Spacing device for disassembling spatially large-bearing product

A technology with a limit device and a large space, which is applied in the directions of transportation and packaging, space navigation equipment, and space navigation vehicles, etc., to achieve the effect of satisfying verticality

Active Publication Date: 2020-02-21
SHANGHAI INST OF SPACE POWER SOURCES
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0004] The technical problem solved by the present invention is: to overcome the deficiencies of the prior art, to propose a limiting device for the disassembly of products with a large space, and to solve the problem of the design of the on-orbit disassembly limit for products with a large space outside the cabin according to the functional requirements of the products outside the cabin

Method used

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  • Spacing device for disassembling spatially large-bearing product
  • Spacing device for disassembling spatially large-bearing product
  • Spacing device for disassembling spatially large-bearing product

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Embodiment Construction

[0024] The present invention will be further elaborated below in conjunction with embodiment.

[0025] The key structure of the on-rail dismounting and limiting method for large-space load-carrying products of the present invention lies in positioning pins and limiting blocks. in, figure 1 Shown is the overall schematic diagram of the limit device. It can be seen from the figure that one M4 process screw hole is designed in the center of the end face of the positioning pin 1 for the installation and disassembly of the positioning pin 1. The positioning pin is fixed on the cabin flange 3; the positioning pin 1. There must be enough length to limit the position, and cooperate with the cabin flange 3 and the limit block 2 to limit the position and prevent the axial movement of the mechanical arm. The space is large and the limiting device for product disassembly includes a cabin flange 3, two positioning pins 1 and two limiting blocks 2; among them, the cabin flange 3 is a disc-...

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Abstract

The invention relates to a spacing device for disassembling a spatially large-bearing product, and belongs to the field of the in orbit disassembling design of the large-bearing product. The spacing device comprises a cabin flange plate, two positioning pins and two spacing blocks, wherein the cabin flange plate is of a disk-shaped structure; two positioning pins are symmetrically arranged on theinstallation surface of the cabin flange plate; the two spacing blocks are independently correspondingly cooperated with the two positioning pins; the spacing and the fixing of the cabin flange plateare realized; the two spacing blocks are in 180-degree distribution; when an outer cabin rises to an outer space, under a vacuum environment, screws between the cabin flange plate and the outer cabinare disassembled; under the spacing cooperation of the positioning pins and the spacing blocks, the circumferential spacing of the cabin flange plate is realized; and 12 screws are disassembled in sequence. According to the function requirements of an out-cabin product, the problem that the in-orbit disassembling and spacing design of the out-cabin product large-bearing product can be solved.

Description

technical field [0001] The invention belongs to the field of on-rail disassembly design for large load-bearing products, and relates to a limiting device for dismounting large-space load-bearing products. Background technique [0002] The construction of the space station, the third step of China's manned spaceflight project, will be built in 2020 and 2022. After the Chinese space station is put into normal operation, it will carry out scientific research and space experiments, and promote China's space science research and development into the world's advanced ranks. The construction of China's space station will aim at mastering the construction technology of the space station, using the technology synchronized with the times, and building a space station with the characteristics of the times. [0003] After the completion of the three-chamber combination of the Chinese space station, in order to meet the needs of long-life use and breakthroughs in space technology experi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/22B64G1/66
CPCB64G1/22B64G1/66
Inventor 金磊马季军谢朋儒沈冰冰王柳曲芳仪凌财华方良超
Owner SHANGHAI INST OF SPACE POWER SOURCES
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