Pressure protection device for sealed cabin of manned spacecraft under emergency pressure loss condition

A technology of manned spacecraft and protective devices, which is applied in the direction of aerospace safety/emergency devices, aerospace equipment, aerospace vehicles, etc., to achieve the effects of improving safety and reliability, light weight, and improving reliability

Active Publication Date: 2020-04-07
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

At present, in the event of a pressure emergency in the Shenzhou spacecraft and space station missions, the emergency oxygen supply function of the pressure suit in the cabin can only be supported, which can only support about 4 hours of emergency time, which is far from meeting the requirements of the spacecraft under the most severe conditions during the moon landing process. It takes about 7 days to transfer to the moon-earth return orbit until it returns to the ground safely

Method used

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  • Pressure protection device for sealed cabin of manned spacecraft under emergency pressure loss condition
  • Pressure protection device for sealed cabin of manned spacecraft under emergency pressure loss condition
  • Pressure protection device for sealed cabin of manned spacecraft under emergency pressure loss condition

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Embodiment Construction

[0022] The present invention will be further elaborated below in conjunction with embodiment.

[0023] The invention provides a pressure protection device in the case of emergency loss of pressure in a sealed cabin of a manned spacecraft. An inflatable flexible sealed capsule cabin environment is established inside the sealed cabin to realize pressure emergency protection. The flexible capsule cabin is provided with an interface for matching connection with the air supply system of the spacecraft airtight cabin and a sealed zipper opening for astronauts to enter and exit it. After analysis, the possible leakage position in the sealed cabin is the upper part of the sealed cabin. According to the principle of reusing the functions of the existing supporting equipment as much as possible, the flexible capsule cabin is installed in the connection area between the side wall of the sealed cabin and the big bottom. When the pressure in the airtight cabin of the return cabin is normal...

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Abstract

The invention relates to a pressure protection device used under the pressure loss condition of a sealed cabin of a re-entry capsule of a manned spacecraft. A flexible cabin inner bag is arranged in aconnecting area of the side wall of the re-entry capsule and an outsole; the side wall is shaped after unfolding; when the sealed cabin of the re-entry capsule loses pressure, by starting the flexible cabin inner bag installed in the re-entry capsule in advance, the flexible cabin inner bag is rapidly unfolded, fixed, inflated and sealed, so that a new sealed environment is created, and resourcessuch as a life support system, cabin pressure clothes and communication which are originally arranged on the spaceship are used for jointly guaranteeing that astronauts fly emergently on orbit for seven days until the astronauts return safely.

Description

technical field [0001] The invention relates to a pressure protection device in the case of emergency loss of pressure in a sealed cabin of a manned spacecraft, which is mainly aimed at the requirements of manned moon landing missions, and provides pressure protection for the emergency loss of pressure in the sealed cabin, and belongs to the non-destructive recovery technology of manned space vehicles field. Background technique [0002] The development of my country's manned moon landing project is of great significance in terms of economy, technology and national development strategy. my country's manned lunar exploration will aim at the low-latitude areas of the moon, and adopt the direct flight mode to the moon, which requires the spacecraft to independently complete near-month braking and return to the moon. Based on the current lunar landing flight mode of the lunar orbiting space station, during the manned lunar landing mission, if the airtight cabin of the spacecraf...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/52
CPCB64G1/52B64G1/525
Inventor 竺梅芳戈嗣诚王立武李博唐明章廖航甄铎
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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