航空制造技术2024,Vol.67Issue(16) :138-146.DOI:10.16080/j.issn1671-833x.2024.16.138

基于矩独立法的异质叠层复合材料铆接工艺参数灵敏度分析研究

Sensitivity of Riveting Parameters of Heterogeneous Laminated Composites Based on Moment Independence Method

殷俊清 孙鹏涛 郭彧瑞 张祎增 郭飞燕
航空制造技术2024,Vol.67Issue(16) :138-146.DOI:10.16080/j.issn1671-833x.2024.16.138

基于矩独立法的异质叠层复合材料铆接工艺参数灵敏度分析研究

Sensitivity of Riveting Parameters of Heterogeneous Laminated Composites Based on Moment Independence Method

殷俊清 1孙鹏涛 1郭彧瑞 1张祎增 1郭飞燕2
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作者信息

  • 1. 西安工程大学,西安 710600
  • 2. 北京科技大学,北京 100083
  • 折叠

摘要

为解决碳纤维增强复合材料(Carbon fiber reinforced polymer,CFRP)与金属材料叠层构件铆接工艺复杂化的问题,提出了 一种基于矩独立方法的叠层复合材料铆接工艺参数灵敏度分析的方法.首先,以CFRP与铝合金(Al)异质叠层材料结构为研究对象,采用有限元方法建立了 CFRP/A1叠层结构的铆接仿真分析模型,并通过试验验证了仿真分析模型的正确性.其次,以铆接干涉量为目标,建立了基于随机森林方法的铆接工艺参数代理模型;随后通过代理模型进行数据扩展,以17项铆接工艺参数为输入变量,铆接干涉量为输出变量,采用基于矩独立的PAWN方法进行全局灵敏度分析,并给出了基于该方法的灵敏度系数.在铆接工艺参数对铆接干涉量的全局灵敏度系数中,异质叠层复合材料的弹性模量和厚度的灵敏度系数较大,分别为0.16921和0.11837,其次是系数为0.012的位移载荷和0.011的铆钉直径.其余工艺参数的灵敏度系数较小,一些对铆接干涉量影响很不显著的参数的灵敏度系数接近0.

Abstract

In order to solve the problem that the riveting process of carbon fiber reinforced polymer(CFRP)and metal material laminated components is more complicated than that of a single material,a method for sensitivity analysis of the riveting process parameters of laminated composites based on the method of moment-independent PAWN is proposed.Firstly,taking CFRP and aluminum alloy(Al)heterogeneous laminated composite structure as the research object,the simulation and analysis model of riveting CFRP/Al laminated structure is established by using the finite element method,and the correctness of the simulation and analysis model is verified by experiments.Secondly,a proxy model of riveting process parameters based on the random forest method is established with the riveting interference amount as the target;furthermore,data extension is carried out through the proxy model,and a global sensitivity analysis based on the moment-independent PAWN method is carried out with 17 riveting process parameters as input variables and the riveting interference amount as the output variable,and the sensitivity coefficients based on this method are given.Among the global sensitivity coefficients of riveting process parameters on riveting interference amount,the sensitivity coefficients of elasticity modulus and thickness of the heterogeneous laminated composites are 0.16921 and 0.11837,respectively,followed by the coefficients of 0.012 for the displacement load and 0.011 for the rivet diameter.The values of other process parameters are small,and the sensitivity coefficients of some parameters that have insignificant effects on the riveting interference amount are close to zero.

关键词

叠层复合材料/有限元方法/铆接干涉量/随机森林代理模型/矩独立全局灵敏度分析

Key words

Laminated composites/Finite element method/Riveting interference amount/Random forest proxy model/Global sensitivity analysis based on moment independence

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基金项目

航空科学基金(ASFC-20200016111001)

国家自然科学基金(52175450)

出版年

2024
航空制造技术
北京航空制造工程研究所

航空制造技术

CSTPCD北大核心
影响因子:0.403
ISSN:1671-833X
参考文献量2
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