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 (É2); 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 (É1) different from first rotational speed (É2).


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    Title :

    ROTOR FOR AN AIRCRAFT CAPABLE OF HOVERING


    Additional title:

    ROTOR FÜR EIN SCHWEBEFLUGFÄHIGES LUFTFAHRZEUG
    ROTOR POUR UN AÉRONEF CAPABLE DE VOL STATIONNAIRE


    Contributors:

    Publication date :

    2019-07-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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