There is disclosed a rotor (3, 3', 3'') for an aircraft (1) capable of hovering, comprising: a stationary support structure (10); a rotative element (11), which is rotatable about a first axis (A) with respect to said stationary support structure (10) with a first rotational speed (ω2); at least one blade (13), which is operatively connected with said rotative element (11); and a transmission group (37, 37''), which comprises an output element (36, 36', 36'') rotatable about first axis (A) with a second rotational speed (ω1) different from first rotational speed (ω2).

    L'invention concerne un rotor (3, 3', 3'') d'un aéronef (1) permettant un vol stationnaire, comprenant : une structure de support fixe (10) ; un élément rotatif (11) pouvant tourner autour d'un premier axe (A) par rapport à ladite structure de support fixe (10) à une première vitesse de rotation (ω2) ; au moins une pale (13) reliée fonctionnellement audit élément rotatif (11) ; et un groupe de transmission (37, 37'') comprenant un élément de sortie (36, 36', 36'') pouvant tourner autour d'un premier axe (A) à une seconde vitesse de rotation (ω1) différente de la première vitesse de rotation (ω2).


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    Title :

    ROTOR FOR AN AIRCRAFT CAPABLE OF HOVERING


    Additional title:

    ROTOR D'AÉRONEF PERMETTANT UN VOL STATIONNAIRE


    Contributors:

    Publication date :

    2018-07-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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