复合材料学报2024,Vol.41Issue(9) :4765-4777.DOI:10.13801/j.cnki.fhclxb.20240423.003

基于人工神经网络的固体推进剂细观损伤与宏观刚度映射关系

Artificial neural network-based mapping of microscopic damage to macroscopic stiffness in solid propellants

张滔韬 杨玉新 张二晗 校金友 吕海宝 文立华 雷鸣 侯晓
复合材料学报2024,Vol.41Issue(9) :4765-4777.DOI:10.13801/j.cnki.fhclxb.20240423.003

基于人工神经网络的固体推进剂细观损伤与宏观刚度映射关系

Artificial neural network-based mapping of microscopic damage to macroscopic stiffness in solid propellants

张滔韬 1杨玉新 2张二晗 3校金友 3吕海宝 4文立华 3雷鸣 3侯晓5
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作者信息

  • 1. 西北工业大学 航天学院,西安 710072;西安航天动力技术研究所,西安 710025
  • 2. 西安航天动力技术研究所,西安 710025
  • 3. 西北工业大学 航天学院,西安 710072
  • 4. 哈尔滨工业大学 复合材料与结构研究所,哈尔滨 150001
  • 5. 中国航天科技集团公司,北京 100048
  • 折叠

摘要

作为一种高夹杂比颗粒增强聚合物基复合材料,固体推进剂的宏观力学性能主要由其细观结构决定.外加载荷下,初始缺陷或细观颗粒团聚均可诱发局部应力集中,导致颗粒-基体细观界面脱粘,材料宏观力学性能劣化.如何构建细观损伤与宏观性能间的映射关系,已成为推进剂细观实验结果合理运用、固体火箭发动机结构灾变准确预报的关键.为此,本文发展了基于连续介质力学框架的人工神经网络,以变形梯度的不变量为输入、自由能为输出,遴选现有自由能函数和损伤增长函数形式为神经网络设计激活函数,使神经网络先验地满足变形连续性、坐标不变性、热力学一致性等要求.基于上述物理相容性,神经网络能在稀疏训练数据条件下快速收敛,还能够自下而上地实现损伤状态的遗传映射.最后,采用有限元分析获取的数据集,验证了该网络模型对不同预损伤下的推进剂在单轴拉伸、等双轴拉伸、纯剪切3种加载条件下的宏观刚度预报能力.

Abstract

As a particle-reinforced polymer composite with high inclusion ratio,the macro-mechanical properties of solid propellants depend on their meso-structures.Especially,under external loads,the stress concentration usually happens besides the regions of the initial imperfections and the particle agglomerations,leading to the in-terfacial debonding between the particles and the polymeric binders,consequently deteriorating macroscopic mechanical properties.How to build a relationship between the microscopic damage states and the macroscopic mechanical performances is the key issue for both the rational usage of the microscopic experimental results of solid propellants and the accurate prediction of structural disasters in solid rocket motors.For this purpose,this article develops an artificial neural network(ANN)based on the framework of continuum mechanics,with the scalar invariant of the deformation gradient tensor as the input and the scalar free energy as the output.Existing free energy functions and damage growth functions are selected as the activation functions of the ANN,and therefore the ANN can naturally satisfy the requirements of the continuum mechanics,including the deformation continuity,the coordinate invariance,and the thermodynamic consistency.These merits can guarantee the rapid convergence of the ANN with sparse training data,and additionally can obtain a bottom-up mapping of the microscopic damage states towards the macroscopic mechanical performances.Finally,using the dataset obtained from finite element analysis,the predictive ability of the ANN on the mechanical properties of solid propellants with different pre-damage states under uniaxial tension,biaxial tension,and pure shear are validated.

关键词

固体推进剂/力学本构关系/人工神经网络/细观损伤/细-宏观映射

Key words

solid propellants/constitutive model/artificial neural network/microscopic damage/macroscopic and microscopic scale-effect

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基金项目

国家自然科学基金-联合基金资助项目(U22B20131)

出版年

2024
复合材料学报
北京航空航天大学 中国复合材料学会

复合材料学报

CSTPCDCSCD北大核心
影响因子:0.933
ISSN:1000-3851
参考文献量2
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