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Satellite Universal Force Balance Hoisting System

A type of force and satellite technology, applied in the field of satellite hoisting system, can solve the problems that the cross spreader cannot meet the requirements of model versatility, the cross spreader cannot be used for satellite lifting, and the device cannot be used as a spreader alone, etc. Save, save floor space, and facilitate transportation

Active Publication Date: 2020-07-14
SHANGHAI INST OF SATELLITE EQUIP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] 1) Repeated adjustment of the lifting ring screw, the adjustment efficiency is low, the risk of satellite operation is increased, and the uniform force cannot be guaranteed quantitatively;
[0005] 2) The cross spreader cannot be used for hoisting satellites whose centroid and centroid obviously do not coincide;
[0006] 3) Cable-stayed slings are required above the cross spreader, which puts forward higher requirements for the hanging height of the factory building;
[0007] 4) The current cross spreader cannot meet the requirements of model versatility
Adding a uniform force device at the lower end of the ordinary satellite spreader can effectively solve the problem of uneven force on the satellite spreader, but this device cannot be used alone as a spreader and must be installed under the existing satellite spreader

Method used

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  • Satellite Universal Force Balance Hoisting System
  • Satellite Universal Force Balance Hoisting System
  • Satellite Universal Force Balance Hoisting System

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Embodiment Construction

[0038] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0039] Such as figure 1 , figure 2 As shown, a universal force-balanced hoisting system for satellites provided by an embodiment of the present invention includes: a fixed main beam assembly 1 , an expandable main beam assembly 2 , an auxiliary beam assembly 3 , a caster assembly 4 , and an elevator assembly 5 .

[0040] The fixed main beam assembly 1, the expandable main beam assembly 2, and the auxiliary beam assembly 3 all adopt The main body of the cross-section is made of Q345B material, which ...

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Abstract

The invention provides a satellite universal type force balancing lifting system, which comprises a fixed main beam assembly (1), an extensible main beam assembly (2), a auxiliary beam assembly (3), acaster assembly (4), and a lifter assembly (5); the lifter assembly (5) is mounted on the fixed main beam assembly (1) and drives the extensible main beam assembly (2) to move between an extended position and an retracted position. According to the satellite universal type force balancing lifting system, it is ensured that a satellite is lifted multiple times, manual adjustment is not required, all lifting points can maintain uniform stress, and compared with a cross load lifting device, the application range of the satellite universal type force balancing lifting system is wider; and the satellite universal type force balancing lifting system adopts the lever principle to distribute lifting point force of a satellite load lifting device, and is suitable for lifting the satellites with mass centroid and centroid not coinciding obviously.

Description

technical field [0001] The invention relates to a satellite hoisting system, in particular to a general-purpose force balance hoisting system for satellites. Especially the satellite hoisting uniform force device. Background technique [0002] Satellite hoisting generally adopts a cross spreader. During the satellite hoisting process, affected by the status of the spreader and the slight difference in the connection mode between the suspenders and shackles, it cannot guarantee that each lifting point is evenly stressed, so that the satellite structure, the entire satellite, etc. The spreaders are all in a relatively bad stress state. [0003] Usually, before the satellite is hoisted, the sling is found to be slack, and it is considered that the lifting point is not stressed. Generally, the slack of the sling is adjusted by the ring screw of the sling connector until all the slings are in a tensioned state. This method has the following problems: [0004] 1) Repeated adjus...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B66C6/00B66C7/00
CPCB66C6/00B66C7/00
Inventor 赵乐乐张少文施丹邱军马海龙马赫
Owner SHANGHAI INST OF SATELLITE EQUIP
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