Aircraft electric propulsion system including: a motor including a hollow rotor, and a power and control electronics device, in which the power and control electronics device includes at least two ring-shaped electrical tracks each including at least two inverters, the inverters being connected to each other in parallel, wherein the electrical tracks delimit a hollow circular part of the power and control electronics device, the hollow circular part being placed in the axis of the hollow rotor of the motor.
AIRCRAFT ELECTRIC PROPULSION SYSTEM
2024-07-25
Patent
Electronic Resource
English
Electric propulsion system for aircraft, aircraft comprising such electric propulsion system
European Patent Office | 2024
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