一种虚拟试验架构下的舱段结构建模与承载破坏模拟技术  

Modeling and Bearing Damage Simulation Methodology for Cabin Structure in a Virtual Test Framework

作　　者：王成华[1] 蒋雯霄 杨阳[1] 李磊[1] WANG Chenghua;JIANG Wenxiao;YANG Yang;LI Lei(Beijing Institute of Space Long March Vehicle,Beijing,100076)

机构地区：[1]北京航天长征飞行器研究所,北京100076

出　　处：《导弹与航天运载技术（中英文）》2024年第2期74-79,99,共7页Missiles and Space Vehicles

摘　　要：在一种面向产品的飞行器结构强度虚拟试验架构下,发展经典材料弹塑性损伤本构和通用有限元技术,并基于Abaqus内置Python软件开发虚拟试验插件工具,创建飞行器舱段结构人机交互虚拟试验平台,形成了对舱段结构承载破坏过程进行高逼真度模拟的虚拟试验能力。采取逐级验模的精度确认技术,开展从试棒到舱段壳体的虚/实试验对比,验证舱段结构虚拟试验的可行性,结果显示:虚拟试验能对舱段结构的承载破坏情况做高逼真度的模拟,对极限承载能力的预示精度达到4.6%。A product-oriented virtual test framework for structural strength of aircraft bodies is proposed,under which the classical elastic-plastic damage constitutive of materials and general finite element technology are developed,and a human-computer interactive virtual test platform for aircraft cabin structure is created based on the virtual test plug-in tool developed by Abaqus built-in Python software.Using the accurate confirmation technology of step-by-step inspection,the virtual/real test comparison from the specimen to the complex cabin is carried out to verify the feasibility of the virtual test of the cabin structure.The results show that the virtual test can simulate the load-bearing failure of the cabin structure with high fidelity,and the prediction accuracy of the ultimate load-bearing capacity is 4.6%.

关 键 词：虚拟试验 舱段结构 承载破坏 测试验证 塑性损伤 

分 类 号：TB330.1[一般工业技术—材料科学与工程] V475[航空宇航科学与技术—飞行器设计]