Centrifugal cabin of space station

By designing the cabin structure used in the space station, including the rotating inner cabin and synchronous transfer compartment, the long -term influence of aerospace members' long -term weightless state on health is achieved, the production of artificial gravity is achieved, and the quality of life of astronauts and recovery of healthy health is improved. speed.

CN119370348APending Publication Date: 2025-01-28徐吉春
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Patent Information

Application Number
CN202310923271.3
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2023-07-26
Publication Date
2025-01-28

AI Technical Summary

Technical Problem

The existing space station cabin causes astronauts to be in a state of weightlessness for a long time, affecting their life activities and physical health, and resulting in a long recovery time after returning to the ground.

Method used

Design a cabin structure for artificial gravity produced in the space station, including connecting cabins, amplifiers and channels and channels, outer cabins, rotating inner cabins and metastasis. Realize the safe transfer of personnel or materials.

Benefits of technology

By generating artificial gravity, reduce the adverse effects on the health of astronauts, improve the quality and work efficiency of astronauts in the space station, and shorten the time to recover health after returning to the ground.

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Abstract

The invention relates to the technical field of space station cabins, in particular to a structure for generating artificial gravity of a space station and a working method of the structure. According to the cabin structure for generating the artificial gravity in the space station and the working method of the cabin structure, in order to achieve the purpose, the following technical scheme is provided, and the cabin structure for generating the artificial gravity in the space station comprises a cabin body, comprising a connecting cabin, a radial connecting rod, at least one radial channel, an outer cabin, an inner cabin and a transfer cabin, wherein the connecting cabin is static relative to other cabins of the space station; the inner cabin rotates at a certain angular speed relative to the outer cabin; and the transfer cabin is used for transferring personnel or materials between the inner cabin and the outer cabin. And the inner cabin is controlled by a motor to rotate at a certain angular speed on a track fixed in the outer cabin. And the rotating state of the transfer cabin is changed through a motor on a track fixed on the outer cabin, so that the transfer cabin is synchronized with the outer cabin or the inner cabin. And the connecting cabin, the radial channel and the outer cabin are of an integral sealing structure.
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Description

Technical Field

[0001] The present invention relates to the technical field of space station cabins, and in particular to a structure for generating artificial gravity in a space station and a working method thereof. Background Art

[0002] Currently, astronauts in the space station are in a state of weightlessness during their missions. Long-term exposure to weightlessness will have certain adverse effects on people's life activities and physical health (including muscle atrophy and swelling of the whole body), so that it will take a long time to recover after returning to the ground. Summary of the invention

[0003] The present invention is intended to provide a cabin structure and a working method thereof for generating artificial gravity in a space station, so as to solve the problem that the existing cabin has adverse effects on human health.

[0004] In order to achieve the above-mentioned purpose, the present invention provides the following technical solutions: A cabin structure for generating artificial gravity in a space station, comprising a connection cabin relatively stationary with other cabins of the space station, a radial connection rod and at least one radial channel, an outer cabin, an inner cabin rotating at a certain angular velocity relative to the outer cabin, and a transfer cabin for transferring personnel or materials between the inner cabin and the outer cabin. The inner cabin rotates at a certain angular velocity on a track fixed in the outer cabin through motor control. The transfer cabin changes its rotation state through a motor on a track fixed in the outer cabin to achieve synchronization with the outer cabin or the inner cabin.

[0005] The connecting cabin is cylindrical.

[0006] The outer cabin is annular and connected to the connecting cabin through multiple radial channels.

[0007] The connecting cabin, radial passage and outer cabin are an integrally sealed structure.

[0008] The inner cabin is annular and rotates at a constant angular velocity in the outer cabin.

[0009] The transfer cabin is ring-shaped.

[0010] Cabin doors 1 and 2 are installed between the radial passage and the transfer cabin, and cabin doors 3 and 4 are installed between the transfer cabin and the inner cabin.

[0011] There is a corresponding door opening button installed next to each cabin door, namely Button 1, Button 2, Button 3, and Button 4. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Figure 1 This is a schematic diagram of the front structure.

[0013] Figure 2 Schematic diagram of the side structure Implementation

[0014] The present invention is further described in detail below in conjunction with the accompanying drawings and embodiments:

[0015] The process of astronauts entering the inner cabin:

[0016] The astronaut reaches hatch 1 through the connecting cabin and radial channel, and presses door opening button 1 to send a door opening signal.

[0017] The system controls the transfer cabin to be synchronized with the radial channel and locks the doors 1 and 2 when they are aligned, and automatically opens the doors 1 and 2.

[0018] At this time, the astronauts enter the transfer cabin, and hatch 1 and hatch 2 are automatically closed and unlocked.

[0019] The astronaut adjusts his posture to face the hatch 3 with his head and feet in a standing position, holds the handrail to stabilize his body, and presses the door opening button 3 to send a door opening signal.

[0020] The system controls the transfer cabin to be synchronized with the inner cabin and locks the cabin door 3 and the cabin door 4 when they are aligned, and automatically opens the cabin door 3 and the cabin door 4.

[0021] When the astronauts enter the inner cabin, hatch 3 and hatch 4 are automatically closed and unlocked.

[0022] Astronauts' extravehicular activity:

[0023] The astronaut walks to the hatch 4 and presses the door opening button 4 to send a door opening signal.

[0024] The system controls the transfer cabin to be synchronized with the inner cabin and locks the cabin doors 3 and 4 when they are aligned, and automatically opens the cabin doors 3 and 4.

[0025] At this time, the astronauts enter the transfer cabin, and hatch 3 and hatch 4 are automatically closed and unlocked.

[0026] The astronaut holds the handrail to stabilize his body and presses the door opening button 2 to send the door opening signal.

[0027] The system controls the transfer cabin to be synchronized with the radial channel and locks the doors 1 and 2 when they are aligned, and automatically opens the doors 1 and 2.

[0028] When the astronauts enter the radial channel, hatch 1 and hatch 2 are automatically closed and unlocked.

Claims

1. A cabin structure for generating artificial gravity in a space station, characterized by: It includes a connecting cabin that is relatively stationary with other cabins of the space station, a radial connecting rod and at least one radial channel, an outer cabin, an inner cabin that rotates at a certain angular velocity relative to the outer cabin, and a transfer cabin used to transfer personnel or materials between the inner cabin and the outer cabin. The inner cabin rotates at a certain angular velocity on a track fixed in the outer cabin through motor control.

2. According to claim 1, a cabin structure for generating artificial gravity in a space station is characterized by: The transfer cabin changes its rotation state on the track fixed on the outer cabin through a motor to achieve synchronization with the outer cabin or the inner cabin.

3. According to claim 1, a cabin structure for generating artificial gravity in a space station is characterized by: The connecting cabin, radial passage and outer cabin are an integrally sealed structure.

Citation Information

Patent Citations

  • Gravity cabin

    CN105947240A

  • Artificial gravity system with rotating hub that is sealed with rotary seals

    US20170240302A1