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A kind of assembly method of spacecraft structural plate

A spacecraft structure and assembly method technology, applied in the aerospace field, can solve the problems of high operator experience and cooperation requirements, affect the progress of spacecraft development, consume human resources and time, etc., achieve flexible structure and improve assembly efficiency , the effect of avoiding the risk of line pressure

Active Publication Date: 2021-09-24
INNOVATION ACAD FOR MICROSATELLITES OF CAS +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] Although the operation process of the plywood is not complicated, it requires a high level of experience and cooperation of the operator, and requires a high degree of concentration and fine operation to ensure that it does not rub against other structures or press the cross-board cables, which consumes a lot of time. Human resources and time, thereby increasing the manufacturing cost of the satellite
Moreover, the personnel on the monitoring post are usually the R&D personnel of the relevant components, and they spend too much time on assembly, which means that the time spent on R&D is reduced, which also affects the overall development progress of the spacecraft to a certain extent.

Method used

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  • A kind of assembly method of spacecraft structural plate
  • A kind of assembly method of spacecraft structural plate
  • A kind of assembly method of spacecraft structural plate

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Embodiment Construction

[0042] In the following description, the present invention is described with reference to various examples. One skilled in the art will recognize, however, that the various embodiments may be practiced without one or more of the specific details, or with other alternative and / or additional methods, materials, or components. In other instances, well-known structures, materials, or operations are not shown or described in detail so as not to obscure the inventive concepts of the present invention. Similarly, for purposes of explanation, specific quantities, materials and configurations are set forth in order to provide a thorough understanding of embodiments of the invention. However, the invention is not limited to these specific details. Furthermore, it should be understood that the embodiments shown in the drawings are illustrative representations and are not necessarily drawn to correct scale.

[0043] In this specification, reference to "one embodiment" or "the embodiment...

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Abstract

The invention discloses a method for assembling a structure plate of a spacecraft. Firstly, a cable support is installed on the structure, and it is unfolded at a specified angle, so that the cross-plate cable can cross the cable support to avoid pressure lines, and then the structure plate is adjusted to a vertical state. And close to the main structure of the satellite. After arriving at the designated position, fix the cross-board cables, fold and disassemble the cable brackets, and finally complete the structural board plywood.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to an assembly method of a spacecraft structural plate. Background technique [0002] With the rapid development of aerospace technology, it is very important to shorten the development and production cycle of spacecraft under the premise of ensuring quality. Because the spacecraft has extremely high requirements on assembly accuracy and quality, in addition to the operators, it is necessary to arrange a large number of monitoring posts during the current spacecraft assembly process, which greatly increases the labor cost. [0003] Taking the final assembly of the satellite structure board as an example, during the assembly process, when the distance between the satellite structure board and the main body of the satellite may cause the risk of pressing on the cross-board cable, the assembly speed needs to be slowed down, and the operators and monitoring personnel are all focused ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/10
CPCB64F5/10
Inventor 田艳安洋孙之民许国平张嘎曹昕
Owner INNOVATION ACAD FOR MICROSATELLITES OF CAS