Reliability-driven DC-link optimization for fault-tolerant 3L T-type eVTOL propulsion inverters
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.
Authors
- Niklas Krug (ORCID: https://orcid.org/0000-0001-5147-8846)
- Marek Gałek (ORCID: https://orcid.org/0000-0002-6983-9758)
- Florian Holzapfel (ORCID: https://orcid.org/0000-0003-4733-9186)
Institutions
- Institute of Flight (US)
- Sustainable Energy Systems (United Kingdom) (GB)
- Technical University of Munich (DE)
Publication Details
- Journal
- Aerospace Systems
- Published
- 2026-04-28
- DOI
- https://doi.org/10.1007/s42401-026-00477-y
- Primary Topic
- Advanced DC-DC Converters
- Type
- article
- Field-Weighted Citation Impact
- 0.00