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Design and freeform fabrication of deployable structures with lattice skins

机译:具有格子蒙皮的可展开结构的设计和自由形式制造

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Purpose - Frontier environments - such as battlefields, hostile territories, remote locations, or outer space - drive the need for lightweight, deployable structures that can be stored in a compact configuration and deployed quickly and easily in the field. This paper seeks to introduce the concept of lattice skins is introduced to enable the design, solid freeform fabrication (SFF), and deployment of customizable structures with nearly arbitrary surface profile and lightweight multi-functionality. Design/methodology/approach - Using Duraform FLEX material in a selective laser sintering machine, large deployable structures are fabricated in a nominal build chamber by decomposing them into smaller parts. Before fabrication, lattice sub-skins are added strategically beneath the surface of the part. The lattices provide elastic energy for folding and deploying the structure or constrain expansion upon application of internal air pressure. Nearly, arbitrary surface profiles are achievable and internal space is preserved for subsequent usage. Findings - A set of virtual and physical prototypes are presented, along with the computational modeling approach used to design them. The prototypes provide proof of concept for lattice skins as a deployment mechanism in SFF and demonstrate the effect of lattice structures on deployed shape. Research limitations/implications - The research findings demonstrate not only the feasibility of a new deployment mechanism-based on lattice skins - for deploying freeform structures, but also the potential utility of SFF techniques for fabricating customized deployable structures. Originality/value - A new lattice skin mechanism is introduced for deploying structures with nearly arbitrary surface profiles and open, usable, internal space. Virtual and physical prototypes are introduced for proof of concept, along with an optimization approach for automated design of these structures.
机译:目的-边界环境(例如战场,敌对领土,偏远地区或外太空)推动了对轻型可部署结构的需求,这些结构可以紧凑的结构存储并可以在野外快速轻松地部署。本文旨在介绍引入晶格蒙皮的概念,以实现设计,实体自由形式制造(SFF)和部署具有几乎任意表面轮廓和轻巧多功能性的可定制结构。设计/方法/方法-在选择性激光烧结机中使用Duraform FLEX材料,将大的可展开结构分解为更小的零件,从而在标称制造室内制造它们。在制造之前,有策略地在零件表面下添加晶格子蒙皮。当施加内部气压时,格子提供用于折叠和展开结构或限制膨胀的弹性能。几乎可以实现任意的表面轮廓,并保留内部空间以供后续使用。结果-展示了一组虚拟和物理原型,以及用于设计它们的计算建模方法。原型为SFF中的展开机制提供了晶格外观的概念验证,并演示了晶格结构对展开形状的影响。研究的局限性/意义-研究结果不仅证明了基于晶格蒙皮的新型展开机制用于部署自由形式结构的可行性,而且还证明了SFF技术在制造定制可展开结构方面的潜在实用性。创意/价值-引入了一种新的晶格蒙皮机制,用于部署具有几乎任意表面轮廓和开放,可用的内部空间的结构。引入虚拟和物理原型以进行概念验证,以及用于自动设计这些结构的优化方法。

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