机翼长桁数字孪生模型构建及可视化研究OA
Research on the Construction and Visualization of Digital Twin Models of Wing Truss
机翼壁板的强度与疲劳试验能保障飞机在飞行过程中的安全性,但在试验中存在无法确定机翼下壁板的准确性能以及含孔部位孔边力学参数测量难等问题.本文研究了机翼下壁板长桁结构数字孪生模型的构建及可视化方法.首先进行了长桁含孔部位的力学理论分析以及有限元数值仿真,建立了长桁含孔部位的有限元模型;结合响应面优化方法对有限元模型进行网格降阶,得到降阶模型;然后以多种工况下的仿真数据作为数据模型的训练数据集进行数据模型的训练,构建了长桁含孔部位的数字孪生模型;最后以某开发软件为数字孪生引擎,搭建数字孪生模型可视化平台,得到在虚拟加载条件下长桁含孔部位的应力场、应变场以及结构变形.
The strength and fatigue tests of the wing lower panels ensure the safety of the aircraft during flight.However,there are issues in the tests,such as the inability to accurately determine the performance of the wing lower panels and the measurement of mechanical parameters at the hole edges in regions with holes.This paper investigates the construction and visualization methods of a digital twin model of the wing lower wall panel truss structure.Firstly,the mechanical mechanism analysis and finite element numerical simulation of the section with holes in the truss were conducted,and the mechanism model and finite element model of the section with holes in the truss were established;Combining response surface optimization method to reduce the mesh order of the finite element model,a reduced order model was obtained;Subsequently,simulation data from various operating conditions were used as the training dataset for the data model,and a digital twin model of the long truss with holes was constructed.Finally,Unity game development software was used as the digital twin engine to build a digital twin model visualization platform,which realized the stress field,strain field,and structural deformation of the long truss with holes under virtual loading conditions.
郭蔡果荟;于翀;李博;孟薇;张鹤宇
航空工业北京长城计量测试技术研究所,北京 100095航空工业北京长城计量测试技术研究所,北京 100095航空工业北京长城计量测试技术研究所,北京 100095航空工业北京长城计量测试技术研究所,北京 100095航空工业北京长城计量测试技术研究所,北京 100095
航空航天
疲劳试验长桁数字孪生可视化虚拟试验
fatigue testlong trussdigital twinvisualizationvirtual experiment
《航空科学技术》 2026 (5)
102-110,9
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