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Single point flexible compression release device for spacecraft

A technology for releasing devices and spacecraft, which is applied to docking devices for aerospace vehicles, etc., can solve problems such as potential safety hazards, increased cost of ground tests, non-reusable pyrotechnic devices and compression rods, etc., and achieves good economic benefits and low cost Effect

Active Publication Date: 2017-12-15
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] This type of compression and release mechanism has the following limitations: the instantaneous large-scale shock load generated will affect the attitude of the satellite and the sensitive unit, and the corrosive and polluting gas will be generated during the ignition of the pyrotechnic device, which directly uses the explosion of explosives to produce There are certain potential safety hazards in the energy. The pyrotechnic device is a dangerous product, which brings inconvenience to ground storage and use. The cost of the ground test increases due to the non-reusable characteristics of the pyrotechnic device and the compression rod.

Method used

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  • Single point flexible compression release device for spacecraft
  • Single point flexible compression release device for spacecraft
  • Single point flexible compression release device for spacecraft

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Embodiment Construction

[0036] 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 modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0037] In this embodiment, the single-point flexible compression release device for spacecraft provided by the present invention includes a fuse cutter 101, a compression seat 102, a tension cable assembly 103, a moving block 104, and a locking nut 105;

[0038] Wherein, the moving block 104 and the pressing seat 102 are connected by a tension cable assembly 103; the locking nut 105 is arranged on the tension cable assembly 103 and outside the moving block 104;

[0039] The fuse cutter 101 is arra...

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Abstract

The invention provides a single-point flexible hold-down and release device for a spacecraft. The single-point flexible hold-down and release device comprises a fusing cutter, a hold-down base, a tension cable component, a moving block and a lock nut, wherein the moving block is connected with the hold-down base through the tension cable component, the lock nut is arranged on the tension cable component and outside the moving block, the fusing cutter which is arranged on the hold-down base is used for fusing the tension cable component, the hold-down base is used for being installed on the body of the spacecraft, and the moving block is used for being arranged in a stepped hole of a deployed appendage of the spacecraft so that the moving block has only one rotational degree of freedom around the central axis. The single-point flexible hold-down and release device for the spacecraft can effectively compress the deployed appendage onto the hold-down base with the compression force adjustable. In addition, thermal cutting can be achieved through the fusing cutter, so that low impact is caused in a releasing process without causing pollution.

Description

technical field [0001] The invention relates to a compression release device, in particular to a single-point flexible compression release device for a spacecraft. Background technique [0002] At present, the compression rod / pyrotechnic cutter type compression release mechanism commonly used in China, its working principle is to directly use the thrust generated by the explosion of the pyrotechnic device to push the cutter in the cutter, so that it can press the pressure at high speed. Tight rod cut off. [0003] This type of compression and release mechanism has the following limitations: the instantaneous large-scale shock load generated will affect the attitude of the satellite and the sensitive unit, and the corrosive and polluting gas will be generated during the ignition of the pyrotechnic device, which directly uses the explosion of explosives to produce There are certain potential safety hazards in the energy. The pyrotechnic device is a dangerous product, which br...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/64
CPCB64G1/64
Inventor 王萌聂斌斌赵发刚成飞顾志悦
Owner SHANGHAI SATELLITE ENG INST