized.

Description

technical field [0001] The invention relates to a missile sling, in particular to a missile sling capable of rapidly adjusting the state and automatically locking. Background technique [0002] There are various lifting methods for missiles. The previous missile slings were either simple to operate but poor in safety, or high in safety but complicated in operation. Moreover, the adjustment ability of the previous missile spreader is poor. When the missile is hoisted in different states, the state adjustment of the spreader is time-consuming and labor-intensive. Therefore, it is necessary to provide a new technical solution to solve the above problems. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide a missile spreader that can quickly adjust the state and automatically lock. [0004] For solving the technical problem of the present invention, the technical scheme that the present invention adopts is: [0005] A...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B66C1/22
CPCB66C1/22
Inventor 李新武罗云张红余孙春春熊志艳刘朝宏邹志强杨龙军方源罗敏芳马威章伟袁素娇高欣舒婷
Owner JIANGXI HONGDU AVIATION IND GRP
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