轻质碳纤维增强格子圆柱壳的最新进展

IF 11.5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Ming Li , Hengyi Zhu , Changliang Lai , Wenyi Bao , Han Han , Renbang Lin , Weiping He , Hualin Fan
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引用次数: 9

摘要

碳纤维增强复合材料(CFRC)由于具有较高的强度和刚度,被广泛应用于航空航天工程的轻量化结构设计。在复合材料圆柱壳中引入各种各样的晶格被认为是提高力学性能并同时减轻重量的最有前途的策略之一。本文介绍了晶格、晶格夹层和晶格加筋壳三种典型晶格结构的构型和制造方法。实验研究了这些圆柱壳在压缩下的力学性能,以及它们的自由振动特性。此外,还提出了一种非破坏性的方法,可以对此类壳体的力学性能和屈曲载荷进行非破坏性的识别。此外,还提出了多失效理论来预测失效载荷和失效模式。最后,对CFRC格子圆柱壳在轻量化设计中的发展进行了总结。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Recent progresses in lightweight carbon fibre reinforced lattice cylindrical shells

Owing to their high strengths and stiffnesses, carbon fibre reinforced composites (CFRC) are widely used in aerospace engineering for lightweight structural designs. The introduction of a wide variety of lattices into composite cylindrical shells is considered one of the most promising strategies for improving the mechanical properties and simultaneously reducing weight. Herein, the configurations and manufacturing methods of three typical types of lattice structures, namely lattice, lattice sandwich, and lattice stiffened shells, are demonstrated. Experimental investigations are presented to discuss the mechanical properties of these cylindrical shells under compression, along with their free vibration characteristics. Further, non-destructive methods, which can identify the mechanical properties and buckling loads of such shells non-destructively, are demonstrated. Moreover, multi-failure theories proposed to predict the failure loads and failure modes are presented. Finally, the development of CFRC lattice cylindrical shells in lightweight designs is summarised.

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来源期刊
Progress in Aerospace Sciences
Progress in Aerospace Sciences 工程技术-工程:宇航
CiteScore
20.20
自引率
3.10%
发文量
41
审稿时长
5 months
期刊介绍: "Progress in Aerospace Sciences" is a prestigious international review journal focusing on research in aerospace sciences and its applications in research organizations, industry, and universities. The journal aims to appeal to a wide range of readers and provide valuable information. The primary content of the journal consists of specially commissioned review articles. These articles serve to collate the latest advancements in the expansive field of aerospace sciences. Unlike other journals, there are no restrictions on the length of papers. Authors are encouraged to furnish specialist readers with a clear and concise summary of recent work, while also providing enough detail for general aerospace readers to stay updated on developments in fields beyond their own expertise.
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