A Fast Finite Element Modeling and Post-processing Method for Solar Sail Structure

A finite element and solar technology, applied in electrical digital data processing, special data processing applications, instruments, etc., can solve the problems of time-consuming and laborious, unable to reflect the mechanical properties of large ultra-flexible sail surfaces, and unable to reflect the mechanical properties of solar sails. Easy to store and carry, reducing the effect of repetitive work

Inactive Publication Date: 2016-08-24
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] When analyzing the mechanical characteristics of solar sails, finite element modeling is a thorny issue in the mechanical analysis process, which is time-consuming and labor-intensive. Usually, small changes in the structural form or changes in configuration dimensions will lead to repetitive workload of finite element analysis
At the same time, ordinary post-processing analysis cannot reflect the real mechanical properties of solar sails, and the mechanical properties of large ultra-flexible sails cannot be reflected at all through simple result data.

Method used

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  • A Fast Finite Element Modeling and Post-processing Method for Solar Sail Structure
  • A Fast Finite Element Modeling and Post-processing Method for Solar Sail Structure
  • A Fast Finite Element Modeling and Post-processing Method for Solar Sail Structure

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Embodiment

[0056] Example: Static finite element simulation analysis of 160m solar sail structure

[0057] 1) Set the configuration of the solar sail as a square sail, and set its two diagonals as the reserved space for the support arm, and reserve the space for the end point of the support arm to be 5 times the diameter of the support arm; set the support arm to connect with the sail surface The form is a connection configuration only at the ends of the support arms.

[0058] 2) According to the set configuration of the square solar sail, set the membrane of the sail surface as a single type, set the side length of the square sail to 160m, and obtain the geometric model of the sail surface with reserved square diagonals.

[0059] 3) Set the support arm type to the circular tube section shape; generate the support arm geometric model according to the diagonal position reserved by the obtained sail surface geometric model.

[0060] 4) Set the center body mass m center =100kg, terminal w...

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Abstract

Disclosed is a solar sail structure finite element modeling and post-processing method. The solar sail structure finite element modeling and post-processing method includes: 1), setting a solar sail configuration mode and a connecting format of a support arm and a sail surface and reserving an area for the support arm; 2), establishing a solar-sail geometric model with the preserved area; 3), setting a support arm model and generating a support-arm geometric model in the reserved area; 4), establishing finite element models of the solar sail surface and the support arm; 5), subjecting the solar sail surface and the support arm to finite element mode assembly according to the generated infinite element models of the solar sail surface and the support arm; 6), setting statics boundary conditions and loading conditions on the finite element models; 7), calculating buckling load of the support arm, simulating reverse acceleration speed released by the inertia, and exerting the reverse acceleration speed on the infinite element models; 8), analyzing statics of a solar sail to acquire maximum deformation and axial pressure of the support arm; 9), calculating buckling safety factors and structuring feasibility of a solar sail structural scheme according to the buckling safety factors.

Description

technical field [0001] The invention relates to a fast modeling and post-processing method of a structure finite element, and is especially suitable for analyzing the mechanical characteristics of a large super-flexible solar sail structure connected by a support arm and a film. Background technique [0002] A solar sail is a spacecraft that uses the sun's reflected light pressure on a large area of ​​film to provide flight power. As long as there is sunlight, it can continue to accelerate, and eventually achieve a much greater speed than ordinary spacecraft. It is not limited by fuel and can run in space for a longer time, so solar sail spacecraft The generation of the space is of great significance to the future space exploration. [0003] The light pressure points to the normal direction of the solar sail, so by controlling the angle between the solar sail and the sun's rays, the magnitude of the light pressure can be changed, and the light pressure can be turned into a ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
CPCY02E60/00
Inventor 杨辰刘宇飞张兴华侯欣宾王立
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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