A rotor for a hover-capable aircraft is described that comprises: a drive mast; a hub operatively connected to the drive mast and rotatable about a first axis; and at least two blades hinged to the hub, 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 with respect to said hub; the aircraft further comprising sensor means configured to detect the attitude of at least one said blade with respect to the hub; the sensor means are configured to acquire an optical image associated with the attitude of the blade with respect to the hub.


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    Titel :

    Rotor for a hover-capable aircraft and method for detecting the attitude of a blade with respect to a hub of such a rotor


    Beteiligte:
    REDAELLI MATTEO (Autor:in) / RIVIELLO LUCA (Autor:in) / COLOMBO ATTILIO (Autor:in) / TRAINELLI LORENZO (Autor:in) / ZAPPA EMANUELE (Autor:in) / ROLANDO ALBERTO (Autor:in) / CORDISCO POTITO (Autor:in) / VIGONI EDOARDO (Autor:in) / TERRANEO MAURO (Autor:in) / GRASSETTI RICCARDO (Autor:in)

    Erscheinungsdatum :

    2020-10-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / H04N PICTORIAL COMMUNICATION, e.g. TELEVISION , Bildübertragung, z.B. Fernsehen



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