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A Self-Adaptive Penetration Deployment Attachment Device for Space Target Surface Attachment

A technology for attachment devices and space targets, which is applied in the field of self-adaptive penetration and deployment attachment devices, can solve the problems of target penetration and destruction, large penetration kinetic energy, and violations, and achieve a wide range of applicable objects, low manufacturing cost, and tolerance big difference

Active Publication Date: 2022-03-04
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The anchor attachment device is suitable for attachment to the hard surface of asteroids in microgravity, and the penetration kinetic energy is relatively large. The deployment mechanism is an active power deployment method, and a pyrotechnic device is required to unlock the action. It is not suitable for the capture of debris, satellites, etc. It will cause penetration and destruction of the target, which violates the original intention of on-orbit rescue and maintenance

Method used

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  • A Self-Adaptive Penetration Deployment Attachment Device for Space Target Surface Attachment
  • A Self-Adaptive Penetration Deployment Attachment Device for Space Target Surface Attachment
  • A Self-Adaptive Penetration Deployment Attachment Device for Space Target Surface Attachment

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Embodiment 1

[0023] The schematic diagram of the composition of the self-adaptive penetration deployment attachment device on the surface of the space target is as follows: figure 1 , figure 2 As shown, it includes: nose cone 1, spear body skeleton 2, barb shaft 3, first barb 4, second barb 5, baffle sleeve 6, limit ejector rod 7, rear end cover 8, fixing pin 9, torsion spring 10, buffer pad 11, buffer washer 12,

[0024] The lance skeleton 2 includes two cylindrical structures with different diameters. The middle part of the cylindrical structure with a larger diameter is provided with a rectangular hole symmetrical to the central axis of the lance skeleton 2 along the radial direction to form a cavity, and the walls on both sides of the cavity are arranged symmetrically. With pin hole;

[0025] Wherein the tail of the nose cone 1 is screwed into the lance body skeleton 2 through threaded connection, and the barb shaft 3 is introduced from the pin shaft hole on one side of the lance bo...

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Abstract

The invention relates to an self-adaptive penetrating and deploying attachment device for attaching to the surface of a space target, comprising: a nose cone, a spear body skeleton, a barb shaft, a first barb, a second barb, a baffle sleeve, a stopper Ejector rod, rear end cover, torsion spring; the tail of the nose cone is installed in the lance body skeleton; the barb shaft is introduced from the pin hole on one side of the lance body skeleton, and passes through the end mounting hole of the second barb and the torsion spring and the end mounting hole of the first barb, and enter the pin hole on the other side of the lance frame; the end with the smaller diameter of the lance frame is inserted into the baffle sleeve and can slide in the baffle sleeve, and the baffle sleeve The lugs at the end of the barrel block the ends of the first barb and the second barb; the limit push rod penetrates through the other end of the baffle sleeve and is installed at the end of the spear body with a smaller diameter, and the rear end cover is installed into the port on the other end of the baffle sleeve. The invention solves the problem of micro-damage capture of large space debris, on-orbit maintenance and off-orbit operation of faulty satellites.

Description

technical field [0001] The invention belongs to the field of on-orbit service and space operation applications such as space debris cleaning, on-orbit maintenance and rescue of faulty satellites, and relates to an adaptive penetration and deployment attachment device. Background technique [0002] Space debris, faulty satellites, abandoned satellites and other space targets are increasing day by day, and the safe operation of space vehicles in orbit is seriously threatened. It will become more and more difficult to deal with traditional active avoidance methods, and will greatly reduce the life of space vehicles; Defense methods can only deal with some types of space targets. On the other hand, large-scale space flight platform facilities will highlight the function of on-orbit maintenance and repair services. For example, to rescue or repair a faulty satellite, it is necessary to complete the task of capturing it at close range. The satellites launched in the early stage p...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G4/00
CPCB64G4/00
Inventor 冯蕊朱谦王立武唐明章刘永健谭春林王永滨龙龙冯瑞霍东阳
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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