形状记忆聚合物的电-热-力学耦合建模

Midhan Siwakoti, Russell W. Mailen
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引用次数: 1

摘要

形状记忆聚合物(SMPs)因其应变恢复率高、成本低、活化能低等特点,在自折叠折纸领域得到了广泛的研究。smp利用粘弹性材料的特性来改变形状,以响应施加的刺激,例如光或电。由于其更高的能量密度和更短的响应时间,电气驱动是可取的。以往的研究报道了在特定的外加电压或电流条件下导电聚合物复合材料形状恢复的实证结果,这需要严格的实验。在这里,我们引入了一个能够预测电驱动smp的电-热-机械耦合响应的有限元框架。作为输入,该框架需要材料性能,如电导率和粘弹性参数。粘弹性响应采用符合实验动态力学分析(DMA)数据的proony序列模型来实现。利用这一框架,我们预测了受各种热、电和机械载荷影响的电动smp的形状恢复行为,并评估了响应对材料性能的敏感性。此外,我们还展示了材料预拉伸条件和局部导电途径对形状恢复和自折叠的影响。该计算框架提供了对电驱动smp的电-热-机械响应的基本理解,可用于设计航空航天应用的电驱动自折叠折纸。
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Coupled Electro-Thermo-Mechanical Modeling of Shape Memory Polymers
Shape memory polymers (SMPs) are extensively studied for self-folding origami due to their large strain recovery, low cost, and low activation energy. SMPs utilize viscoelastic material behavior to change shape in response to an applied stimulus, for instance light or electricity. Electrical actuation is desirable due to its higher energy density and shorter response time. Previous studies reported empirical results on shape recovery of conductive polymer composites actuated by specific applied voltage or current conditions, which required rigorous experimentation. Here, we introduce a finite element framework capable of predicting the coupled electro-thermo-mechanical response of electrically actuated SMPs. As inputs, this framework requires material properties, such as electrical conductivity and viscoelastic parameters. The viscoelastic response is implemented using a Prony series model that is fit to experimental dynamic mechanical analysis (DMA) data. Using this framework, we predict the shape recovery behavior of electrically actuated SMPs subject to various thermal, electrical, and mechanical loads and evaluate the sensitivity of the response to the material properties. Additionally, we show the effects of material pre-straining conditions and localized conductive pathways on shape recovery and self-folding. This computational framework provides a fundamental understanding of the electro-thermo-mechanical response of electrically actuated SMPs and can be used to design electrically actuated self-folding origami for aerospace applications.
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