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A novel free-hanging 3D printing method for continuous carbon fiber reinforced thermoplastic lattice truss core structures

机译:连续碳纤维增强热塑性晶格桁架芯结构的新型自由悬挂3D打印方法

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摘要

Continuous Fiber Reinforced Thermoplastic (CFRTP) lattice truss core structures are potential to aerospace engineering because of their high weight reduction efficiency and multifunctional application. A novel free-hanging 3D printing method was firstly presented by the authors to manufacture CFRTP lattice truss core structures. The free-hanging printing path generation strategy was established to realize the undercut and overhanging truss structure without any support. Based on the free-hanging 3D printing method, the typical lattice topologies and more complex structures like the integral variable-thickness wing were printed. The cross sectional morphology of samples printed by using the free-hanging printing method were analyzed. The investigations on the parameters such as relative density, fiber volume content and truss angle were conducted to reveal the relationship between the process parameters and out-of-plane compressive properties. The experiment results demonstrated that the average structural error was about 1.89% compared with the theoretical geometry. The compression strength of the printed sample was 224% higher than that of the pure thermoplastic resin counterpart. The specific compressive strength of free-hanging printed samples was in competitive status compared with currently existed CFRTP lattice structures in available literatures. (C) 2017 Elsevier Ltd. All rights reserved.
机译:连续纤维增强热塑性塑料(CFRTP)晶格桁架芯结构具有减轻重量的高效率和多功能应用,因此在航空航天工程中具有潜力。作者首先提出了一种新颖的自由悬挂3D打印方法来制造CFRTP晶格桁架核心结构。建立了自由悬挂式印刷路径生成策略,以在没有任何支持的情况下实现底切和悬垂桁架结构。基于自由悬挂的3D打印方法,可以打印出典型的晶格拓扑结构和更复杂的结构,例如整体可变厚度机翼。分析了使用自由悬挂印刷法印刷的样品的横截面形态。对相对密度,纤维体积含量和桁架角等参数进行了研究,以揭示工艺参数与面外压缩性能之间的关系。实验结果表明,与理论几何尺寸相比,平均结构误差约为1.89%。印刷样品的抗压强度比纯热塑性树脂的抗压强度高224%。与现有文献中现有的CFRTP晶格结构相比,自由悬挂式印刷样品的比抗压强度处于竞争状态。 (C)2017 Elsevier Ltd.保留所有权利。

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