An aeronautical propulsion system (50) defining a central axis and comprising:a fan (104) having a plurality of fan blades (128) rotatable about the central axis and defining a fan pressure ratio, FPR; andan electric motor (136) mechanically coupled to the fan (104) for driving the fan (104), the electric motor (136) comprising a number of poles (154), and defining a maximum power;wherein the relationship between the fan pressure ratio (104), the number of poles (154) of the electric motor (136), and the maximum power of the electric motor (136) is defined by an equation.


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    Title :

    ELECTRIC PROPULSION SYSTEM FOR AN AIRCRAFT


    Additional title:

    ELEKTRISCHES ANTRIEBSSYSTEM FÜR EIN FLUGZEUG
    SYSTÈME DE PROPULSION ÉLECTRIQUE POUR UN AÉRONEF



    Publication date :

    2020-01-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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