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On-orbit repeated locking and releasing mechanism for space

A technology for repeatedly locking and releasing mechanisms, which is applied in the docking device of aerospace vehicles, etc., can solve the problems of non-reusable use and excessive impact, and achieve the effect of simple structure, small impact and good controllability

Inactive Publication Date: 2017-05-03
赵士野
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In my country, although many technical achievements and engineering applications have been made in the field of spacecraft connection and separation mechanisms in recent years, the research on large-load low-impact repetitive locking and releasing mechanisms for on-orbit applications has not yet been carried out, and the existing locks The tight release mechanism is not reusable and has the problem of excessive shock during release

Method used

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  • On-orbit repeated locking and releasing mechanism for space

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Embodiment Construction

[0012] combine figure 1 , figure 2 , a space-on-rail repetitive locking and releasing mechanism in this embodiment includes a locking trunnion mechanism, a compression hook mechanism, a locking base mechanism, a crank rocker mechanism and a drive gear mechanism. The locking trunnion mechanism is arranged on the lock Tighten the upper end of the base mechanism, and the driving gear mechanism is respectively connected with the pressing lock hook mechanism and the crank rocker mechanism; the locking base mechanism includes a base 4, the upper end of the base 4 is provided with a V-shaped groove, and the middle part of the base 4 is provided with Mechanism accommodating chamber; the locking trunnion mechanism includes a trunnion 12, and the lower end of the trunnion 12 is arranged in a V-shaped groove on the base 4; the pressing lock hook mechanism includes a lock hook gear 7, a lock hook body 8, The first locking hook horizontal axis 9, the second cam 16, the second micro switc...

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Abstract

The invention relates to a repeated locking and releasing mechanism, in particular to an on-orbit repeated locking and releasing mechanism for space, and aims to solve the problem of repeated on-orbit locking and releasing of a large-scale actual load in a spacecraft. The on-orbit repeated locking and releasing mechanism comprises a trunnion locking mechanism, a lock hook compacting mechanism, a base locking mechanism, a crank and rocker mechanism and a driving gear mechanism, wherein the trunnion locking mechanism is arranged at the upper end of the base locking mechanism; and the driving gear mechanism is connected with the lock hook compacting mechanism and the crank and rocker mechanism. According to the on-orbit repeated locking and releasing mechanism disclosed by the invention, the trunnion locking mechanism, the lock hook compacting mechanism, the base locking mechanism, the crank and rocker mechanism and the driving gear mechanism are arranged in a crossed manner, so that the on-orbit repeated locking and releasing mechanism is simple and compact in structure; all the freedom degrees of a fixed object can be completely limited, and repeated locking can be realized; the maneuverability is good, so that the using requirement of on-orbit locking-releasing-relocking can be met. The on-orbit repeated locking and releasing mechanism disclosed by the invention is suitable for the technical field of aerospace and the technical field of electromechanical integration.

Description

technical field [0001] The invention relates to a repetitive locking and releasing mechanism, in particular to a space-on-rail repetitive locking and releasing mechanism. Background technique [0002] In the field of aerospace, pyrotechnic devices such as explosive bolts and pyrotechnic cutters are mostly used for the connection and separation of spacecraft and payloads. Although they have the characteristics of simple structure and high reliability, they cannot achieve the function of repeated locking on orbit. The huge impact generated by the separation has a serious impact on the attitude and precision control of the space manipulation platform. [0003] In recent years, with the development of space station construction and space detection technology, the space-to-earth shuttle system needs to lock-release-relock the transported large-scale and heavy-duty materials. There are no space control platforms in orbit. Mission requirements for shock release of delicate payload...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/64
Inventor 赵士野
Owner 赵士野
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