Spacecraft cabin door opening and closing device

A technology of opening and closing device and spacecraft, applied in the aerospace field, can solve problems such as endangering the safety of astronauts, and achieve the effect of reducing operation, high safety and operability

Pending Publication Date: 2022-01-18
LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Astronauts will wear space suits before leaving the cabin. Due to time constraints, it is impossible to completely pump the cabin to a vacuum state. Then open the cabin door. There will be a certain amount of residual gas in the cabin, which will be generated during the door opening process. A certain impact will endanger the safety of the astronauts. At the same time, in order to reduce the operation of the astronauts, the hatch needs to be able to automatically open to the specified position.

Method used

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  • Spacecraft cabin door opening and closing device
  • Spacecraft cabin door opening and closing device
  • Spacecraft cabin door opening and closing device

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Embodiment Construction

[0021] In order to enable those skilled in the art to better understand the solution of the present application, the technical solution in the embodiment of the application will be clearly and completely described below in conjunction with the accompanying drawings in the embodiment of the application. Obviously, the described embodiment is only It is an embodiment of a part of the application, but not all of the embodiments. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the protection scope of this application.

[0022] Such as Figure 1-Figure 2 As shown, the application provides a spacecraft door opening and closing device, including a booster mechanism 1 and a damping mechanism 2, and the booster mechanism 1 and the damping mechanism 2 are fixedly installed on the cabin body 5 of the spacecraft through a pin 3 and a hinge bracket 4 And on the cabin door 6, the...

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PUM

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Abstract

The invention relates to the technical field of spaceflight, in particular to a spacecraft cabin door opening and closing device which comprises a power assisting mechanism and a damping mechanism, wherein the power assisting mechanism and the damping mechanism are fixedly mounted on a cabin body and a cabin door of a spacecraft through pins and hinge supports, and the power assisting mechanism and the damping mechanism are arranged in parallel. Through parallel connection of the power assisting mechanism and the damping mechanism, the spacecraft cabin door can be autonomously and slowly opened, instantaneous impact of residual air pressure in the cabin on the cabin door can be counteracted in the opening process, the cabin door is prevented from being closed too fast in the closing process, operation of astronauts in the cabin leaving process is reduced, and high safety and operability are achieved.

Description

technical field [0001] The present application relates to the field of aerospace technology, in particular, to an opening and closing device for a cabin door of a spacecraft. Background technique [0002] Astronauts will wear space suits before leaving the cabin. Due to time constraints, it is impossible to completely pump the cabin to a vacuum state. Then open the cabin door. There will be a certain amount of residual gas in the cabin, which will be generated during the door opening process. A certain impact will endanger the safety of the astronauts. At the same time, in order to reduce the operation of the astronauts, the hatch needs to be able to automatically open to the specified position. Contents of the invention [0003] The main purpose of this application is to provide a spacecraft door opening and closing device, through the cooperation of the booster mechanism and the damping mechanism, the door is opened, and the impact of the residual air pressure in the cab...

Claims

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Application Information

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IPC IPC(8): E05F15/53E05F3/02B64G1/22
CPCE05F15/53E05F3/02B64G1/22
Inventor 崔志武崔晓杰康昌玺刘轶鑫柳明明崔致和
Owner LANZHOU INST OF PHYSICS CHINESE ACADEMY OF SPACE TECH
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