An engine for an aircraft is presented comprising a rotor, an electric motor actuating the rotation of the rotor and an ECU controlling the electric motor, wherein the rotation of the rotor provides a main flow of air causing the thrust of the engine and wherein the ECU is located within the volume defined by the main flow.

    L'invention concerne un moteur pour un aéronef comprenant un rotor, un moteur électrique mettant le rotor en rotation et une unité de commande électronique commandant le moteur électrique, la rotation du rotor fournissant un flux principal d'air provoquant la poussée du moteur et l'unité de commande électronique étant située à l'intérieur du volume défini par le flux principal.


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    Title :

    AIRCRAFT ENGINE


    Additional title:

    MOTEUR D'AÉRONEF


    Contributors:

    Publication date :

    2022-08-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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