A power distribution circuit for an electrically powered aircraft includes a plurality of batteries and a plurality of electric propulsion systems. A plurality of isolated power distribution circuits each couple a battery of the plurality of batteries to two or more electric propulsion systems. The plurality of electric propulsion systems are positioned on the aircraft to apply balanced forces to the aircraft such that in the event of a failure, the aircraft remains stable and only experiences a loss in altitude or speed.
ELECTRICALLY POWERED PROPULSION SYSTEMS FOR AIRCRAFT
ELEKTRISCH ANGETRIEBENE ANTRIEBSSYSTEME FÜR FLUGZEUGE
SYSTÈMES DE PROPULSION À ALIMENTATION ÉLECTRIQUE POUR AÉRONEF
13.11.2024
Patent
Elektronische Ressource
Englisch