Figure 1

Supercapacitors provide exceptional power density, high dimensional stability, and very long cycle life, making them excellent candidates for new structural energy storage systems. They typically use high surface area carbon electrodes laminated with a separator ( and ). This architecture maps onto conventional composite laminate designs if suitable constituents are developed. However, there are several challenges. One is to provide a ‘structural electrode’, a conductive carbon-rich electrode with high electrochemical surface area and maximum mechanical performance, in particular stiffness and strength. Here, we use both intrinsically high strength nanoscale carbons (nanotubes), and combine high strength carbon fibres with nanostructured carbon matrices.

Figure 2

For example, structural supercapacitor composites can combine carbon fibre fabrics with thin electric double-layer capacitor based on carbon nanotube (CNT) fibre veils as interleaves, () as shown in Figure 1. The first step is to produce a thin (100 micron-thick) electrochemical double-layer capacitor (EDLC) by laminating two CNT fibre electrodes with a polymer electrolyte. This material can then be integrated between structural woven CF lamina by a conventional vacuum resin infusion manufacturing process. This strategy produces structural composites with electrochemical properties that are very resilient to mechanical deformations. In-situ galvanostatic charge discharge measurements during bending show almost no changes in capacitance even at very large deformations (Figure 2 a-d). This resilience is due to the high toughness of the CNT fibre fabrics.

The second challenge is the development of a ‘structural electrolyte’ that can carry mechanical shear loads whilst providing a high ionic conductivity. Here, we use nanostructured polymer systems that organise to form bicontinuous structural and ionic-conducting phases, though thermally-induced phase segregation ()) or self-assembly of block copolymers (). For example, a fine-tuned mixture of a structural matrix with a lithium salt, segregates upon curing into a bi-continuous microstructure of stiff matrix with channels for ion transport (). A more top-down approach, can exploit CNT fibre electrodes: by making macroscopic patterns in the electric double-layer capacitor part of the structural supercapacitor to promote the interconnection of carbon fibre plies by epoxy (Figure 2 e-f). This method is not only simple, but also enables the design and fabrication of composites with different balances of mechanical and electrochemical properties.

Figure 3

Another strategy uses high surface area carbon aerogels as a monolithic porous ‘matrix’ for conventional structural carbon fibres. The aerogel provides both electrochemical activity and mechanical rigidity ( and ) schematically shown in Figure 3.

Realizing high energy/power densities and excellent mechanical properties simultaneously presents numerous challenges in terms of material properties, fabrication routes, testing, evaluation, etc. Further details are discussed in specific reviews on the topic (; ).

References

, N Shirshova, et al.Composites Part A: Applied Science and Manufacturing, Volume: 46, Pages: 96-107 (2013)

, T Carlson and LE Asp, Composites Part B: Engineering, Volume 49, Pages 16-21 (2013)

, EA Senokos, et al.Scientific Reports, Volume: 8, Article Number: 3407 (2018)

, H Qian, et al.ACS Applied Materials & Interfaces, Volume: 5, Issue: 13, Pages: 6113-6122 (2013)

, SN Nguyen, et al., Composites Science and Technology, Volume: 182, Article: 107720 (2019)

, H Krebs, et al.,Reactive and Functional Polymers, Volume: 72, Issue: 12, Pages: 931-938 (2012)

, S Leijonmarck, et al., Composites Science and Technology, Volume: 89, Pages: 149-157 (2013)

, N Shirshova, et al., Journal of Materials Chemistry A, Volume: 1, Issue: 48, Pages: 15300–15309 (2013)

, Chapter 20 - Multifunctional structural battery and supercapacitor composites, LE Asp and ES Greenhalgh, Challenges and New Solutions, Pages: 619-611 (2015)

, C González, et al., Progress in Materials Science, Volume: 89, Pages: 194-251 (2017)

Contact

Professor Emile S Greenhalgh
Department of Aeronautics
911今日黑料
South Kensington Campus
London SW7 2AZ

+44 (0)7958 210 089
e.greenhalgh@imperial.ac.uk