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Passive-trigger-type space debris capturing device

A space debris and capture device technology, applied in the field of aerospace, to reduce costs, improve collection effects, and consume less energy

Inactive Publication Date: 2017-10-20
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to overcome the shortcomings of the above-mentioned prior art, and provide a passive trigger type space debris capture device, which belongs to the passive cleaning method, consumes very little energy, mainly relies on external natural factors to clean up debris, and uses a passive trigger mechanism to capture debris , the device has good reusability and can meet the needs of reducing costs

Method used

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  • Passive-trigger-type space debris capturing device

Examples

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Embodiment Construction

[0033] The present invention is described in further detail below in conjunction with accompanying drawing:

[0034] see Figure 1-9 , this passive trigger type space debris capture device includes two capture storage bins 1, and a trigger system 2 and a base 9 connected between the two capture storage bins 1, the trigger system 2 is connected to the base 9;

[0035] The capture storage bin 1 includes a storage bin body, and a storage bin connecting rod assembly connected with the storage bin body; the storage bin body is provided with a storage bin mouth 23, and the storage bin connecting rod assembly is connected to the base 9, and the storage bin body is The storage bin wall 3 is a polygonal shell; the trigger system 2 includes a motor, a screw drive system, a slider type opening and closing system and a spring trigger 8; the motor is connected to the screw drive system, and the upper and lower ends of the screw drive system are respectively It is connected with the spring...

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PUM

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Abstract

The invention discloses a passive-trigger-type space debris capturing device. The passive-trigger-type space debris capturing device comprises two capturing storage bins, a trigger system and a base, wherein the trigger system and the base are connected between the two capturing storage bins, and the trigger system and the base are connected. The capturing storage bins comprise storage bin bodies and storage bin connecting rod assemblies connected with the storage bin bodies; and storage bin openings are formed in the storage bin bodies, the storage bin connecting rod assemblies are connected with the base, and the trigger system comprises a motor, a lead screw driving system, a sliding-block-type opening and closing system and a spring trigger. The passive-trigger-type space debris capturing device has the beneficial effects that the space debris capturing device belongs to a passive cleaning method, space debris can be effectively acquired through an integral enveloped-type structure of the two capturing storage bins, and the debris is acquired passively by arranging the trigger system; and because the debris is cleaned mainly depending on natural factors of the outside world, the consumed energy is extremely little, and the cost is reduced.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and relates to a passive trigger type space debris capture device. Background technique [0002] The existence of space debris is a serious threat to the safety of spacecraft in orbit. The collision between them and the spacecraft will cause damage to surface devices, lead to failure of spacecraft systems, and bring great harm to the normal operation of spacecraft. At the same time, the continuous expansion of the number of space debris also poses a serious threat to limited orbital resources. At present, the orbits with relatively concentrated debris are sun-synchronous orbits and geosynchronous orbits. When the density of space debris reaches a critical value, the chains between debris Collisions can cause permanent damage to orbital resources. [0003] For space debris larger than 10cm, the kinetic energy is very large, and it will cause devastating damage when it hits a spacecraft. Debris...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G4/00
Inventor 岳晓奎杨冬王环袁建平宁昕
Owner NORTHWESTERN POLYTECHNICAL UNIV
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