A rotor (3, 3') for a hover-capable aircraft (1) is described that comprises: a drive mast (6); a hub (5) operatively connected to the drive mast (6) and rotatable about a first axis (A); and at least two blades (9) hinged to the hub (5), via a rigid or elastically deformable connection, so as to be able to assume an attitude rotated about and/or translated along at least a second axis (B, C, D) with respect to said hub (5); the aircraft (1) further comprising sensor means (25) configured to detect the attitude of at least one said blade (9) with respect to the hub (5); the sensor means (25) are configured to acquire an optical image associated with the attitude of the blade (9) with respect to the hub (5).


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    Titel :

    ВИНТ ДЛЯ ЛЕТАТЕЛЬНОГО АППАРАТА, ВЫПОЛНЕННОГО С ВОЗМОЖНОСТЬЮ ВИСЕНИЯ, И СПОСОБ ОБНАРУЖЕНИЯ ПРОСТРАНСТВЕННОГО ПОЛОЖЕНИЯ ЛОПАСТИ ОТНОСИТЕЛЬНО ВТУЛКИ ТАКОГО ВИНТА


    Erscheinungsdatum :

    12.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Russisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge