A hybrid propulsion system for a multi-rotor rotary-wing aircraft, including: an internal combustion engine, an electric machine coupled to the internal combustion engine, a rectifier connected to the electric machine, a converter, an electric network connecting the rectifier to the converter, electric motors connected to the converter, rotary-blade assemblies coupled to the electric motors, wherein the system includes: a detector configured to detect a reduction in a demand for electrical power within the system to below a predetermined value, a bypass circuit configured to bypass the electric machine when the detector detects a reduction in the demand for electrical power.


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    Title :

    SYSTÈME PROPULSIF HYBRIDE ET PROCÉDÉ DE CONTRÔLE D'UN TEL SYSTÈME


    Additional title:

    HYBRID PROPULSION SYSTEM AND METHOD FOR CONTROLLING SUCH A SYSTEM
    HYBRIDANTRIEBSSYSTEM UND VERFAHREN ZUR STEUERUNG EINES SOLCHEN SYSTEMS


    Contributors:

    Publication date :

    2023-08-30


    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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