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An on-rail mounting system

A technology of installation system and gripping device, which is applied in the field of aerospace, can solve problems such as inability to realize manual on-orbit installation, achieve wide applicability and alleviate the effect of insufficient transportation capacity

Active Publication Date: 2022-07-15
SHANGHAI INST OF SPACE PROPULSION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the above scheme cannot realize the ability of manual on-orbit installation

Method used

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  • An on-rail mounting system
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Embodiment Construction

[0053] The present invention will be described in detail below with reference to 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, for those skilled in the art, several changes and improvements can be made without departing from the inventive concept. These all belong to the protection scope of the present invention.

[0054] like Figure 1 to Figure 7 As shown, an on-rail installation system provided according to the present invention includes a gripping part 1, a main body to be replaced 2, a connecting active end 3 and a connecting passive end 4, wherein the gripping part 1 contains a robotic arm target 5, a manual gripping Holding device 6 and mechanical arm holding device 7, connecting active end 3 includes coarse positioning pin 8, in-position switch 9 and fine positioning pin 10, connecting passive end 4 includes robot...

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Abstract

The invention provides an on-orbit installation system, which can launch products that cannot be launched upwards in a single time from a spacecraft into orbit, and be operated and installed by an astronaut or a mechanical arm on the orbit, so as to realize the on-orbit installation of the product and improve the functional performance of the spacecraft Or extend the life of the spacecraft. The present invention includes a grasping part, a main body to be replaced, a connecting active end and a connecting passive end, wherein the connecting passive end goes up with the spacecraft and hangs in the spacecraft cabin or outside the cabin where it needs to be docked, and the remaining three parts follow the new The spacecraft goes up and is assembled by the astronaut in the cabin and then installed by the robotic arm or the astronaut in orbit. The invention can solve the problem of the limited carrying capacity of the launch vehicle, transport the products that need to go up in multiple times, realize the on-orbit assembly and use of the products through the universal and universal interface design, and has the advantages of wide application range and easy operability. strong features.

Description

technical field [0001] The invention relates to the field of aerospace, in particular to an on-orbit installation system. Background technique [0002] Limited by the carrying capacity of the rocket and the life limit of some consumable products, it is impossible to transport all products into orbit in a single launch or as the product life expires. The spacecraft already in orbit are assembled to improve the functional performance of the spacecraft or extend the life of the spacecraft. [0003] Usually, the spacecraft is designed to integrate the products required for the whole life cycle. However, with the large-scale and long life of the spacecraft, it is gradually impossible to integrate all the products in the whole life cycle at one time. Therefore, it is necessary to provide a A solution that can be replaced and assembled on-orbit to realize the perfect on-orbit assembly level of products. [0004] This solution divides the demand of spacecraft into parts, which can...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G4/00
CPCB64G4/00B64G2004/005
Inventor 康亮杰赵杨王文正肖开阳戴晖李彦达苗鹏
Owner SHANGHAI INST OF SPACE PROPULSION