A propulsion system for a helicopter includes a linked turbine engine that is configured to drive a main rotor configured to be coupled to a rotary wing. The propulsion system further includes an electric machine that is configured to form an electric motor. The electric machine is coupled directly or indirectly to the main rotor.
SYSTEME PROPULSIF POUR UN HELICOPTERE
PROPULSION SYSTEM FOR A HELICOPTER
ANTRIEBSSYSTEM FÜR EINEN HUBSCHRAUBER
2024-01-03
Patent
Electronic Resource
French