An electrically powered propulsion system for an aircraft includes batteries, electric propulsion assemblies, and power distribution circuits. Each battery is coupled with two or more of the electric propulsion assemblies via a respective one of the power distribution circuits. The electric propulsion assemblies are positioned on the aircraft and operable to apply balanced forces to the aircraft such that in the event of a failure, the aircraft is not subjected to large changes in roll, pitch, and/or yaw.
ELECTRICALLY POWERED PROPULSION SYSTEMS FOR AIRCRAFT
12.09.2024
Patent
Elektronische Ressource
Englisch