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一种用于复合材料层压板固化诱导变形的分析模型。

An Analytical Model for Cure-Induced Deformation of Composite Laminates.

作者信息

Peng Xiaobo, Xu Jiang, Cheng Yong, Zhang Long, Yang Jie, Li Yinghui

机构信息

School of Mechanics and Aerospace Engineering, Southwest Jiaotong University, Chengdu 610031, China.

AVIC Chengdu Aircraft Industry (Group) Co., Ltd., Chengdu 610091, China.

出版信息

Polymers (Basel). 2022 Jul 17;14(14):2903. doi: 10.3390/polym14142903.

Abstract

Curing deformation prediction plays an important role in guiding the tools, curing process design, etc. Analytical methods can provide a rapid prediction and in-depth understanding of the curing deformation mechanism. In this paper, an analytical model is presented to study the cure-induced deformation of composite laminates. Based on the classical laminate theory, the thermal stress and deformation of composites during the curing process are calculated by considering the evolution of the mechanical properties of resin. Additionally, the coupling stiffness of the laminate is taken into consideration in the analytical model. An interface layer between the tool and the part is developed to simulate the variation of the tool-part interaction with the degree of resin cure. The maximum curing deformations and deformation profiles of different lay-up composite parts predicted by the proposed model are compared with the results of the finite element method and previous literature reports. Then, a comprehensive parametric study is carried out to investigate the influence of curing cycle, geometry, tool thermal expansion, and resin characteristics on the curing deformation of composite parts. The results reveal that geometry has a significant influence on the curing deformation of composite parts, but for dimensionally determined parts, curing deformation is mainly attributable to their own anisotropy in macro and micro aspects, as well as the stretching effect of the tool on the part. The percentage contribution of different factors to curing deformation composites with different lay-ups and geometries is also discussed.

摘要

固化变形预测在指导工装、固化工艺设计等方面起着重要作用。解析方法能够对固化变形机理进行快速预测并深入理解。本文提出了一种解析模型来研究复合材料层合板的固化诱导变形。基于经典层合板理论,通过考虑树脂力学性能的演变来计算复合材料在固化过程中的热应力和变形。此外,解析模型中还考虑了层合板的耦合刚度。在工装和部件之间建立了一个界面层,以模拟工装与部件的相互作用随树脂固化程度的变化。将所提模型预测的不同铺层复合材料部件的最大固化变形和变形轮廓与有限元方法的结果以及先前文献报道进行了比较。然后,开展了全面的参数研究,以考察固化周期、几何形状、工装热膨胀和树脂特性对复合材料部件固化变形的影响。结果表明,几何形状对复合材料部件的固化变形有显著影响,但对于尺寸确定的部件,固化变形主要归因于其在宏观和微观方面自身的各向异性以及工装对部件的拉伸作用。还讨论了不同因素对不同铺层和几何形状的固化变形复合材料的贡献百分比。

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