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Air-controlled auxiliary docking device and air-controlled auxiliary docking method for satellites

A docking device and satellite technology, applied in the aerospace field, can solve the problems of poor docking position and angle tolerance, and achieve the effects of strong tolerance, convenient unlocking, and simple structure

Active Publication Date: 2020-01-21
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The invention provides an air-controlled auxiliary docking device to solve the technical problem of poor docking position and angle tolerance of the existing auxiliary docking device

Method used

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  • Air-controlled auxiliary docking device and air-controlled auxiliary docking method for satellites
  • Air-controlled auxiliary docking device and air-controlled auxiliary docking method for satellites
  • Air-controlled auxiliary docking device and air-controlled auxiliary docking method for satellites

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Embodiment Construction

[0027] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in various ways defined and covered below.

[0028] figure 1 It is a schematic structural diagram of an air-controlled auxiliary docking device in a preferred embodiment of the present invention; figure 2 It is a schematic diagram of the longitudinal section structure of the single-section airbag body in the preferred embodiment of the present invention; image 3 It is a schematic diagram of the cross-sectional structure of the single-section airbag body in the preferred embodiment of the present invention; Figure 4 It is a structural exploded view of the connection sealing device of the preferred embodiment of the present invention; Figure 5 It is a schematic flow chart of the air-controlled assisted docking method of the satellite in the preferred embodiment of the present invention.

[0029] Such as...

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Abstract

The invention discloses a pneumatic auxiliary docking device and a pneumatic auxiliary docking method for a satellite. The pneumatic auxiliary docking device for the satellite comprises an inflatabledocking lock head, a gasbag structure and an installation base, wherein the inflatable docking lock head is used for conducting flexible guide and conducting docking locking through inflation expansion in the satellite docking process, the gasbag structure is used for inflating in different directions to adjust attitudes, and the installation base is used for being in mechanical connection with asatellite body. The inflatable docking lock head is connected to the first end of the gasbag structure in a sealing mode, and the installation base is connected to the second end of the gasbag structure in a sealing mode. Through the pneumatic auxiliary docking device, the inflation pressure and amount of different areas in the gasbag structure loaded on the service satellite are controlled, so that the variation of the appearance attitude of the gasbag structure is controlled, the inflatable docking lock head is driven to move and is inserted into an engine jet pipe of the target satellite toachieve flexible capturing, and allowance capacity of docking capture positions and angles is high.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to an air-controlled auxiliary docking device. In addition, the present invention also relates to an air-controlled auxiliary docking method of a satellite using the above-mentioned air-controlled auxiliary docking device. Background technique [0002] On-orbit service of spacecraft involves on-orbit fuel filling and life extension, maintenance assembly and upgrade, debris removal, auxiliary orbit change, etc., and one of the key technologies is to realize autonomous docking and capture of spacecraft through auxiliary docking devices. [0003] There are many types of existing auxiliary docking devices. The telescopic rod-type auxiliary docking device sends the expandable mechanism into the engine nozzle of the target satellite by extending the double rods, and then shortens the double rods to make the service satellite gradually approach the target satellite. The mechanism captu...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/64
CPCB64G1/646
Inventor 张翔许展鹏陈小前黄奕勇陈勇赵勇张熠
Owner NAT UNIV OF DEFENSE TECH
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