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Ansys Ls-Dyna-based ball load service module falling analysis method

An analysis method and service cabin technology, applied in the field of load service cabin equipment, can solve problems such as high requirements for test models and environment construction, difficulty in simulating the load cabin fall process, and inability to perform effective analysis, so as to improve analysis accuracy and reduce The cost of experimentation and the effect of easy construction

Pending Publication Date: 2022-07-08
AEROSPACE INFORMATION RES INST CAS
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Problems solved by technology

[0004] The present invention provides a method for analyzing the fall of a spherical load service cabin based on Ansys Ls-Dyna. The whole analysis time is short, and the analysis efficiency and accuracy are improved, so as to overcome the long analysis period and experimental cost in the prior art. It is relatively high, and has high requirements for the test model and environment construction, and it is difficult to simulate the load cabin fall process, which leads to the problem that effective analysis cannot be carried out

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  • Ansys Ls-Dyna-based ball load service module falling analysis method
  • Ansys Ls-Dyna-based ball load service module falling analysis method
  • Ansys Ls-Dyna-based ball load service module falling analysis method

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Embodiment Construction

[0023] To make the purposes, technical solutions, and advantages of the embodiments of the present invention clearer, the following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention.

[0024] like figure 1 As shown, the fall analysis method of the ball-borne load service cabin based on Ansys Ls-Dyna of the present invention comprises the following steps:

[0025] Step S1: establishing a three-dimensional structural model of the spherical load service cabin in CAD software, and preprocessing the three-dimensional structural model to obtain a structural model of the spherical load service cabin.

[0026] In this step, CAD software, preferably Solidworks 3D structural software, is used to establish a 3D structural model for the structure of the spherical load service cabin, and preprocessing the established 3D structural model, including: ...

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Abstract

According to the method, on the basis of an Ansys software platform, the finite element model of the ball load service module is established for falling analysis, coarse mesh division is used during primary analysis, the mesh division time can be shortened, the whole analysis time can be saved, the finite element analysis rate can be increased, and an analysis result can be obtained quickly; and when the analysis result meets the falling requirement, grid optimization is carried out on the whole model according to a finite element grid inspection standard, so that the accuracy of the analysis result is improved. According to the method, the problems that in the prior art, the analysis period is long, the experiment cost is high, the requirement for building a test model and an environment is high, and effective analysis cannot be carried out due to the fact that simulation of the falling process of the load cabin is difficult are solved.

Description

technical field [0001] The invention relates to the field of load service cabin equipment, in particular to a fall analysis method of a ball load service cabin based on Ansys Ls-Dyna. Background technique [0002] Near space generally refers to the airspace with a height of (20-100) km, which refers to a special position between aviation and aerospace airspace. The near space payload service module is an opto-mechatronics device, which will carry high-altitude balloons to near space for scientific experiments. In order to ensure the follow-up processing of scientific experiments, the payload service module will return to the ground at a specific speed after completing the scientific task in the adjacent space. Considering that at the moment of landing, the collision with the ground will affect the stability of the payload service module. Therefore, , In order to recover the relevant instruments and equipment in the load service cabin, it is necessary to analyze the safety o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/23G06T17/00G06T17/20G06F111/04G06F119/14
CPCG06F30/23G06T17/00G06T17/205G06T17/20G06F2119/14G06F2111/04Y02T90/00
Inventor 钱路路王光明赵益昕王占超黄旻
Owner AEROSPACE INFORMATION RES INST CAS
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