Manufacturing and mechanical properties of composite orthotropic Kagome honeycomb using novel modular method

Abstract

This work deals with manufacturing and analysis of orthotropic composite Kagome honeycomb panels. A novel modular mold is proposed to manufacture carbon fiber reinforced composite Kagome honeycombs. The designed mold can be assembled freely to manufacture Kagome honeycombs with different configuration combinations and can realize easy demolding. Furthermore, two typical fiber placement methods are considered during the fabrication process, from which the more effective fiber placement method is determined. Finally, representative volume element method is used to perform homogenization analysis of the Kagome honeycomb panels and to obtain equivalent in-plane and bending stiffness. Finite element analysis using these equivalent properties is conducted and validated against the experimental results of the manufactured composite Kagome honeycomb panels under different loading cases.

Keywords

composite / Kagome honeycomb / manufacturing / placement of fibers / equivalent stiffness

References

[1] Ashby M F. Drivers for material development in the 21st century. Progress in Materials Science, 2001, 46(3–4): 191–199

[2] Evans A G. Lightweight materials and structures. MRS Bulletin, 2001, 26(10): 790–797

[3] Fan H, Zeng T, Fang D N, Mechanics of advanced fiber reinforced lattice composites. Acta Mechanica Sinica, 2010, 26(6): 825–835

[4] Restrepo D, Mankame N D, Zavattieri P D. Programmable materials based on periodic cellular solids. Part I: Experiments. International Journal of Solids and Structures, 2016, 100–101: 485–504

[5] Fan H, Yang L, Sun F, Compression and bending performances of carbon fiber reinforced lattice-core sandwich composites. Composites. Part A, Applied Science and Manufacturing, 2013, 52: 118–125

[6] Galletti G G, Vinquist C, Es-Said O S. Theoretical design and analysis of a honeycomb panel sandwich structure loaded in pure bending. Engineering Failure Analysis, 2008, 15(5): 555–562

[7] Zhang G, Ma L, Wang B, Mechanical behaviour of CFRP sandwich structures with tetrahedral lattice truss cores. Composites. Part B, Engineering, 2012, 43(2): 471–476

[8] Deshpande V S, Ashby M F, Fleck N A. Foam topology: Bending versus stretching dominated architectures. Acta Materialia, 2001, 49(6): 1035–1040

[9] Totaro G, Gürdal Z. Optimal design of composite lattice shell structures for aerospace applications. Aerospace Science and Technology, 2009, 13(4–5): 157–164

[10] Niu B, Yan J, Cheng G. Optimum structure with homogeneous optimum cellular material for maximum fundamental frequency. Structural and Multidisciplinary Optimization, 2009, 39(2): 115–132

[11] Deshpande V S, Fleck N A. Collapse of truss core sandwich beams in 3-point bending. International Journal of Solids and Structures, 2001, 38(36‒37): 6275–6305

[12] Zuo X Q, Zhou Y, Mei J. Structure and compressive behavior of Fe25Cr5Al metallic honeycomb fabricated by powder extrusion molding and sintering. Materials for Mechanical Engineering, 2006, 30(10): 34–35 (in Chinese)

[13] Vasiliev V V, Barynin V A, Rasin A F. Anisogrid lattice structures—Survey of development and application. Composite Structures, 2001, 54(2‒3): 361–370

[14] Sorrentino L, Marchetti M, Bellini C, Design and manufacturing of an isogrid structure in composite material: Numerical and experimental results. Composite Structures, 2016, 143: 189–201

[15] Han D, Tsai S W. Interlocked composite grids design and manufacturing. Journal of Composite Materials, 2003, 37(4): 287–316

[16] Fan H, Meng F, Yang W. Sandwich panels with Kagome lattice cores reinforced by carbon fibers. Steel Construction, 2008, 81(4): 533–539

[17] Wang A J, McDowell D L. Yield surfaces of various periodic metal honeycombs at intermediate relative density. International Journal of Plasticity, 2005, 21(2): 285–320

[18] Niu B, Wang B. Directional mechanical properties and wave propagation directionality of Kagome honeycomb structures. European Journal of Mechanics. A, Solids, 2016, 57: 45–58

[19] Cheng G, Cai Y, Xu L. Novel implementation of homogenization method to predict effective properties of periodic materials. Acta Mechanica Sinica, 2013, 29(4): 550–556

[20] Cai Y, Xu L, Cheng G. Novel numerical implementation of asymptotic homogenization method for periodic plate structures. International Journal of Solids and Structures, 2014, 51(1): 284–292

[21] Peng B, Yu W. A micromechanics theory for homogenization and dehomogenization of aperiodic heterogeneous materials. Composite Structures, 2018, 199: 53–62 doi:10.1016/j.compstruct.2018.05.047

[22] Liu S, Su W. Effective couple-stress continuum model of cellular solids and size effects analysis. International Journal of Solids and Structures, 2009, 46(14‒15): 2787–2799

[23] Whitney J M. Structural Analysis of Laminated Anisotropic Plates. New York: CRC Press, 1987, 23–26

[24] Dassault Systemes Simulia, Inc. Abaqus Analysis User’s Manual. Version 6.11. 2011

[25] Kueh A, Pellegrino S. ABD matrix of single-ply triaxial weave fabric composites. In: Proceedings of the 48th AIAA/ASME/ASCE/AHS/ASC Structural Dynamics and Materials Conference. Honolulu: AIAA, 2007, 5498–5514

Acknowledgements

This work was partially supported by the National Natural Science Foundation of China (Grant Nos. 51975087, 51790172, 51675082, and 51505064) and the Fundamental Research Funds for the Central Universities (Grant No. DUT17ZD207). These supports are gratefully appreciated.

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