ELECTRICAL POWERING OR DRIVE SYSTEM FOR A MOTOR IN AN ELECTRICALLY DRIVEN AIRCRAFT

This disclosure describes at least embodiments of a power management system for an electric or hybrid aircraft. The system can include a first motor and a second motor supported by a housing of the aircraft. The first motor can be powered by a first battery pack, and the second motor can be powered...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: DEMONT, Sébastien
Format: Patent
Sprache:eng ; fre
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!