Provided in this disclosure is a dual-motor propulsion assembly, and corresponding methods of operation, that is configured for use in an electric aircraft. Dual-motor propulsion assembly provides redundant systems by including vertically stacked motors, wherein one motor may still power a propulsor of the assembly if the other motor malfunctions or becomes inoperative.
DUAL-MOTOR PROPULSION ASSEMBLY
28.09.2023
Patent
Elektronische Ressource
Englisch