A Linked Space Repeated Locking and Release Mechanism

A technology of repeated locking and releasing mechanism, applied in the aerospace field, can solve problems such as poor reliability and controllability, and achieve the effects of reliable locking and tightening, small impact and simple structure

Active Publication Date: 2017-06-06
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] In order to solve the problem of poor reliability and controllability in the locking process of the existing locking and releasing mechanism, the present invention further proposes a linkage type space repeated locking and releasing mechanism

Method used

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  • A Linked Space Repeated Locking and Release Mechanism
  • A Linked Space Repeated Locking and Release Mechanism

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Experimental program
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Effect test

specific Embodiment approach 1

[0014] Specific implementation mode one: combine figure 1 and figure 2 Describe this embodiment. The interlocking space repetitive locking and releasing mechanism described in this embodiment includes a repeatable locking and releasing mechanism and a linkage driving mechanism. The repeatable locking and releasing mechanism includes a locking mechanism and a locked component. The locking mechanism includes a connecting rod 3, a rocker connecting rod shaft 4, a rocking rod 5, a lock hook rocker shaft 6, a lock hook 8, a locking housing 14, a bearing base 15, a worm 25, a worm wheel 26, a first Transition gear 27, first transition gear shaft 28, second transition gear shaft 29, second transition gear 30, crank gear 31, crank connecting rod shaft 32, rocker shaft 33 and crank gear shaft 34, bearing base 15 is installed in the lock In the tight housing 14, one end of the worm 25 is inserted on the bearing base 15, the other end of the worm 25 passes through the side wall of the ...

specific Embodiment approach 2

[0016] Specific implementation mode two: combination figure 1 and figure 2 Describe this embodiment, the locked mechanism of a linkage type space repeated locking release mechanism described in this embodiment includes a loading rod 9, a loading nut 10, a locked shaft 11 and a locked housing 12, the loading rod 9 Inserted in the locked housing 12, the upper end of the loading rod 9 is connected with the loading nut 10, the lower end of the loading rod 9 is connected with the locked shaft 11, and the locked shaft 11 is articulated with the mouth of the locking hook 8.

[0017] The technical effect of this embodiment is: with such an arrangement, by turning the loading nut 10 , the loading rod 9 can be moved up and down in a straight line, and then the position of the locked shaft 11 can be adjusted. Other components and connections are the same as those in the first embodiment.

specific Embodiment approach 3

[0018] Specific implementation mode three: combination figure 1 and figure 2 Describe this embodiment, the locking mechanism of a linkage type space repetition locking release mechanism described in this embodiment also includes a corner block 1, a single-tooth crank 2 and a micro switch 7, one end of the single-tooth crank 2 and the crank gear 31 Connect, the other end of the single-tooth crank 2 is in contact with the microswitch 7 installed at the installation port on the side wall of the locking housing 14, and the corner block 1 is installed at the installation port on the side wall of the locking housing 14.

[0019] The technical effect of this embodiment is: so set, the micro switch 7 is in contact with the single-tooth crank 2 on the crank gear 22 in the locked state to release the signal to turn off the motor. Other components and connections are the same as those in the first embodiment.

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PUM

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Abstract

The invention relates to a repeated locking and releasing mechanism, in particular to a linkage type space repeated locking and releasing mechanism. The linkage type space repeated locking and releasing mechanism aims at solving the problem that reliability and controllability of an existing locking and releasing mechanism in the locking process are poor. The linkage type space repeated locking and releasing mechanism comprises a repeatable locking and releasing mechanism and a linkage driving mechanism. The repeatable locking and releasing mechanism comprises a locking mechanism and a locked assembly. The locking mechanism comprises a connection rod, a rocker connection rod shaft, a rocker, a lock hook rocker shaft, a lock hook, a locking shell, a bearing base, a worm, a worm gear, a first transition gear, a first transition gear shaft, a second transition gear shaft, a second transition gear, a crank gear, a crank connection rod shaft, a rocker shaft and a crank gear shaft. The linkage type space repeated locking and releasing mechanism is used in the aerospace field.

Description

technical field [0001] The invention relates to a repetitive locking and releasing mechanism, in particular to a linked space repetitive locking and releasing mechanism, which belongs to the field of aerospace. 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 this device has the characteristics of simple structure and high reliability, it cannot realize the on-orbit repeated locking function. The huge impact of pyrotechnic separation has a serious impact on the attitude and precision control of the space control platform. [0003] In recent years, with the development of space station construction and space detection technology, the space-to-earth shuttle system has an increasingly strong demand for locking-release-relocking of transported large-scale, heavy-duty materials and aerospace vehicle doors. There are al...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/22
Inventor 岳洪浩邓宗全杨飞周少程张文星彭金圣
Owner HARBIN INST OF TECH
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