Abstract This article proposes a mission-profile-based sizing methodology for DC-link capacitors in eVTOL propulsion inverters. While DC-link capacitors contribute significantly to converter volume, traditional design relies on conservative worst-case operating points, leading to significant oversizing. To address this, an electro-thermal modelling approach is developed to evaluate capacitor lifetime based on core temperature fluctuations throughout a dynamic flight profile. The methodology accounts for thermal properties, modulation strategies, and the effects of fault-tolerant operation. Although the method is applicable to various inverter topologies and capacitor technologies, the three-level T-type (3L-TT) fault-tolerant converter benefits most, as demonstrated by an exemplary design achieving a 37.5% reduction in DC-link volume compared to conventional methods while for a specified life-time goal.
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Niklas Krug
Marek Gałek
Florian Holzapfel
Aerospace Systems
Technical University of Munich
Institute of Flight
Sustainable Energy Systems (United Kingdom)
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Krug et al. (Tue,) studied this question.
www.synapsesocial.com/papers/69f2a4f18c0f03fd67764083 — DOI: https://doi.org/10.1007/s42401-026-00477-y