Abstract
Industrial-oriented mid-frequency alternating current (MF-AC) magnetron sputtering technique is used to fabricate LiNi0.5Mn1.5O4 high-voltage thin-film cathodes. Films are deposited on bare stainless-steel substrate at room temperature and then annealed to induce crystallization in disordered spinel phase. In situ X-ray diffraction is used to follow film structural evolution from room temperature to 900 °C. Scanning electron microscopy, X-ray photoelectron spectroscopy, and Raman spectroscopy are used to study the evolution with temperature of film morphology, surface chemical composition, and crystal structure arrangement, respectively. Film structure evolves almost continuously in the studied temperature range. A pattern corresponding to spinel phase is observed after annealing at 600 °C, while poor crystallization is obtained for lower temperatures, and additional unwanted phase changes are observed for higher temperatures. Cyclic voltammetry, rate capability, and cycling performance of fabricated films are tested. Only the film annealed at 600 °C shows redox peaks corresponding to Ni oxidation from 2+ to 3+ and 3+ to 4+ oxidation states, confirming that this film crystallizes in disordered spinel phase. The thin-film cathode shows good rate performance and outstanding cyclability, despite the impurities formed upon electrolyte decomposition at high voltage.
Original language | English |
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Article number | 2002125 |
Pages (from-to) | 2002125 |
Number of pages | 1 |
Journal | Advanced Materials Interfaces |
Volume | 8 |
Issue number | 10 |
DOIs | |
Publication status | Published - 21 May 2021 |
Keywords
- AC magnetron sputtering
- Li-ion batteries
- LiNi Mn O
- Raman
- thin-film cathodes
- X-ray photoelectron spectroscopy
- LiNi0.5 Mn1.5 O4
Project and Funding Information
- Project ID
- info:eu-repo/grantAgreement/EC/H2020/687561/EU/Monolithic Batteries for Spaceship Applications/MONBASA
- Funding Info
- The authors acknowledge the financial support from the European H2020 project MONBASA (Monolithic Batteries for Spaceship Applications, Grant No. 687561) and Basque Government through Elkartek 2017 program with the project Elkartek CICe2017‐L4. The authors would also like to acknowledge the assistance and support received from M. Jáuregui for the in situ XRD measurements.