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Shell simulation model rapid extraction method and system based on satellite deck structure

A simulation model and extraction method technology, applied in design optimization/simulation, geometric CAD, special data processing applications, etc., can solve problems such as a lot of time and reduce model construction efficiency, and achieve the effect of improving convenience and speed of iteration

Pending Publication Date: 2022-05-13
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, this patent needs to calculate the space cabin information before modeling, which takes a lot of time when the model is complex, which reduces the efficiency of model construction

Method used

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  • Shell simulation model rapid extraction method and system based on satellite deck structure
  • Shell simulation model rapid extraction method and system based on satellite deck structure
  • Shell simulation model rapid extraction method and system based on satellite deck structure

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Experimental program
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Effect test

Embodiment

[0042] According to the method for quickly extracting the shell simulation model based on the satellite deck structure provided by the present invention, it includes: step 1: start the Pro / E software environment, open the deck three-dimensional skeleton model; step 2: copy the outline of the deck, and output the stand-alone, load Information, determine the outer contour envelope; Step 3: Screen and reserve the required holes on the deck; Step 4: Extend the lapped face group; Step 5: Assemble, group and output the shell simulation model.

[0043] Copy and create the deck outline in the form of published geometry, and judge and filter out the single machine and load information required for deck simulation according to the preset configuration conditions and output them, including name, mass, center of mass position and mounting foot position, on the deck Add the quilt feature of the outline of the outer deck to the 3D skeleton model, determine the envelope of the outer outline o...

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PUM

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Abstract

The invention provides a shell simulation model rapid extraction method and system based on a satellite deck structure, and the method comprises the steps: 1, starting a Pro / E software environment, and opening a deck three-dimensional skeleton model; 2, copying a cabin plate contour, outputting single machine and load information, and determining an external contour envelope; 3, holes needed in the deck are screened and reserved; 4, the lap joint face set is extended; and 5, assembling, grouping and outputting a shell simulation model. According to the method, the shell of the cabin plate three-dimensional model is rapidly extracted, the obstacle of the digital technology between design and simulation is broken through, the three-dimensional model information is rapidly and effectively transmitted and fed back to the simulation modeling process in a lossless mode, the satellite simulation efficiency is improved, and the cost is reduced.

Description

technical field [0001] The invention relates to the technical field of aerospace vehicle structures, in particular to a method and system for quickly extracting a shell simulation model based on a satellite deck structure. Background technique [0002] At present, the development of satellites is faced with the situation of simultaneous development of multiple models, high-density launches, high quality and reliability requirements, and short development cycle requirements. High-quality, high-efficiency, and high-benefit satellite structure design is required, which requires refined and rapid structural design simulation, and the ability to quickly adapt to structural design changes and continuously iterate. [0003] The existing satellite simulation modeling methods are basically separated from the 3D design, requiring designers to handle the transfer of design information between design and simulation. In order to solve the above problems, the object of the present invent...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/15G06F30/20
CPCG06F30/15G06F30/20
Inventor 姚骏程尧王开浚张宗华许斌顾志悦
Owner SHANGHAI SATELLITE ENG INST