journal article·2019-10

Unit cell modeling on torsion damage behavior of a novel three-dimensional integrated multilayer fabric-reinforced composite tubular structure

Bing He, Zhongxing Mi, Youjiang Wang, Bohong Gu

Textile Research Journal· Volume 89· Issue 19-20
Publisher page

Abstract

Torsion damage behaviors of composite tubes are key factors in the design of tube structures, such as transmission shafts. During service, torsion in the transmission shaft induces delamination damage. A novel three-dimensional fully integrated multilayer tubular fabric aimed to eliminate delamination was invented by authors. This fabric is in tubular form with several layers of crimp-free in-layer yarns oriented at prescribed orientations and fully interlocked by a set of through-layer yarns, which are often made of the same type of fibers as the in-layer yarns. We investigated torsion damage behaviors of the integrated fabric-reinforced composite tubes. The torque–torsion angle curves were obtained and the torsion damages were phenomenologically analyzed. A unit cell model of the integrated fabric composite circular tube was established to numerically reveal the torsion damage mechanisms. For optimizing the torsion behaviors, the axial yarns should have high stiffness and the binder yarn should have high strength. More specifically, the axial yarn should use carbon fiber tows, and high-strength polymer fiber tows could be used for the binder yarns.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Structural Analysis and Optimization · Mechanical Behavior of Composites · Mechanical stress and fatigue analysis

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

College of Textiles, Donghua University, China

Stoneferry Technology, LLC, USA

School of Materials Science & Engineering, Georgia Institute of Technology, USA

References (27)

Show source-provided references
1. 10.1016/j.ijimpeng.2008.09.00610.1016/j.ijimpeng.2008.09.006 ↗
2. 10.1016/S0008-6223(02)00442-610.1016/S0008-6223(02)00442-6 ↗
3. 10.1016/j.compstruct.2005.04.00610.1016/j.compstruct.2005.04.006 ↗
4. 10.1016/S0261-3069(00)00030-310.1016/S0261-3069(00)00030-3 ↗
5. 10.1016/j.matlet.2005.01.00710.1016/j.matlet.2005.01.007 ↗
6. Sancaktar E and Schauber DA. Failure behavior of filament-wound carbon fiber/epoxy composite tubes under axial compression. In: ASME 2 003 international mechanical engineering congress and exposition , Conference Sponsors: Textile Engineering Division, Washington, DC, USA, 15–21 November, pp.441–452.10.1115/IMECE2003-41656 ↗
7. Wu F, Xiao X, Dong Y, et al. Quasi-static axial crush response and energy absorption of layered composite structure formed from novel crochet-sintered mesh tube and thin-walled tube. Compos Struct 2018; 192: 592–604.10.1016/j.compstruct.2018.03.054 ↗
8. 10.1016/j.ast.2007.03.00410.1016/j.ast.2007.03.004 ↗
9. 10.1016/j.matdes.2014.03.06910.1016/j.matdes.2014.03.069 ↗
10. 10.1177/073168441769425510.1177/0731684417694255 ↗
11. 10.1016/j.compstruct.2006.04.04610.1016/j.compstruct.2006.04.046 ↗
12. 10.1177/002199831772204310.1177/0021998317722043 ↗
13. 10.1016/j.matdes.2010.08.04210.1016/j.matdes.2010.08.042 ↗
14. 10.1016/S0020-7683(01)00170-610.1016/S0020-7683(01)00170-6 ↗
15. Wang Y, Zhao Q, Mi Z-X, et al. Method of forming integrated multilayer fabrics . Patent 8,082,761 B2, USA, 2011.
16. Mi Z-X, Zhao Q, Wang Y, et al. Integrated hollow fabric structure . Patent 8,161,775 B2, USA, 2012.
17. Mi Z-X, Zhao Q, Wang Y, et al. Integrated multiaxial articles: method, apparatus and fabrics . Patent 8,341,980 B2, USA, 2013.
18. 10.1016/j.compositesa.2017.09.00910.1016/j.compositesa.2017.09.009 ↗
19. 10.1016/j.compositesa.2016.11.03310.1016/j.compositesa.2016.11.033 ↗
20. 10.1016/S0266-3538(01)00098-710.1016/S0266-3538(01)00098-7 ↗
21. Huang ZM · Compos Sci Technol · 2004 · 64 · 518
22. 10.1177/08927057000130040110.1177/089270570001300401 ↗
23. 10.1177/00219983710050010610.1177/002199837100500106 ↗
24. 10.1007/s11668-017-0304-510.1007/s11668-017-0304-5 ↗
25. 10.1533/ijcr.2004.028910.1533/ijcr.2004.0289 ↗
26. 10.1016/j.compositesa.2016.11.03310.1016/j.compositesa.2016.11.033 ↗
27. 10.1016/j.compstruct.2016.10.13010.1016/j.compstruct.2016.10.130 ↗