An electrical power system is disclosed for an aircraft having a hybrid-electric propulsion system, which includes a battery assembly for storing energy, an electric motor controller operatively connected to the battery assembly for conditioning and controlling power to an electric motor, and an electric motor receiving power through the motor controller for delivering torque to a shaft of the hybrid-electric propulsion system.
ELECTRICAL POWER SYSTEM FOR AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM
ELEKTRISCHES ANTRIEBSSYSTEM FÜR FLUGZEUG MIT EINEM HYBRIDEN ELEKTRISCHEN ANTRIEBSSYSTEM
SYSTÈME D'ALIMENTATION ÉLECTRIQUE POUR AÉRONEF AYANT UN SYSTÈME DE PROPULSION HYBRIDE-ÉLECTRIQUE
2022-11-16
Patent
Electronic Resource
English
ELECTRICAL POWER SYSTEM FOR AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM
European Patent Office | 2020
|ELECTRICAL POWER SYSTEM FOR AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM
European Patent Office | 2021
|ELECTRICAL POWER SYSTEM FOR AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM
European Patent Office | 2020
|