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数字孪生驱动的结构全场变形高精度反演方法

黄熠玮 耿一斌 高天贺 胡轩玮 王圆 马红艳 田阔

航空学报2025,Vol.46Issue(19):118-129,12.
航空学报2025,Vol.46Issue(19):118-129,12.DOI:10.7527/S1000-6893.2024.30967

数字孪生驱动的结构全场变形高精度反演方法

Digital twin driven high precision reconstruction method for full-field deformation of structure

黄熠玮 1耿一斌 2高天贺 1胡轩玮 1王圆 3马红艳 1田阔4

作者信息

  • 1. 大连理工大学 工程力学系,大连 116024
  • 2. 中国商飞上海飞机设计研究院,上海 201210
  • 3. 神州五行航天科技有限公司,大连 116085
  • 4. 大连理工大学 工程力学系,大连 116024||辽宁省飞行器结构强度数字孪生重点实验室,沈阳 110035
  • 折叠

摘要

Abstract

To address the issue that traditional direct and indirect deformation monitoring methods are difficult to meet the requirements of high-precision real-time deformation monitoring of structures,a digital twin-driven high-precision re-construction method for full-field deformation of structure is proposed.Firstly,a multi-directional digital twin strain field is constructed by integrating simulation and measured strain data,which reduces the influence of load deviation and other factors on the simulation reliability,and ensures the strain accuracy of the deformation reconstruction.Secondly,a modal coordinate solving and deformation reconstruction method considering multi-directional strain is proposed.By incorporating multi-directional strain in the modal coordinate solving process,this method solves the problem of insuffi-cient stability of the reconstruction results when single-directional strain is used,and improves the stability of the full-field deformation reconstruction of the structure.Finally,based on the proposed method,the experimental validation is carried out with the wing structure,and the results are compared with the simulation and the deformation reconstruc-tion results of the traditional modal superposition method.The result shows that the proposed method has a higher ad-vantage of reconstruction accuracy in the place of large deformation.The relative error between the reconstruction re-sults of the proposed method and the measured deformation is less than 0.8%,and the absolute error is less than 0.09 mm,which is 7%and 12%lower than that of the traditional modal method and the simulation method,respec-tively.At the same time,the average relative error of the proposed method for deformation reconstruction at multiple measurement points is 1.2%,which is 5.7%and 9.3%lower than that of the traditional modal method and simulation analysis method,respectively.Moreover,when the number of strain gauges is small,the deformation reconstruction accuracy of the proposed method is improved by more than one order of magnitude compared with the traditional modal superposition method,which indicates that the proposed method has higher deformation reconstruction accu-racy and stability.

关键词

数字孪生/变形反演/模态叠加/数据融合/机翼结构

Key words

digital twin/deformation reconstruction/modal superposition/data fusion/wing structure

分类

航空航天

引用本文复制引用

黄熠玮,耿一斌,高天贺,胡轩玮,王圆,马红艳,田阔..数字孪生驱动的结构全场变形高精度反演方法[J].航空学报,2025,46(19):118-129,12.

基金项目

辽宁省人工智能领域科技重大专项(2023JH26/10100007) (2023JH26/10100007)

辽宁省优秀青年基金(2024JH3/10200003) (2024JH3/10200003)

国家重点研发计划(2022YFB3404700) Major Science and Technology Projects in the Field of Artificial Intelligence of Liaoning Province(2023JH26/10100007) (2022YFB3404700)

Excellent Youth Fund under the Science and Technology Program of Liaoning Province(2024JH3/10200003) (2024JH3/10200003)

National Key Research and Development Program of China(2022YFB3404700) (2022YFB3404700)

航空学报

OA北大核心

1000-6893

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