期刊
PROGRESS IN AEROSPACE SCIENCES
卷 135, 期 -, 页码 -出版社
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.paerosci.2022.100860
关键词
Carbon fibre; Lattice cylindrical shell; Mechanical properties; Analytical modelling; Mechanical testing
资金
- National Natural Science Foundation of China [11972184, 11802212, U20A20286]
- Natural Science Foundation of Jiangsu Province of China [BK20201286]
- Systematic Project of Guangxi Key Laboratory of Disaster Prevention and Engineering Safety [2021ZDK006]
This article introduces the application of carbon fiber reinforced composite lattice cylindrical shells in lightweight structural designs. The configurations of three typical lattice structures are demonstrated, and their performance under compression and vibration is discussed. Non-destructive methods and failure theories are also presented to predict the mechanical properties and failure loads of the 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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