Comparative performance assessment of li batteries with solid and highly concentrated electrolytes for aviation applications

Non-flammable next-generation batteries with high power and energy density are essential to meet the high demands of aircraft applications. These cells require electrolytes that not only are stable but that also ensure reliable battery performance under dynamic load conditions. This study employs a physicochemical model to evaluate and compare the electrochemical performance of cells using different cathodic electrolytes: hybrid solid electrolytes, highly concentrated liquid electrolytes, and ionic liquids (ILs). To isolate the intrinsic behavior of each electrolyte under ideal conditions, the evaluation deliberately excludes side reactions, interfacial stability, and contact limitations, focusing solely on gravimetric energy, power output, and mission performance theoretically achievable with such cells. Cells with LiFSI as salt, IL-hydrofluoroether (HFE) as cathode electrolyte or with LiFSA as salt and sulfolane-HFE show superior performance and require less battery mass for aircraft use. To meet the mission requirements of a regional aircraft configuration and when assuming ideal conditions, cathode thicknesses of 70 μm, 60 μm, and 40 μm for sulfolane-HFE, IL-HFE, and hybrid solid electrolytes, respectively, were determined. This approach helps to identify promising electrolyte candidates, exclude stable candidates that cannot fulfil the dynamic power demand, reduce unnecessary experimental efforts, and support the development of efficient and safe battery systems for aviation. • Li-batteries with hybrid solid electrolytes face ionic transport limits, lowering high-rate performance. • Cells with sulfolane-HFE and IL-HFE electrolytes show high energy and power for aircraft systems. • LiFSA-sulfolane/HFE and LiFSI-IL/HFE batteries can reduce aircraft system weight by up to 50%. • Optimal cathode thickness depends on electrolyte type and discharge rate for best specific energy. • For 2C discharge, optimal thickness is 70 µm for LiFSA-sulfolane/HFE and 60 µm for LiFSI-IL/HFE.

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Publication Details

Journal
Journal of Energy Storage
Published
2025-09-04
DOI
https://doi.org/10.1016/j.est.2025.118213
Citations
1
Primary Topic
Advanced Battery Materials and Technologies
Type
article
Field-Weighted Citation Impact
0.73

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Comparative performance assessment of li batteries with solid and highly concentrated electrolytes for aviation applications

Helmut Kühnelt, Ulrike Krewer, Florian Baakes, Ningxin Zhang et al.
1 citations
Journal of Energy Storage
Advanced Battery Materials and Technologies
0.73
article

Comparative performance assessment of li batteries with solid and highly concentrated electrolytes for aviation applications

Helmut Kühnelt, Ulrike Krewer, Florian Baakes, Ningxin Zhang, Somayeh Toghyani
article en
1 citations

Abstract

Non-flammable next-generation batteries with high power and energy density are essential to meet the high demands of aircraft applications. These cells require electrolytes that not only are stable but that also ensure reliable battery performance under dynamic load conditions. This study employs a physicochemical model to evaluate and compare the electrochemical performance of cells using different cathodic electrolytes: hybrid solid electrolytes, highly concentrated liquid electrolytes, and ionic liquids (ILs). To isolate the intrinsic behavior of each electrolyte under ideal conditions, the evaluation deliberately excludes side reactions, interfacial stability, and contact limitations, focusing solely on gravimetric energy, power output, and mission performance theoretically achievable with such cells. Cells with LiFSI as salt, IL-hydrofluoroether (HFE) as cathode electrolyte or with LiFSA as salt and sulfolane-HFE show superior performance and require less battery mass for aircraft use. To meet the mission requirements of a regional aircraft configuration and when assuming ideal conditions, cathode thicknesses of 70 μm, 60 μm, and 40 μm for sulfolane-HFE, IL-HFE, and hybrid solid electrolytes, respectively, were determined. This approach helps to identify promising electrolyte candidates, exclude stable candidates that cannot fulfil the dynamic power demand, reduce unnecessary experimental efforts, and support the development of efficient and safe battery systems for aviation. • Li-batteries with hybrid solid electrolytes face ionic transport limits, lowering high-rate performance. • Cells with sulfolane-HFE and IL-HFE electrolytes show high energy and power for aircraft systems. • LiFSA-sulfolane/HFE and LiFSI-IL/HFE batteries can reduce aircraft system weight by up to 50%. • Optimal cathode thickness depends on electrolyte type and discharge rate for best specific energy. • For 2C discharge, optimal thickness is 70 µm for LiFSA-sulfolane/HFE and 60 µm for LiFSI-IL/HFE.

Journal of Energy StorageVol. 135
AIT Austrian Institute of Technology GmbH (AT), Applied Materials (Singapore) (SG)
Horizon 2020 Framework Programme, HORIZON EUROPE Framework Programme
Openalex Percentile: Top 24%
Advanced Battery Materials and Technologies
0.73
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