Composite additive manufacturing of morphing aerospace structures

IF 2 Q3 ENGINEERING, MANUFACTURING
Urban Fasel , Dominic Keidel , Leo Baumann , Giovanni Cavolina , Martin Eichenhofer , Paolo Ermanni
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引用次数: 89

Abstract

Continuous carbon fibre composite additive manufacturing opens up new possibilities for automated, cost-effective manufacturing of highly-loaded structures. This is achieved by the high design freedom of the process, allowing to tailor the fibre placement and by thereby fully exploiting the anisotropy and strength of the composite material. On the other hand, compliant or so-called morphing mechanisms – exploiting the elastic properties of the material to achieve shape changes – show great potential in improving the flight performance of aerospace structures. Such structures exhibit complex internal topologies, making them prohibitively expensive to manufacture with conventional processes. Combining additive manufacturing of composites with the utilization of morphing mechanisms has the potential to concurrently reduce manufacturing cost whilst greatly improving the flight performance of aerospace structures. The applicability of composite additive manufacturing to morphing aerospace structures is discussed in this letter. For the first time, the complete composite primary- and morphing-structure of a fixed-wing drone was additively manufactured. The drone was successfully flight-tested, evaluating the potential of combining these two emerging technologies.

可变形航空航天结构的复合增材制造
连续碳纤维复合材料增材制造为高负荷结构的自动化、经济高效制造开辟了新的可能性。这是通过工艺的高度设计自由度来实现的,允许定制纤维放置,从而充分利用复合材料的各向异性和强度。另一方面,柔性或所谓的变形机制-利用材料的弹性特性来实现形状变化-在改善航空航天结构的飞行性能方面显示出巨大的潜力。这种结构表现出复杂的内部拓扑结构,使得用传统工艺制造它们的成本过高。复合材料增材制造与变形机理的结合,在降低制造成本的同时,极大地提高了航空航天结构的飞行性能。本文讨论了复合材料增材制造在航空航天结构变形中的适用性。首次采用增材制造方法制造了固定翼无人机的完整复合材料主结构和变形结构。该无人机成功进行了飞行测试,评估了结合这两种新兴技术的潜力。
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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来源期刊
Manufacturing Letters
Manufacturing Letters Engineering-Industrial and Manufacturing Engineering
CiteScore
4.20
自引率
5.10%
发文量
192
审稿时长
60 days
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