There is disclosed a rotor for an aircraft capable of hovering, comprising: a stationary support structure; a rotative element, which is rotatable about a first axis with respect to said stationary support structure with a first rotational speed; at least one blade, which is operatively connected with said rotative element; and a transmission group, which comprises an output element rotatable about first axis with a second rotational speed different from first rotational speed.


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    Titel :

    ROTOR FOR AN AIRCRAFT CAPABLE OF HOVERING


    Beteiligte:
    BOTTASSO LUIGI (Autor:in) / ZOCCHI ANTONIO (Autor:in) / BRUNETTI MASSIMO (Autor:in) / MEDICI LUCA (Autor:in) / WANG JAMES (Autor:in) / LUCCHI GIORGIO (Autor:in)

    Erscheinungsdatum :

    21.11.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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