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Shock-free wrapping tape type unlocking separation mechanism

A separation mechanism and wrapping technology, applied in the aerospace field, can solve the problems of large shock response, pollution, high production cost, etc., and achieve the effect of shock absorption

Inactive Publication Date: 2014-12-24
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to propose a non-shock wrapping type unlocking and separating mechanism, which solves the problems of high production cost, large impact response, long working time, small load and pollution existing in the prior art

Method used

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  • Shock-free wrapping tape type unlocking separation mechanism
  • Shock-free wrapping tape type unlocking separation mechanism
  • Shock-free wrapping tape type unlocking separation mechanism

Examples

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Embodiment Construction

[0022] The present invention will be further described below in conjunction with the accompanying drawings.

[0023] See attached figure 1 , attached figure 2 and attached image 3 As shown, the unlocking and separating mechanism of the present invention includes a non-impact connection unlocking assembly 23 and a strap-type separation assembly 24; the connecting bolts 1 of the two non-impact connection unlocking assemblies 23 are connected to the described Tape separation assembly 24 is connected.

[0024] See attached Figure 5 The non-impact connection unlocking assembly 23 includes a connecting bolt 1, a lower baffle plate 2, a mounting seat 3, a separation nut A4, a separation nut B5, a guide cylinder 6, a disconnection shaft 9, a memory alloy cylinder 11, a heating plate 12, a spacer Heat cylinder 10, upper baffle plate 14; said mounting seat 3 is divided into left cavity and right cavity, and a through hole is opened in the middle of said left cavity and said right...

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Abstract

The invention discloses a shock-free wrapping tape type unlocking separation mechanism, belongs to the technical field of aerospace, and aims at solving the problems of high production cost, high shock response, long working time, small load and pollution. Connecting bolts of two shock-free connection unlocking assemblies are connected with a wrapping tape type separation assembly through wrapping tape gaskets and nuts; a memory alloy barrel is heated to be recovered to the original shape; a disconnection shaft is pulled and broken into two parts; an actuation spring pushes a guide barrel to move; connecting bolts are released; and a left wrapping tape and a right wrapping tape are pushed away by a separation spring and separated from an upper supporting seat and a lower supporting seat, so that the upper supporting seat is separated from the lower supporting seat. According to the invention, the three-stage release process is achieved, so that the bearing capacity can be amplified step by step on one hand and the shock response can be minimized through step-by-step release at the same time; a tension spring and the actuation spring can effectively absorb shock generated by brittle failures of the bolts; and the shock-free connection unlocking assemblies can bear a larger clamping force and the wrapping tape type unlocking separation mechanism can bear a large load.

Description

technical field [0001] The invention relates to a non-impact strap-type unlocking and separating mechanism, which belongs to the technical field of aerospace. Background technique [0002] The spacecraft needs a variety of connection and separation mechanisms to realize space connection and unlocking functions, such as the separation of multi-stage launch vehicles, the separation of satellites and rockets, and the deployment of solar wings on satellites or spacecraft. Taking the separation of the satellite and the rocket as an example, since the satellite and the rocket are connected by multiple unlocking mechanisms before separation, multiple unlocking mechanisms are required to be able to carry the vibration load of the launch during the launch process, and multiple unlocking mechanisms are required to be synchronized and low Unlocking with impact or even without impact can realize the separation of star and arrow. Therefore, high requirements are put forward for the carry...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/64
Inventor 曹乃亮杨利伟辛宏伟杨会生李志来
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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