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典型复合材料结构固化变形仿真预测与控制验证

杨智勇 左小彪 范春浩 易美军 鲍益东 王超 胡俊山 李艳

宇航材料工艺2024,Vol.54Issue(2):54-61,8.
宇航材料工艺2024,Vol.54Issue(2):54-61,8.DOI:10.12044/j.issn.1007-2330.2024.02.006

典型复合材料结构固化变形仿真预测与控制验证

Simulation Prediction and Control Verification of Curing Deformation on Typical Composite Structure

杨智勇 1左小彪 1范春浩 2易美军 1鲍益东 2王超 1胡俊山 2李艳1

作者信息

  • 1. 航天材料及工艺研究所,北京 100076
  • 2. 南京航空航天大学机电学院,南京 210016
  • 折叠

摘要

Abstract

In response to the problem of difficult control of deformation during the curing process of typical composite material structures,the curing deformation of typical composite structures was simulated and predicted,and the curing deformation was controlled and verified from two aspects:curing process and die compensation.In terms of curing process,the optimal curing process curve was determined based on the deformation data of each design point.In terms of mold compensation,a method of adaptive adjustment of the finite element model of the component was proposed.A collaborative control method based on global compensation was adopted to comprehensively consider the curing process parameters and mold surface compensation.The results show that the solidification deformation error of L-shaped components through simulation is 12.4%.The optimal solidification process curve of L-shaped components obtained by response surface optimization algorithm has a deviation of no more than 3.3%between the predicted solidification deformation value and the minimum maximum deformation value at each experimental design point.After adaptive adjustment of the T-shaped reinforced wall panel finite element model,the maximum relative error between the numerical simulation value and the experimental measurement value for the deviation distance between the lower surface and the target profile is 17.20%.The mold of the semi cylindrical wall panel is compensated by the collaborative control method of global compensation,and the maximum curing deformation is reduced by nearly 90%compared with the traditional single mold surface compensation control method.

关键词

固化变形/仿真预测/最优固化工艺/自适应调整/协同控制/验证

Key words

Curing deformation/Simulation and prediction/The optimal curing process/Adaptive adjustment/Synergetic control/Verification

分类

通用工业技术

引用本文复制引用

杨智勇,左小彪,范春浩,易美军,鲍益东,王超,胡俊山,李艳..典型复合材料结构固化变形仿真预测与控制验证[J].宇航材料工艺,2024,54(2):54-61,8.

基金项目

基础科研计划项目 ()

宇航材料工艺

OA北大核心CSTPCD

1007-2330

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