A rotor (8, 8', 106"', 106"", 106""', 106""") for an aircraft (1, 100) is described, comprising an input shaft (10, 108) rotatable around a first axis (C, I); an output member (15, 112) rotatable around a second axis (D, J); a coupling element (20, 20', 20", 20"') functionally interposed between the input shaft (10, 108) and the output member (15, 112) and adapted to transmit the motion from the input shaft (10, 108) to the output member (15, 112); the coupling element (20, 20', 20", 20"') is configured to allow, in use, a fixed or variable inclination between the respective first and second axes (C, I, D, J); the coupling element (20, 20', 20", 20"') comprises at least a first corrugated element (21, 22, 25, 120"', 121"', 120"", 121"", 122"") made of an elastically deformable material; the first corrugated element (21, 22, 25; 120"', 121"'; 120"", 121"", 122"") allows the inclination through elastic deformation.


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    Titel :

    ROTOR FOR AN AIRCRAFT CAPABLE OF HOVERING


    Weitere Titelangaben:

    ROTOR FÜR EIN FLUGZEUG, DAS SCHWEBEFÄHIG IST
    ROTOR POUR UN AÉRONEF CAPABLE DE VOL STATIONAIRE


    Beteiligte:
    BOTTASSO LUIGI (Autor:in) / POGGI STEFANO (Autor:in) / WOODY PHIL (Autor:in) / LOSI FABRIZIO (Autor:in) / NAVA ALESSANDRO (Autor:in) / SARTORI SERGIO (Autor:in) / SIMONETTA ROBERTO (Autor:in) / AIROLDI ALESSANDRO (Autor:in) / BOIOCCHI MATTEO (Autor:in)

    Erscheinungsdatum :

    03.08.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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