Sealed cabin structure subassembly assembling method and sealed cabin structure

An assembly method and technology of the structural part are applied in the directions of measuring devices, optical devices, instruments, etc., to achieve good application prospects and economic benefits, shorten the development cycle, and improve the effects of production efficiency

Pending Publication Date: 2022-03-25
BEIJING SATELLITE MFG FACTORY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The sealed cabin usually has a large number of parts, however, there is no mature solution to complete the assembly of these parts in the prior art

Method used

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  • Sealed cabin structure subassembly assembling method and sealed cabin structure
  • Sealed cabin structure subassembly assembling method and sealed cabin structure
  • Sealed cabin structure subassembly assembling method and sealed cabin structure

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Embodiment Construction

[0049] In order to more clearly describe the embodiments of the present invention or the technical solutions in the prior art, the following will briefly introduce the drawings that are used in the embodiments. Apparently, the drawings in the following description are only some embodiments of the present invention, and those skilled in the art can also obtain other drawings according to these drawings without creative efforts.

[0050] When describing the embodiments of the present invention, the terms "vertical", "transverse", "upper", "lower", "front", "rear", "left", "right", "vertical", " The orientation or positional relationship expressed by "horizontal", "top", "bottom", "inner" and "outer" is based on the orientation or positional relationship shown in the relevant drawings, which are only for the convenience of describing the present invention and simplifying the description, and It is not to indicate or imply that the device or element referred to must have a particu...

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Abstract

The invention relates to a sealed cabin structure subassembly assembling method and a sealed cabin structure. The sealed cabin structure subassembly assembling method comprises the following steps that a, a glue joint support (2), a vertical beam (4) and an angle diaphragm beam system (3) are sequentially installed on a cabin body (1); b, a pull rod (7) is installed on the corner diaphragm beam system (3); c, the horizontal plate (5) and the vertical plate (6) are sequentially installed on the cabin body (1), and the whole cabin is tested. According to the invention, assembling, debugging, cementing, testing and other items of the large-scale sealed structure cabin subassembly can be efficiently realized.

Description

technical field [0001] The invention relates to a method for assembling a structure part of a sealed cabin and a structure of the sealed cabin. Background technique [0002] The space station is the base for human beings to enter space, and its airtight cabin generally includes a working cabin and a large column section. The airtight cabin is the place where astronauts work and live in space. It is equipped with various equipment for astronauts, making it an important part of the mission of the space station. Its performance also directly affects the life safety of astronauts and The success or failure of space station missions. The airtight cabin usually has a large number of parts, however, there is no mature solution to complete the assembly of these parts in the prior art. Contents of the invention [0003] The object of the present invention is to provide a method for assembling the structure part of the sealed cabin and the structure of the sealed cabin. [0004] ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B11/24G01B11/26
CPCG01B11/24G01B11/26
Inventor 王咏莉张斌杨晶樊晓霞冯文雄龙海东李扬洲
Owner BEIJING SATELLITE MFG FACTORY
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