On-orbit dragging-off tool for case in manned spaceflight cabin

A technology of manned spaceflight and internal chassis, which is applied in the field of manned spaceflight systems, can solve the problems of insufficient operating force of astronauts on orbit, and achieve the effects of simple structure, reduced physical exertion, and convenient operation

Active Publication Date: 2022-02-15
10TH RES INST OF CETC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to improve the reliability of the manned aerospace electronic stand-alone unit, the present invention aims at the above-mentioned problems, and aims to provide a tool for quickly plugging and unplugging the chassis of aerospace electronic equipment in the manned space cabin for easy maintenance, so as to solve the problem of astronauts in weightlessness. The problem of insufficient on-orbit operating force in the environment

Method used

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  • On-orbit dragging-off tool for case in manned spaceflight cabin
  • On-orbit dragging-off tool for case in manned spaceflight cabin
  • On-orbit dragging-off tool for case in manned spaceflight cabin

Examples

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Embodiment Construction

[0020] see Figure 1-3 . In an illustrative preferred embodiment described below, an on-orbit dragging tool for a chassis in a manned spacecraft includes: a backplane 5 fixed at the rear end of the aerospace cabinet 1, and fixedly connected to the left and right of the ladder frame of a column on one side of the aerospace cabinet 1 The guide rail 4 of the direction, the aerospace electronic case 2 designed with reference to the international VITA series standard, the crank connecting rod advancer 3 that can be rotatably linked on the hinge seat of the front panel of the aerospace electronic case 2, is characterized in that: the aerospace electronic case 2 is installed in the aerospace electronic case 2. The left and right inner sides of the lower part of the ladder frame of the cabinet 1 can be moved in a straight line forward and backward through the guide rails 4; the crank connecting rod advancer 3 is hinged through the crank connecting rod hinge 20 of the hinge seat on the...

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Abstract

The invention discloses an on-orbit dragging-off tool for a case in a manned spaceflight cabin, and belongs to the field of manned spaceflight systems. According to the technical scheme, a spaceflight electronic case is installed on the lower portion of a step frame of the spaceflight cabinet and linearly moves through a guide rail; a crank connecting rod precession device is rotationally connected to the guide rail through a crank connecting rod hinge device hinged to a hinge base of a front panel of the case, the rotating motion of the crank connecting rod precession device is converted into linear motion of the spaceflight electronic case along the guide rail, and the crank connecting rod precession device rotates clockwise or anticlockwise. And the spaceflight electronic case is linked to linearly move forwards and backwards along the guide rail, so that on-orbit dragging of the spaceflight electronic case and a back plate is quickly realized. In-orbit dragging of the case and the back plate is achieved through a lever mechanism and a crank sliding block mechanism, operation is convenient, operation force and physical output of astronauts can be effectively reduced, the manned spaceflight operation condition can be adapted, and the in-orbit operation capacity of the astronauts and the pulling force needed for disassembling and assembling the case are met.

Description

technical field [0001] The invention belongs to the field of manned spaceflight systems, in particular to an on-orbit dragging tool for a chassis in a manned spaceflight capsule. Background technique [0002] As a scientific platform for humans to explore the mysteries of space, the biggest feature of the space station is that it can stay in space for a long time, providing a safe and reliable working environment for humans to directly participate in space scientific research. However, due to the long-term impact of the very harsh space environment such as high vacuum, low temperature, solar electromagnetic radiation, ionosphere, and earth radiation, the reliability of its airborne electronic equipment has been continuously reduced, and some functional modules cannot work normally. It directly affects the completion of the entire flight mission. Therefore, the problem of how to prolong the on-orbit operation period of spacecraft electronic equipment needs to be solved urgen...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/66
CPCB64G1/66Y02T50/40
Inventor 刘攀王东方伟陈福林
Owner 10TH RES INST OF CETC
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