SCIENCE CHINA Technological Sciences, Volume 62 , Issue 8 : 1478-1480(2019) https://doi.org/10.1007/s11431-018-9489-1

How green composite materials could benefit aircraft construction

More info
  • ReceivedDec 19, 2018
  • AcceptedMar 7, 2019
  • PublishedJun 13, 2019


There is no abstract available for this article.


[1] Bachmann J, Hidalgo C, Bricout S. Environmental analysis of innovative sustainable composites with potential use in aviation sector—A life cycle assessment review. Sci China Tech Sci, 2017, 60: 1301-1317 CrossRef Google Scholar

[2] Bachmann J, Yi X, Gong H, et al. Outlook on ecologically improved composites for aviation interior and secondary structures. CEAS Aeronaut J, 2018, 9: 533-543 CrossRef Google Scholar

[3] Soutis C. Introduction: Engineering Requirements for Aerospace Composite Materials. In: Irving P E, Soutis C, eds. Polymer Composites in the Aerospace Industry. Elsevier, Woodhead Publishing, 2015. 1–17. Google Scholar

[4] Ramon E, Sguazzo C, Moreira P. A review of recent research on bio-based epoxy systems for engineering applications and potentialities in the aviation sector. Aerospace, 2018, 5: 110 CrossRef Google Scholar

[5] Li C, Liu X, Zhu J, et al. Synthesis, characterization of a rosin-based epoxy monomer and its comparison with a petroleum-based counterpart. J MacroMol Sci Part A, 2013, 50: 321-329 CrossRef Google Scholar

[6] Ma S, Liu X, Jiang Y, et al. Bio-based epoxy resin from itaconic acid and its thermosets cured with anhydride and comonomers. Green Chem, 2013, 15: 245-254 CrossRef Google Scholar

[7] Dai J, Peng Y, Teng N, et al. High-performing and fire-resistant biobased epoxy resin from renewable sources. ACS Sustain Chem Eng, 2018, 6: 7589-7599 CrossRef Google Scholar

[8] Zhang X F, Wu Y, Wei J H, et al. Curing kinetics and mechanical properties of bio-based composite using rosin-sourced anhydrides as curing agent for hot-melt prepreg. Sci China Tech Sci, 2017, 60: 1318-1331 CrossRef Google Scholar

[9] Yi X S, Zhang X, Ding F, et al. Development of bio-sourced epoxies for bio-composites. Aerospace, 2018, 5: 65 CrossRef Google Scholar

[10] Li Q, Li Y, Zhou L. A micromechanical model of interfacial debonding and elementary fiber pull-out for sisal fiber-reinforced composites. Compos Sci Tech, 2017, 153: 84-94 CrossRef Google Scholar

[11] Wang C, Ren Z, Li S, et al. Effect of ramie fabric chemical treatments on the physical properties of thermoset polylactic acid (PLA) composites. Aerospace, 2018, 5: 93 CrossRef Google Scholar

[12] Tse B, Yu X, Gong H, et al. Flexural properties of wet-laid hybrid nonwoven recycled carbon and flax fibre composites in poly-lactic acid matrix. Aerospace, 2018, 5: 120 CrossRef Google Scholar

[13] Wang H, Xian G, Li H. Grafting of nano-TiO2 onto flax fibers and the enhancement of the mechanical properties of the flax fiber and flax fiber/epoxy composite. Compos Part A-Appl Sci Manufacturing, 2015, 76: 172-180 CrossRef Google Scholar

[14] Li Y, Yi X, Yu T, et al. An overview of structural-functional-integrated composites based on the hierarchical microstructures of plant fibers. Adv Compos Hybrid Mater, 2018, 1: 231-246 CrossRef Google Scholar

[15] Yang W D, Li Y. Sound absorption performance of natural fibers and their composites. Sci China Tech Sci, 2012, 55: 2278-2283 CrossRef Google Scholar

[16] Zhang J, Shen Y, Jiang B, et al. Sound absorption characterization of natural materials and sandwich structure composites. Aerospace, 2018, 5: 75 CrossRef Google Scholar

[17] Bachmann J, Wiedemann M, Wierach P. Flexural mechanical properties of hybrid epoxy composites reinforced with nonwoven made of flax fibres and recycled carbon fibres. Aerospace, 2018, 5: 107 CrossRef Google Scholar

[18] Tserpes K, Kora C. A multi-scale modeling approach for simulating crack sensing in polymer fibrous composites using electrically conductive carbon nanotube networks. Part II: Meso- and macro-scale analyses. Aerospace, 2018, 5: 106. Google Scholar

[19] Ye L. Functionalized interleaf technology in carbon-fibre-reinforced composites for aircraft applications. Natl Sci Rev, 2014, 1: 7-8 CrossRef Google Scholar

[20] Dong Q, Guo Y, Chen J, et al. Influencing factor analysis based on electrical-thermal-pyrolytic simulation of carbon fiber composites lightning damage. Composite Struct, 2016, 140: 1-10 CrossRef Google Scholar

[21] Guo Y, Dong Q, Chen J, et al. Comparison between temperature and pyrolysis dependent models to evaluate the lightning strike damage of carbon fiber composite laminates. Compos Part A-Appl Sci Manufacturing, 2017, 97: 10-18 CrossRef Google Scholar

[22] Dong S, Xian G, Yi X S. Life cycle assessment of ramie fiber used for FRPs. Aerospace, 2018, 5: 81 CrossRef Google Scholar

[23] Soutis C, Beaumont, P W R. Multi-Scale Modelling of Composite Material Systems: The Art of Predictive Damage Modelling. Elsevier, 2005. Google Scholar

  • Figure 1

    (Color online) (a) Demonstration of an empennage side panel made of bio-sourced epoxy composites with lightning strike protection for C919, courtesy of Weiping Liu, COMAC; (b) interior panel made of ramie fibre fabric, bio-based epoxy and green honeycomb for MA 600, courtesy of Fangbo Ding, XAC-AVIC.

Copyright 2020  CHINA SCIENCE PUBLISHING & MEDIA LTD.  中国科技出版传媒股份有限公司  版权所有

京ICP备14028887号-23       京公网安备11010102003388号