Towards Fatigue-tolerant Design of Additively Manufactured Strut-based Lattice Metamaterials

N. Apetre, A. Arcari, John Michopoulos, Evan Strickland, Steven N. Rodriguez, Athanasios P. Iliopoulos, J. Steuben, Benjamin D. Graber
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Abstract

The advent of additive manufacturing (AM) has enabled the prototyping of periodic and non-periodic metamaterials (a.k.a. lattice or cellular structures) that could be deployed in a variety of engineering applications where certain combinations of performance features are desirable. For example, these structures could be used in a variety of naval engineering applications where light-weight, large surface area, energy absorption, heat dissipation, and acoustic bandgap control are desirable. Furthermore, combining the multifunctional design optimization of these structures with progressive degradation due to cyclic loading could lead to fatigue-activated attritable systems with potentially tailorable performances not yet in reach by current conventional systems. Nevertheless, in order to deploy these complex geometry structures their multiphysics response has to be well understood and characterized. The objective of the current effort is to describe an initial approach for designing a uniaxial metamaterial specimen for fatigue testing as the first step toward the design of multiaxial fatigue test coupons. In order to compare bending- and stretching-dominated structures, two strut-based lattices made of Ti-6Al-4V alloy consisting of the octet and tetrakaidecahedron (or Kelvin) cells are examined. The specimens are designed to fail in the central area of the specimen where edge effects are minimized. Finite element results of the relevant structural mechanics are implemented and exercised to compare the performance of the four relevant geometries and to evaluate the effect of relative density on fatigue life.
实现基于叠加制造支柱的格状超材料的耐疲劳设计
增材制造(AM)技术的出现使周期性和非周期性超材料(又称晶格或蜂窝结构)的原型得以实现,这些超材料可用于各种工程应用,在这些应用中,某些性能特征组合是理想的。例如,这些结构可用于需要轻质、大表面积、能量吸收、散热和声带隙控制的各种海军工程应用中。此外,将这些结构的多功能优化设计与循环载荷导致的渐进降解相结合,可产生可疲劳激活的可穿戴系统,其潜在的可定制性能是目前的传统系统所无法企及的。尽管如此,要部署这些复杂几何结构,必须充分了解和描述它们的多物理场响应。当前工作的目标是描述设计用于疲劳测试的单轴超材料试样的初步方法,作为设计多轴疲劳测试券的第一步。为了比较以弯曲和拉伸为主的结构,我们研究了由八面体和四开十面体(或开尔文)单元组成的两种基于 Ti-6Al-4V 合金的支柱晶格。试样设计为在试样中心区域失效,边缘效应最小。对相关结构力学的有限元结果进行了实施和演算,以比较四种相关几何形状的性能,并评估相对密度对疲劳寿命的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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