Un dispositif propulsif à portance active (100) comprend une aile annulaire (110) et un ensemble de propulsion à hélices (120) présent à l'intérieur de l'aile annulaire (110). L'ensemble de propulsion (120) comprend des première et deuxième hélices (122, 123) placées de manière colinéaire à l'intérieur de l'aile annulaire. Les première et deuxième hélices (122, 123) sont contra rotatives.

    The invention relates to an active lift propulsion device (200) comprising a ring aerofoil (210) and a propulsion assembly with propellers (220) provided inside the ring aerofoil (210), the propulsion assembly (220) comprising a plurality of propellers (223, 224), the propellers being aligned according to a reference plane perpendicular to a longitudinal axis (XC210) of the ring aerofoil. One portion of the propellers is driven in a first direction of rotation while the other portion of the propellers is driven in a second direction of rotation opposite the first direction of rotation. The ring aerofoil (210) has, in cross-section, an oval shape extending around the longitudinal axis (XC210). The ring aerofoil includes an upper portion (2101) extending downstream from the reference plane perpendicular to the longitudinal axis and a lower portion (2100) extending upstream from said reference plane. The two propellers (223, 224) extend near the trailing edge (212) of the ring aerofoil at the lower portion (2100) of the ring aerofoil (210), and near the leading edge (211) of the ring aerofoil at the upper portion (2101) of said ring aerofoil.


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    Title :

    DISPOSITIF PROPULSIF A PORTANCE ACTIVE


    Contributors:

    Publication date :

    2019-08-16


    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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