产品数字孪生概念方面的几何建模

A. Nezenko, S. Kozlov
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引用次数: 0

摘要

分析了飞机设计几何参数在生产阶段的再现特点。由于各种客观和主观因素对产品几何参数变化的影响,在单件生产和飞机总装中突出的问题。这些因素可以是环境温度的波动、材料的内应力、误差的累积和设计计算中的不准确性等等。利用数字孪生的概念,通过创建一系列具有实际几何参数的几何模型,确定了对几何参数变化问题的综合解决方案。结果表明,飞机外轮廓几何模型序列是其数字孪生的重要组成部分,是设计不同技术路径模型的基础。提出了利用基于过程的几何建模方法,应用结构参数化建模方法创建飞机数字孪生体的几何模型序列。研究表明,在生产阶段创建产品实际几何参数的几何模型的方法不同于在研究和开发阶段用于几何建模的方法。在飞机生产的每个阶段,设计和技术部门在创建飞机单元实际几何参数模型时,考虑了面临的一些主要问题。为解决飞机制造过程中几何参数变化问题,确定了进一步研究几何建模方法的总体方向。所提供的材料是为计算机辅助设计开发适当的几何模型和软件工具的基础。
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GEOMETRIC MODELING IN THE ASPECT OF PRODUCT DIGITAL TWIN CONCEPT
Features of reproducing aircraft design geometric parameters during the production stage analyzed in the presented study. Problematic issues highlighted on unit production and aircraft final assembly due to the influence of various objective and subjective factors on variations of geometric parameters of a product. Such factors can be fluctuations in the ambient temperature, internal stresses of the material, the accumulation of errors, and inaccuracies in design calculations, et cetera. Lines determined for comprehensive solutions of problems on geometric parameters variations by creating a sequence of geometric models with actual geometric parameters using the concept of a digital twin. It was demonstrated that the geometric model sequence of aircraft outer contours is an integral component of its digital twin and the basis for the designing of models of different technical paths. It was proposed to apply the methodology of structural-parametric modeling using approaches of process-based geometric modeling to create the sequence of geometric models of an aircraft digital twin. It was demonstrated that approaches to the creation of geometric models of a product actual geometric parameters at the production stage are different from methods used for geometric modeling at the steps of research and development. A number of the main issues were considered that facing the design and technological departments when creating models of actual geometric parameters of aircraft units at each stage of its production. The general directions were determined for further research of geometric modeling methods to solve the problems of changing geometric parameters during the manufacturing of aircraft. The materials presented serve as the basis for the development of appropriate geometric models and software tools for computer-aided design.
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