The invention relates to an aeronautical thruster (10) having a longitudinal axis (X) and comprising a hub (12), an upstream annular row (14) and a downstream annular row (16) spaced apart from one another along said longitudinal axis (X), the upstream annular row (14) being rotatable about the longitudinal axis (X), and the downstream annular row (16) comprising a first blade (18a) and a second blade (18b) each extending in a radial direction so as to define a radial dimension between the hub (12) and a radially outer end of the corresponding blade (18a; 18b); wherein, observed angularly about the longitudinal axis (X), the second blade (18b) is positioned closer to an angular position at 3H or an angular position at 9H than the first blade (18a), and the radial dimension of the first blade (18a) is greater than the radial dimension of the second blade (18b).


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    Title :

    PROPULSEUR AERONAUTIQUE


    Additional title:

    AERONAUTICAL THRUSTER
    AERONAUTISCHER ANTRIEB



    Publication date :

    2024-05-15


    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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