Quick release device for load of space science experiment

A technology of space science and loading, applied in the direction of teaching models, educational tools, instruments, etc., can solve the problems of wasting time, affecting space science experiments, and easily damaged equipment, and achieve the effect of easy operation

Active Publication Date: 2021-10-15
TECH & ENG CENT FOR SPACE UTILIZATION CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In the process of space science experiments, it is very troublesome to replace the standard load. Often, a standard load is equipped with a mounting structure and installed on the centrifuge; when replacing the standard load, the mounting structure needs to be removed, which wastes time and space When the personnel dismantle the installation structure, it is very easy to damage other related equipment, thus affecting the space science experiment

Method used

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  • Quick release device for load of space science experiment
  • Quick release device for load of space science experiment
  • Quick release device for load of space science experiment

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Embodiment Construction

[0026] In order to make the objects, technical solutions and advantages of the present invention, the present invention will be described in further detail below with reference to the accompanying drawings. It should be understood that the specific embodiments described herein are intended to be used to illustrate the invention and are not intended to limit the invention.

[0027] like Figures 1 to 7 As shown in this embodiment, a quick release device for spatial scientific experimental loads, including

[0028] Dynamic port assembly; including a rectangular dynamic interface plate 1, the two long sides of the moving interface plate 1 respectively have a plurality of mounting ear 2, respectively, each of which is disposed on each of the installed ear 2. There is a mounting hole through which the upper and lower sides is formed, and each of the mounting ear is respectively provided with a certain bit ring 3, and the central bore of the positioning ring 3 corresponds to the mounting...

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Abstract

The invention discloses a quick release device for a load of a space science experiment. The quick release device comprises a movable interface board assembly and a load pushing assembly, wherein the movable interface board assembly comprises a rectangular movable interface board, two opposite long edges of the movable interface board are respectively and correspondingly provided with a plurality of installation lugs which protrude and extend outwards, each installation lug is provided with an installation hole which penetrates through the upper side and the lower side of the installation lug, each installation lug is respectively and fixedly provided with a positioning ring in a corresponding mode, the center holes of the positioning rings correspond to the installation holes, a push ring is arranged on one side of each center hole in the circumferential direction, the push rings extend in the direction parallel to the axis of the center holes to the direction away from the installation lugs, a connector seat is arranged on the movable interface board, and the load pushing assembly comprises a standard load seat, a thrust wedge, a connecting rod assembly and a handle locking assembly. The quick release device has the advantages that an experimental load unit can be quickly and conveniently inserted, pulled, fixed and locked on orbit, and operation of astronauts is facilitated.

Description

Technical field [0001] The present invention relates to the field of construction machinery and spatial structures, and more particularly to a quick release device for spatial scientific experimental loads. Background technique [0002] During the spatial scientific experiment, it is very troublesome when the standard load is replaced. It is often a standard load equipped with a mounting structure, which is installed on the centrifuge; when replacing the standard load, you need to remove the installation structure, waste time, space When removing the installation structure, it is also very easy to damage other related devices, which will affect the spatial scientific experiment. Inventive content [0003] It is an object of the present invention to provide a quick release device for spatial scientific experimental loads, thereby solving the foregoing problems present in the prior art. [0004] In order to achieve the above object, the technical solution used in the present inven...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B25/00
CPCG09B25/00
Inventor 邵彩云周妍林王绍坤
Owner TECH & ENG CENT FOR SPACE UTILIZATION CHINESE ACAD OF SCI
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