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An Actively Controlled Shape-Morphing Compliant Microarchitectured Material

机译:主动控制形状变形的微体系结构材料

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The purpose of this paper is to introduce a new kind of microarchitectured material that utilizes active control to alter its bulk shape through the deformation of its compliant elements. This new kind of microarchitectured material achieves its reconfigurable shape capabilities through a new control strategy that utilizes linearity and closed-form analytical tools to rapidly calculate the optimal internal actuation effort necessary to achieve a desired bulk surface profile. The kind of microarchitectured materials introduced in this paper is best suited for high-precision applications that would benefit from materials that can be programed to rapidly alter their surface or shape by small repeatable amounts in a controlled manner. Examples include distortion-correcting surfaces on which precision optics are mounted, airplane wings that deform to increase maneuverability and fuel efficiency, and surfaces that rapidly reconfigure to alter their texture. In this paper, the principles are provided for optimally designing 2D or 3D versions of the new kind of microarchitectured material such that they exhibit desired material property directionality. The mathematical theory is provided for modeling and calculating the actuation effort necessary to drive these materials such that their lattice shape comes closest to achieving a desired profile. Case studies are provided to demonstrate the utility of this theory and finite-element analysis (FEA) is used to verify the results.
机译:本文的目的是介绍一种新型的微结构材料,该材料利用主动控制通过其顺应元素的变形来改变其整体形状。这种新型的微体系结构材料通过一种新的控制策略来实现其可重构的形状功能,该控制策略利用线性和闭合形式的分析工具快速计算出实现所需整体表面轮廓所需的最佳内部驱动力。本文介绍的这种微体系结构材料最适合于高精度应用,这些应用将受益于可以编程的材料,这些材料可以通过编程以受控的方式以少量的可重复量快速改变其表面或形状。例如,在其上安装了精密光学器件的畸变校正表面,变形以提高机动性和燃油效率的飞机机翼,以及迅速重新配置以改变其质地的表面。在本文中,提供了用于最佳设计新型微体系结构材料的2D或3D版本的原理,以使其表现出所需的材料特性方向性。提供了数学理论,用于建模和计算驱动这些材料以使它们的晶格形状最接近于实现所需轮廓所需的驱动力。提供了案例研究来证明此理论的实用性,并使用有限元分析(FEA)来验证结果。

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