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.


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    Title :

    SYSTEME PROPULSIF POUR UN HELICOPTERE


    Additional title:

    PROPULSION SYSTEM FOR A HELICOPTER
    ANTRIEBSSYSTEM FÜR EINEN HUBSCHRAUBER



    Publication date :

    2024-01-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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