An aircraft propulsion unit includes an electric motor, at least one accessory unit used for operating the electric motor, an inverter module, the inverter module including a plurality of inverters for powering the electric motor and the at least one accessory unit, and a cooling system coupled to the electric motor and the inverter module, the cooling system comprising a coolant path for circulating a coolant through or adjacent to the electric motor and the at least one accessory unit.
AIRCRAFT PROPULSION UNIT
FLUGZEUGANTRIEBSEINHEIT
UNITÉ DE PROPULSION D'AÉRONEF
2023-12-20
Patent
Elektronische Ressource
Englisch