An aeronautical thruster having a longitudinal axis and having a hub, an upstream annular row and a downstream annular row which are spaced apart from each another along the longitudinal axis, the upstream annular row being rotatable around the longitudinal axis, and the downstream annular row having a first blade and a second blade each extending in a radial direction to define a radial dimension between the hub and a radially outer end of the corresponding blade. When observed angularly around the longitudinal axis, the second blade can be positioned closer to an angular position at 3 o'clock or an angular position at 9 o'clock than the first blade, and the radial dimension of the first blade can be greater than the radial dimension of the second blade.


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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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