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Three-dimensional effect enhancement visualization method based on grids

A grid and three-dimensional technology, applied in the field of grid-based enhanced visualization of three-dimensional effects, can solve the problems of high difficulty in secondary development, slow operation response, and large amount of calculation, etc., and achieve the effect of simple and efficient composition calculation

Active Publication Date: 2021-03-23
CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA
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AI Technical Summary

Problems solved by technology

The design of aircraft mechanical and electrical systems includes a large number of aircraft pipe networks and finished products. A software for the design of aircraft electromechanical systems focuses on the design of system architecture and logical relationships. A visualization method for visual expression. This application scenario has low requirements for size, position, and light and shadow rendering accuracy. Traditional 3D rendering engine technology is directly used, which requires a large amount of calculation, slow operation response, and high difficulty in secondary development.

Method used

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  • Three-dimensional effect enhancement visualization method based on grids

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Embodiment Construction

[0030] Based on the existing three-dimensional digital model of aircraft structure and system, the present invention first provides a perspective grid definition method for producing perspective effects, and then defines the aircraft structure, system equipment, and pipe network used to express the internal space of the aircraft The location and picture size method of the two-dimensional vector diagram in the grid, and finally define the occlusion principle of the structure, pipe network and equipment graphics in the grid, and finally realize the enhanced display of the three-dimensional effect of the electromechanical system equipment and pipe network based on the grid. The method is based on the following characteristics:

[0031] 1) The invention contains a set of grids as a background for visualization

[0032] 2) The components in this invention include a vector image and a set of interface coordinate data

[0033] 3) The component visualization elements in this inventio...

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Abstract

The invention belongs to the technical field of image display, and discloses a three-dimensional effect enhancement visualization method based on grids. On the basis of an existing airplane structureand system three-dimensional digital analogy, a perspective grid definition method used for generating a perspective effect is firstly provided, and then a method used for expressing the position andpicture size of an airplane body structure, system equipment and a pipe network two-dimensional vector diagram of an airplane internal space in a grid is defined. And finally, a shielding principle ofthe structure, the pipe network and the equipment graph in the grid is defined, and finally grid-based three-dimensional effect enhanced display of the electromechanical system equipment and the pipenetwork is achieved.

Description

technical field [0001] The invention belongs to the technical field of image display, in particular to a grid-based three-dimensional effect enhanced visualization method. Background technique [0002] The 3D visualization software has powerful spatial expression capabilities, relies on a powerful 3D rendering engine, and its size and position accuracy is high, which can provide designers with almost what you see is what you get rendering effect. The design of aircraft mechanical and electrical systems includes a large number of aircraft pipe networks and finished products. A software for the design of aircraft electromechanical systems focuses on the design of system architecture and logical relationships. The visualization method of visual expression. This application scenario has low requirements on the size, position and rendering accuracy of light and shadow. The traditional 3D rendering engine technology is directly used, which requires a large amount of calculation, s...

Claims

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Application Information

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IPC IPC(8): G06T17/00G06T15/00
CPCG06T17/00G06T15/005
Inventor 陈川刘永绩吴建军何朝阳
Owner CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA
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