Abstract
Electric aircraft represent a promising lowemission alternative to conventional fuel-powered aviation. This study proposes a battery sizing method for small all-electric aircraft using an electro-thermal battery cell model, considering different flight segments based on a reference commercial aircraft. The experiment is conducted to verify the proposed electro-thermal battery cell model. It considers varying battery efficiency throughout the flight mission, highlighting the importance of battery efficieny in the design process.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the 2025 Energy Conversion Congress & Expo Europe (ECCE Europe) |
| Publisher | IEEE |
| Number of pages | 6 |
| ISBN (Electronic) | 979-8-3315-6752-1 |
| ISBN (Print) | 979-8-3315-6753-8 |
| DOIs | |
| Publication status | Published - 2025 |
| Event | 2025 Energy Conversion Congress & Expo Europe (ECCE Europe) - Birmingham, United Kingdom Duration: 1 Sept 2025 → 4 Sept 2025 |
Conference
| Conference | 2025 Energy Conversion Congress & Expo Europe (ECCE Europe) |
|---|---|
| Country/Territory | United Kingdom |
| City | Birmingham |
| Period | 1/09/25 → 4/09/25 |
Bibliographical note
Green Open Access added to TU Delft Institutional Repository as part of the Taverne amendment. More information about this copyright law amendment can be found at https://www.openaccess.nl. Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public.Keywords
- All-electric aircraft (AEA)
- battery
- electro-thermal model
- efficiency