Structure for configuring functional regions for ultra-large type manned spacecraft AIT center

Abstract

The invention discloses a structure for configuring functional regions for an ultra-large type manned spacecraft AIT center. The structure comprises a transferring chamber, a leakage test region, a final assembly and quality test region, a final assembly and electric test region, a mechanical test region, a thermal test region, an EMC test region, a main logistics channel and a final assembly supporting warehouse, wherein the structure is in an I-shaped shape in whole, a first horizontal line of the structure is sequentially provided with the thermal test region, the leakage test region and the mechanical test region, and the thermal test region, the leakage test region and the mechanical test region communicate with one another for transferring of an ultra-large type manned spacecraft; the middle main logistics channel is formed in a vertical part of the structure, the EMC test region is arranged on one side of the middle of the channel, and the transferring chamber and the final assembly supporting warehouse are arranged on the other side of the channel; and one side of a second horizontal line of the structure is provided with the electric test region, and the other side of thesecond horizontal line of the structure is provided with the quality test region, the top of the channel communicates with the leakage test region, and the middle part and the lower part of the channel correspondingly communicate with the regions arranged on the two sides. According to the structure, the regional layout is reasonable, transferring of the spacecraft is smooth, a path is reasonable,the site and resource occupation, the logistics and the like are mutually coordinated, and the application effect is good.

Description

technical field [0001] The invention belongs to the technical field of spacecraft assembly, integration, and test plant process layout design. Specifically, the invention relates to a configuration structure of the AIT central functional area of ​​an ultra-large manned spacecraft, which combines the conventional technical process of a large manned spacecraft , reasonably plan the layout structure of each functional area and other auxiliary areas of the large-scale manned spacecraft assembly, integration, and test workshops, and realize the reasonable flow of the spacecraft assembly and testing phase. Background technique [0002] At present, my country is developing the manned space station. In the process of developing the space station, it is inseparable from the final assembly, testing, and testing of super-large manned spacecraft. There are fixed technical processes for each work and each work needs to be done in Specific work areas are completed, and if these work areas ...

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Problems solved by technology

[0004] Based on this, the purpose of the present invention is to provide a functional area configuration structure suitable for large-scale manned spacecraft assembly, testing, and testing centers. Divide professional areas for testing, etc., and make reasonable layouts for each professional area, loading room, logistics channel, etc., to reduce frequent transfers between large processes, and solve the problem of difficult transfer and high cost of large manned spacecraft

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