System-Level Modeling of the Powertrain for an Electric Aircraft with Superconducting Components
A fuel cell-based electric aircraft is considered a long-term solution for medium range flights to reduce aviation Carbon footprint. Equipping its powertrain with superconductivity reduces the weight and spance and increases efficiency. Such a powertrain includes components, such as superconducting...
Enregistré dans:
| Auteur principal: | |
|---|---|
| Format: | Online |
| Langue: | anglais |
| Publié: |
KIT Scientific Publishing
2025
|
| Sujets: | |
| Accès en ligne: | ONIX_20251202T160246_9783731514350_34 |
| Tags: |
Pas de tags, Soyez le premier à ajouter un tag!
|
| Résumé: | A fuel cell-based electric aircraft is considered a long-term solution for medium range flights to reduce aviation Carbon footprint. Equipping its powertrain with superconductivity reduces the weight and spance and increases efficiency. Such a powertrain includes components, such as superconducting fault current limiter, DC/AC cables and motor, and DC/AC inverter. This work presents the approach to model such a powertrain in MATLAB/SIMULINK for simulation in various flight scenarios. |
|---|